def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 20
channel.test_vals = [-2.667328, 2.797437, 0.018714, 0.006906]
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 20
naca0012.test_vals = [-4.023999, -3.515034, 0.339426, 0.022217]
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 20
wedge.test_vals = [-0.942862, 4.784581, -0.208106, 0.036665]
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [0.281703, 0.011821]
test_list.append(oneram6)
# Fixed CL NACA0012
fixedCL_naca0012 = TestCase('fixedcl_naca0012')
fixedCL_naca0012.cfg_dir = "fixed_cl/naca0012"
fixedCL_naca0012.cfg_file = "inv_NACA0012.cfg"
fixedCL_naca0012.test_iter = 10
fixedCL_naca0012.test_vals = [-7.374806, -1.872330, 0.300000, 0.019471]
test_list.append(fixedCL_naca0012)
# HYPERSONIC FLOW PAST BLUNT BODY
bluntbody = TestCase('bluntbody')
bluntbody.cfg_dir = "euler/bluntbody"
bluntbody.cfg_file = "blunt.cfg"
bluntbody.test_iter = 20
bluntbody.test_vals = [0.540010, 6.916656, 0.000027, 1.869004]
test_list.append(bluntbody)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 20
flatplate.test_vals = [
-4.680775, 0.781235, -0.135957, 0.022978, 2.8549e-03, 2.3621e+00,
-2.3592e+00
]
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765429, -1.297425, 0.019571, 0.310232]
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase('cylinder_lowmach')
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.850130, -1.388096, -0.056036, 108.140811]
test_list.append(cylinder_lowmach)
# 2D Poiseuille flow (body force driven with periodic inlet / outlet)
poiseuille = TestCase('poiseuille')
poiseuille.cfg_dir = "navierstokes/poiseuille"
poiseuille.cfg_file = "lam_poiseuille.cfg"
poiseuille.test_iter = 10
poiseuille.test_vals = [-5.048282, 0.650814, 0.008714, 13.677678]
test_list.append(poiseuille)
# 2D Poiseuille flow (inlet profile file)
poiseuille_profile = TestCase('poiseuille_profile')
poiseuille_profile.cfg_dir = "navierstokes/poiseuille"
poiseuille_profile.cfg_file = "profile_poiseuille.cfg"
poiseuille_profile.test_iter = 10
poiseuille_profile.test_vals = [-12.494752, -7.712204, -0.000000, 2.085796]
test_list.append(poiseuille_profile)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 20
rae2822_sa.test_vals = [-2.020123, -5.269330, 0.807147, 0.060499]
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 20
rae2822_sst.test_vals = [-0.510635, 4.871104, 0.811904, 0.061614]
test_list.append(rae2822_sst)
# RAE2822 SST_SUST
rae2822_sst_sust = TestCase('rae2822_sst_sust')
rae2822_sst_sust.cfg_dir = "rans/rae2822"
rae2822_sst_sust.cfg_file = "turb_SST_SUST_RAE2822.cfg"
rae2822_sst_sust.test_iter = 20
rae2822_sst_sust.test_vals = [-2.430589, 4.871104, 0.811903, 0.061614]
test_list.append(rae2822_sst_sust)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 20
turb_flatplate.test_vals = [-4.157169, -6.737133, -0.176253, 0.057446]
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.388836, -6.689414, 0.230320, 0.157640]
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [
-8.627052, -10.377936, 1.064491, 0.019710, 20.000000, -1.763095,
20.000000, -4.794176
]
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [
-11.450475, -12.797872, -5.863655, 1.049989, 0.019163, -1.856263
]
test_list.append(turb_naca0012_sst)
# NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst_sust = TestCase('turb_naca0012_sst_sust')
turb_naca0012_sst_sust.cfg_dir = "rans/naca0012"
turb_naca0012_sst_sust.cfg_file = "turb_NACA0012_sst_sust.cfg"
turb_naca0012_sst_sust.test_iter = 10
turb_naca0012_sst_sust.test_vals = [
-11.367051, -12.640670, -5.746919, 1.005233, 0.019017, -1.913905
]
test_list.append(turb_naca0012_sst_sust)
# NACA0012 (SST, fixed values for turbulence quantities)
turb_naca0012_sst_fixedvalues = TestCase('turb_naca0012_sst_fixedvalues')
turb_naca0012_sst_fixedvalues.cfg_dir = "rans/naca0012"
turb_naca0012_sst_fixedvalues.cfg_file = "turb_NACA0012_sst_fixedvalues.cfg"
turb_naca0012_sst_fixedvalues.test_iter = 10
turb_naca0012_sst_fixedvalues.test_vals = [
-5.192502, -9.575898, -1.568269, 1.022571, 0.040527, -2.384329
]
test_list.append(turb_naca0012_sst_fixedvalues)
# NACA0012 (SST, explicit Euler for flow and turbulence equations)
turb_naca0012_sst_expliciteuler = TestCase(
'turb_naca0012_sst_expliciteuler')
turb_naca0012_sst_expliciteuler.cfg_dir = "rans/naca0012"
turb_naca0012_sst_expliciteuler.cfg_file = "turb_NACA0012_sst_expliciteuler.cfg"
turb_naca0012_sst_expliciteuler.test_iter = 10
turb_naca0012_sst_expliciteuler.test_vals = [
-3.532228, -3.157766, 3.364025, 1.124824, 0.501717, -float("inf")
]
test_list.append(turb_naca0012_sst_expliciteuler)
# PROPELLER
propeller = TestCase('propeller')
propeller.cfg_dir = "rans/propeller"
propeller.cfg_file = "propeller.cfg"
propeller.test_iter = 10
propeller.test_vals = [-3.389575, -8.409529, 0.000048, 0.056329]
test_list.append(propeller)
#######################################
### Axisymmetric Compressible RANS ###
#######################################
# Axisymmetric air nozzle (transonic)
axi_rans_air_nozzle = TestCase('axi_rans_air_nozzle')
axi_rans_air_nozzle.cfg_dir = "axisymmetric_rans/air_nozzle"
axi_rans_air_nozzle.cfg_file = "air_nozzle.cfg"
axi_rans_air_nozzle.test_iter = 10
axi_rans_air_nozzle.test_vals = [
-12.093575, -6.630426, -8.798725, -2.399130
]
test_list.append(axi_rans_air_nozzle)
#################################
## Compressible RANS Restart ###
#################################
# NACA0012 SST Multigrid restart
turb_naca0012_sst_restart_mg = TestCase('turb_naca0012_sst_restart_mg')
turb_naca0012_sst_restart_mg.cfg_dir = "rans/naca0012"
turb_naca0012_sst_restart_mg.cfg_file = "turb_NACA0012_sst_multigrid_restart.cfg"
turb_naca0012_sst_restart_mg.test_iter = 20
turb_naca0012_sst_restart_mg.ntest_vals = 5
turb_naca0012_sst_restart_mg.test_vals = [
-7.652987, -7.729472, -1.981061, -0.000015, 0.079061
]
test_list.append(turb_naca0012_sst_restart_mg)
#############################
### Compressibele RANS UQ ###
#############################
# NACA0012 1c
turb_naca0012_1c = TestCase('turb_naca0012_1c')
turb_naca0012_1c.cfg_dir = "rans_uq/naca0012"
turb_naca0012_1c.cfg_file = "turb_NACA0012_uq_1c.cfg"
turb_naca0012_1c.test_iter = 10
turb_naca0012_1c.test_vals = [-4.980749, 1.139261, 0.244644, -0.112857]
test_list.append(turb_naca0012_1c)
# NACA0012 2c
turb_naca0012_2c = TestCase('turb_naca0012_2c')
turb_naca0012_2c.cfg_dir = "rans_uq/naca0012"
turb_naca0012_2c.cfg_file = "turb_NACA0012_uq_2c.cfg"
turb_naca0012_2c.test_iter = 10
turb_naca0012_2c.test_vals = [-5.483337, 0.968887, 0.212057, -0.120310]
test_list.append(turb_naca0012_2c)
# NACA0012 3c
turb_naca0012_3c = TestCase('turb_naca0012_3c')
turb_naca0012_3c.cfg_dir = "rans_uq/naca0012"
turb_naca0012_3c.cfg_file = "turb_NACA0012_uq_3c.cfg"
turb_naca0012_3c.test_iter = 10
turb_naca0012_3c.test_vals = [-5.584300, 0.931383, 0.205113, -0.120892]
test_list.append(turb_naca0012_3c)
# NACA0012 p1c1
turb_naca0012_p1c1 = TestCase('turb_naca0012_p1c1')
turb_naca0012_p1c1.cfg_dir = "rans_uq/naca0012"
turb_naca0012_p1c1.cfg_file = "turb_NACA0012_uq_p1c1.cfg"
turb_naca0012_p1c1.test_iter = 10
turb_naca0012_p1c1.test_vals = [-5.133233, 1.075372, 0.337556, -0.077868]
test_list.append(turb_naca0012_p1c1)
# NACA0012 p1c2
turb_naca0012_p1c2 = TestCase('turb_naca0012_p1c2')
turb_naca0012_p1c2.cfg_dir = "rans_uq/naca0012"
turb_naca0012_p1c2.cfg_file = "turb_NACA0012_uq_p1c2.cfg"
turb_naca0012_p1c2.test_iter = 10
turb_naca0012_p1c2.test_vals = [-5.554619, 0.943693, 0.226386, -0.116553]
test_list.append(turb_naca0012_p1c2)
######################################
### Harmonic Balance ###
######################################
# Description of the regression test
harmonic_balance = TestCase('harmonic_balance')
harmonic_balance.cfg_dir = "harmonic_balance"
harmonic_balance.cfg_file = "HB.cfg"
harmonic_balance.test_iter = 25
harmonic_balance.test_vals = [-1.589740, 3.922578, 0.006703, 0.099632]
harmonic_balance.new_output = False
test_list.append(harmonic_balance)
# Turbulent pitching NACA 64a010 airfoil
hb_rans_preconditioning = TestCase('hb_rans_preconditioning')
hb_rans_preconditioning.cfg_dir = "harmonic_balance/hb_rans_preconditioning"
hb_rans_preconditioning.cfg_file = "davis.cfg"
hb_rans_preconditioning.test_iter = 25
hb_rans_preconditioning.test_vals = [
-1.902111, -5.949288, 0.007768, 0.128060
]
hb_rans_preconditioning.new_output = False
test_list.append(hb_rans_preconditioning)
#############################
### Incompressible Euler ###
#############################
# NACA0012 Hydrofoil
inc_euler_naca0012 = TestCase('inc_euler_naca0012')
inc_euler_naca0012.cfg_dir = "incomp_euler/naca0012"
inc_euler_naca0012.cfg_file = "incomp_NACA0012.cfg"
inc_euler_naca0012.test_iter = 20
inc_euler_naca0012.test_vals = [-4.858287, -3.810487, 0.491850, 0.007002]
inc_euler_naca0012.new_output = True
test_list.append(inc_euler_naca0012)
# C-D nozzle with pressure inlet and mass flow outlet
inc_nozzle = TestCase('inc_nozzle')
inc_nozzle.cfg_dir = "incomp_euler/nozzle"
inc_nozzle.cfg_file = "inv_nozzle.cfg"
inc_nozzle.test_iter = 20
inc_nozzle.test_vals = [-5.971249, -4.910844, -0.000196, 0.121635]
inc_nozzle.new_output = True
test_list.append(inc_nozzle)
#############################
### Incompressible N-S ###
#############################
# Laminar cylinder
inc_lam_cylinder = TestCase('inc_lam_cylinder')
inc_lam_cylinder.cfg_dir = "incomp_navierstokes/cylinder"
inc_lam_cylinder.cfg_file = "incomp_cylinder.cfg"
inc_lam_cylinder.test_iter = 10
inc_lam_cylinder.test_vals = [-4.004277, -3.227956, 0.003851, 7.626583]
inc_lam_cylinder.new_output = True
test_list.append(inc_lam_cylinder)
# Buoyancy-driven cavity
inc_buoyancy = TestCase('inc_buoyancy')
inc_buoyancy.cfg_dir = "incomp_navierstokes/buoyancy_cavity"
inc_buoyancy.cfg_file = "lam_buoyancy_cavity.cfg"
inc_buoyancy.test_iter = 20
inc_buoyancy.test_vals = [-4.432484, 0.507522, 0.000000, 0.000000]
inc_buoyancy.new_output = True
test_list.append(inc_buoyancy)
# Laminar heated cylinder with polynomial fluid model
inc_poly_cylinder = TestCase('inc_poly_cylinder')
inc_poly_cylinder.cfg_dir = "incomp_navierstokes/cylinder"
inc_poly_cylinder.cfg_file = "poly_cylinder.cfg"
inc_poly_cylinder.test_iter = 20
inc_poly_cylinder.test_vals = [-7.851512, -2.093420, 0.029974, 1.921595]
inc_poly_cylinder.new_output = True
test_list.append(inc_poly_cylinder)
# X-coarse laminar bend as a mixed element CGNS test
inc_lam_bend = TestCase('inc_lam_bend')
inc_lam_bend.cfg_dir = "incomp_navierstokes/bend"
inc_lam_bend.cfg_file = "lam_bend.cfg"
inc_lam_bend.test_iter = 10
inc_lam_bend.test_vals = [-3.436191, -3.098014, -0.017338, -0.193981]
test_list.append(inc_lam_bend)
############################
### Incompressible RANS ###
############################
# NACA0012, SA
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.788405, -11.040493, 0.000008, 0.309506]
inc_turb_naca0012.new_output = True
test_list.append(inc_turb_naca0012)
# NACA0012, SST_SUST
inc_turb_naca0012_sst_sust = TestCase('inc_turb_naca0012_sst_sust')
inc_turb_naca0012_sst_sust.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012_sst_sust.cfg_file = "naca0012_SST_SUST.cfg"
inc_turb_naca0012_sst_sust.test_iter = 20
inc_turb_naca0012_sst_sust.test_vals = [
-7.276424, 0.145860, 0.000003, 0.312011
]
test_list.append(inc_turb_naca0012_sst_sust)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.627934, -0.164469, 0.052000, 2.547063]
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-8.001289, -2.607956, 1.501322, 1.488559]
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.162564, 0.066401, 1.399788, 2.220402]
square_cylinder.unsteady = True
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977520, 3.481804, -0.012402, -0.007454]
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.074433, 0.033108, -0.001650, -0.000127]
aeroelastic.unsteady = True
test_list.append(aeroelastic)
# Delayed Detached Eddy Simulation
ddes_flatplate = TestCase('ddes_flatplate')
ddes_flatplate.cfg_dir = "ddes/flatplate"
ddes_flatplate.cfg_file = "ddes_flatplate.cfg"
ddes_flatplate.test_iter = 10
ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783]
ddes_flatplate.unsteady = True
test_list.append(ddes_flatplate)
# unsteady pitching NACA0015, SA
unst_inc_turb_naca0015_sa = TestCase('unst_inc_turb_naca0015_sa')
unst_inc_turb_naca0015_sa.cfg_dir = "unsteady/pitching_naca0015_rans_inc"
unst_inc_turb_naca0015_sa.cfg_file = "config_incomp_turb_sa.cfg"
unst_inc_turb_naca0015_sa.test_iter = 1
unst_inc_turb_naca0015_sa.test_vals = [
-3.008629, -6.888974, 1.435193, 0.433537
]
unst_inc_turb_naca0015_sa.unsteady = True
test_list.append(unst_inc_turb_naca0015_sa)
# unsteady pitching NACA0012, Euler, Deforming
unst_deforming_naca0012 = TestCase('unst_deforming_naca0012')
unst_deforming_naca0012.cfg_dir = "disc_adj_euler/naca0012_pitching_def"
unst_deforming_naca0012.cfg_file = "inv_NACA0012_pitching_deform.cfg"
unst_deforming_naca0012.test_iter = 5
unst_deforming_naca0012.test_vals = [
-3.665120, -3.793643, -3.716518, -3.148310
]
unst_deforming_naca0012.unsteady = True
test_list.append(unst_deforming_naca0012)
######################################
### NICFD ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.040287, 1.124488, -0.000009, 0.000000]
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.401601, 0.738205, -0.000035, 0.000000]
test_list.append(edge_PPR)
######################################
### Turbomachinery ###
######################################
# Jones APU Turbocharger
Jones_tc = TestCase('jones_turbocharger')
Jones_tc.cfg_dir = "turbomachinery/APU_turbocharger"
Jones_tc.cfg_file = "Jones.cfg"
Jones_tc.test_iter = 5
Jones_tc.test_vals = [-5.279930, 0.379651, 72.212100, 1.277439]
Jones_tc.new_output = False
test_list.append(Jones_tc)
# Jones APU Turbocharger restart
Jones_tc_rst = TestCase('jones_turbocharger_restart')
Jones_tc_rst.cfg_dir = "turbomachinery/APU_turbocharger"
Jones_tc_rst.cfg_file = "Jones_rst.cfg"
Jones_tc_rst.test_iter = 5
Jones_tc_rst.test_vals = [-4.625251, -1.568824, 33.995140, 10.181940]
Jones_tc_rst.new_output = False
test_list.append(Jones_tc_rst)
# 2D axial stage
axial_stage2D = TestCase('axial_stage2D')
axial_stage2D.cfg_dir = "turbomachinery/axial_stage_2D"
axial_stage2D.cfg_file = "Axial_stage2D.cfg"
axial_stage2D.test_iter = 20
axial_stage2D.test_vals = [-1.933139, 5.380376, 73.357910, 0.925874]
axial_stage2D.new_output = False
test_list.append(axial_stage2D)
# 2D transonic stator
transonic_stator = TestCase('transonic_stator')
transonic_stator.cfg_dir = "turbomachinery/transonic_stator_2D"
transonic_stator.cfg_file = "transonic_stator.cfg"
transonic_stator.test_iter = 20
transonic_stator.test_vals = [-0.565608, 5.833408, 96.476150, 0.062517]
transonic_stator.new_output = False
test_list.append(transonic_stator)
# 2D transonic stator restart
transonic_stator_rst = TestCase('transonic_stator_restart')
transonic_stator_rst.cfg_dir = "turbomachinery/transonic_stator_2D"
transonic_stator_rst.cfg_file = "transonic_stator_rst.cfg"
transonic_stator_rst.test_iter = 20
transonic_stator_rst.test_vals = [-6.619122, -0.615716, 5.002986, 0.002951]
transonic_stator_rst.new_output = False
test_list.append(transonic_stator_rst)
######################################
### Sliding Mesh ###
######################################
# Uniform flow
uniform_flow = TestCase('uniform_flow')
uniform_flow.cfg_dir = "sliding_interface/uniform_flow"
uniform_flow.cfg_file = "uniform_NN.cfg"
uniform_flow.test_iter = 5
uniform_flow.test_vals = [5.000000, 0.000000, -0.188748, -10.631524]
uniform_flow.unsteady = True
uniform_flow.multizone = True
test_list.append(uniform_flow)
# Channel_2D
channel_2D = TestCase('channel_2D')
channel_2D.cfg_dir = "sliding_interface/channel_2D"
channel_2D.cfg_file = "channel_2D_WA.cfg"
channel_2D.test_iter = 2
channel_2D.test_vals = [2.000000, 0.000000, 0.397972, 0.352756, 0.405398]
channel_2D.unsteady = True
channel_2D.multizone = True
test_list.append(channel_2D)
# Channel_3D
channel_3D = TestCase('channel_3D')
channel_3D.cfg_dir = "sliding_interface/channel_3D"
channel_3D.cfg_file = "channel_3D_WA.cfg"
channel_3D.test_iter = 2
channel_3D.test_vals = [2.000000, 0.000000, 0.620171, 0.505178, 0.415313]
channel_3D.unsteady = True
channel_3D.multizone = True
test_list.append(channel_3D)
# Pipe
pipe = TestCase('pipe')
pipe.cfg_dir = "sliding_interface/pipe"
pipe.cfg_file = "pipe_NN.cfg"
pipe.test_iter = 2
pipe.test_vals = [0.150024, 0.491949, 0.677759, 0.963991, 1.006947]
pipe.unsteady = True
pipe.multizone = True
test_list.append(pipe)
# Rotating cylinders
rotating_cylinders = TestCase('rotating_cylinders')
rotating_cylinders.cfg_dir = "sliding_interface/rotating_cylinders"
rotating_cylinders.cfg_file = "rot_cylinders_WA.cfg"
rotating_cylinders.test_iter = 3
rotating_cylinders.test_vals = [
3.000000, 0.000000, 0.777568, 1.134807, 1.224137
]
rotating_cylinders.unsteady = True
rotating_cylinders.multizone = True
test_list.append(rotating_cylinders)
# Supersonic vortex shedding
supersonic_vortex_shedding = TestCase('supersonic_vortex_shedding')
supersonic_vortex_shedding.cfg_dir = "sliding_interface/supersonic_vortex_shedding"
supersonic_vortex_shedding.cfg_file = "sup_vor_shed_WA.cfg"
supersonic_vortex_shedding.test_iter = 5
supersonic_vortex_shedding.test_vals = [
5.000000, 0.000000, 1.216554, 1.639119
]
supersonic_vortex_shedding.unsteady = True
supersonic_vortex_shedding.multizone = True
test_list.append(supersonic_vortex_shedding)
# Bars_SST_2D
bars_SST_2D = TestCase('bars_SST_2D')
bars_SST_2D.cfg_dir = "sliding_interface/bars_SST_2D"
bars_SST_2D.cfg_file = "bars.cfg"
bars_SST_2D.test_iter = 13
bars_SST_2D.test_vals = [13.000000, -0.619686, -1.564595]
bars_SST_2D.multizone = True
test_list.append(bars_SST_2D)
# Sliding mesh with incompressible flows (steady)
slinc_steady = TestCase('slinc_steady')
slinc_steady.cfg_dir = "sliding_interface/incompressible_steady"
slinc_steady.cfg_file = "config.cfg"
slinc_steady.test_iter = 19
slinc_steady.test_vals = [19.000000, -1.800401, -2.114687]
slinc_steady.multizone = True
test_list.append(slinc_steady)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase('statbeam3d')
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-2.378370, -1.585252, -2.028505, 64359.000000]
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase('dynbeam2d')
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-3.240015, 2.895057, -0.353146, 66127.000000]
dynbeam2d.unsteady = True
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase('fsi2d')
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [4.000000, 0.000000, -3.743227, -4.133479]
fsi2d.multizone = True
fsi2d.unsteady = True
test_list.append(fsi2d)
# FSI, Static, 2D, new mesh solver
stat_fsi = TestCase('stat_fsi')
stat_fsi.cfg_dir = "fea_fsi/stat_fsi"
stat_fsi.cfg_file = "config.cfg"
stat_fsi.test_iter = 7
stat_fsi.test_vals = [-5.403596, -5.722583, 0.000000, 10.000000]
stat_fsi.multizone = True
test_list.append(stat_fsi)
# FSI, Dynamic, 2D, new mesh solver
dyn_fsi = TestCase('dyn_fsi')
dyn_fsi.cfg_dir = "fea_fsi/dyn_fsi"
dyn_fsi.cfg_file = "config.cfg"
dyn_fsi.test_iter = 4
dyn_fsi.test_vals = [-4.355806, -4.060582, 0.000000, 102.000000]
dyn_fsi.multizone = True
dyn_fsi.unsteady = True
test_list.append(dyn_fsi)
# FSI, Static, 2D, new mesh solver, restart
stat_fsi_restart = TestCase('stat_fsi_restart')
stat_fsi_restart.cfg_dir = "fea_fsi/stat_fsi"
stat_fsi_restart.cfg_file = "config_restart.cfg"
stat_fsi_restart.test_iter = 1
stat_fsi_restart.test_vals = [-3.474082, -4.242343, 0.000000, 37.000000]
stat_fsi_restart.multizone = True
test_list.append(stat_fsi_restart)
##############################################
### Method of Manufactured Solutions (MMS) ###
##############################################
# FVM, compressible, laminar N-S
mms_fvm_ns = TestCase('mms_fvm_ns')
mms_fvm_ns.cfg_dir = "mms/fvm_navierstokes"
mms_fvm_ns.cfg_file = "lam_mms_roe.cfg"
mms_fvm_ns.test_iter = 20
mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000]
test_list.append(mms_fvm_ns)
# FVM, incompressible, euler
mms_fvm_inc_euler = TestCase('mms_fvm_inc_euler')
mms_fvm_inc_euler.cfg_dir = "mms/fvm_incomp_euler"
mms_fvm_inc_euler.cfg_file = "inv_mms_jst.cfg"
mms_fvm_inc_euler.test_iter = 20
mms_fvm_inc_euler.test_vals = [-9.128033, -9.441406, 0.000000, 0.000000]
test_list.append(mms_fvm_inc_euler)
# FVM, incompressible, laminar N-S
mms_fvm_inc_ns = TestCase('mms_fvm_inc_ns')
mms_fvm_inc_ns.cfg_dir = "mms/fvm_incomp_navierstokes"
mms_fvm_inc_ns.cfg_file = "lam_mms_fds.cfg"
mms_fvm_inc_ns.test_iter = 20
mms_fvm_inc_ns.test_vals = [-7.414944, -7.631546, 0.000000, 0.000000]
test_list.append(mms_fvm_inc_ns)
######################################
### RUN TESTS ###
######################################
for test in test_list:
test.su2_exec = "SU2_CFD -t 2"
test.timeout = 600
test.tol = 1e-4
#end
pass_list = [test.run_test() for test in test_list]
# Tests summary
print('==================================================================')
print('Summary of the hybrid parallel tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s' % test.tag)
else:
print('* FAILED - %s' % test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git pull')
# Build SU2_CFD in parallel using autoconf
os.system('./configure --prefix=$SU2_HOME --with-MPI=mpicxx CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.975507,2.405636,-0.027947,0.070672 ]
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-5.868897,-5.317999,0.335382,0.022264]
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.810772,3.816000,-0.252360,0.044433]
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.722014,-4.159420,0.277228,0.018788]
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.236893,0.247033,-0.163494,0.013566]
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.414640,-0.949884,0.028066,-5.963428]
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-2.750473,-5.507654,0.871049,0.023362] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.166409,4.131494,0.872131,0.023509] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-4.965682,-7.366012,-0.185201,0.015640] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327518,-6.563377,0.230436,0.155816] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.826348,-7.364208,-0.000065,0.803130] #last 4 columns
turb_naca0012.su2_exec = "parallel_computation.py -f"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709964,-11.007318,0.000012,0.211084] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-12.164200,-16.000000,0.005483,0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.369284,-6.550741,-0.000023,0.147730] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-0.586744,-6.051059,-0.032305,25.115000 ] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-4.234330,-9.705736,0.005161,0.398940] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.810435,-6.920519,0.014614,1.020100] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-4.351102,-8.919996,-1.275200,-2.541400] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-2.912541,-8.134391,4.544600,0.105850] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [-6.182255,-6.058331,0.010905,0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-2.381271,-2.874257,-0.048372,0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
# RAM-C II Sphere-Cone -- 61km Altitude
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119,2.854417,-4.439628,0.000188]
ramc.su2_exec = "parallel_computation.py -f"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.439958,0.023984,-0.065783,-12.173188]
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.654688,-1.195462,6.682924,0.987516]
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.542162,0.048674,1.398952,2.196894]
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606963,-9.034619,-3.3385e-07,1.8777e-01] #last 4 columns
discadj_naca0012.su2_exec = "parallel_computation.py -f"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-1.751997, 0.485368, 0.182890, -0.383510] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-1.655243, -0.507187, 0.129010, -0.4776800] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
# Tests summary
print '=================================================================='
print 'Summary of the parallel tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s'%test.tag
else:
print '* FAILED - %s'%test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ[
'SU2_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2'
os.environ[
'SU2_RUN'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir(os.environ['SU2_HOME'])
os.system('git pull')
# Build SU2_CFD in serial using autoconf
os.system('./configure --prefix=$SU2_HOME CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.991375, 2.388702, -0.042177, 0.068520]
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-5.932646, -5.394328, 0.335205, 0.022232]
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.838548, 3.781222, -0.252690, 0.044489]
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.744759, -4.182702, 0.281122, 0.018310]
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.230001, 0.252184, -0.163706, 0.013547]
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.409812, -0.945306, 0.088160, -5.192708]
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-2.729166, -5.506935, 0.860798,
0.023704] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.151533, 4.144621, 0.861331,
0.023855] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.021253, -7.365210, -0.185394,
0.015273] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327517, -6.563378, 0.230436,
0.155816] #last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.826334, -7.364207, -0.000025,
0.803037] #last 4 columns
turb_naca0012.su2_exec = "SU2_CFD"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709986, -11.007545, 0.000008,
0.210347] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-12.214678, -16.000000, 0.005483,
0.536870] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.370788, -6.545955, -0.000023,
0.147730] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [
-0.597482, -6.063713, -0.032305, 25.115000
] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [
-4.234330, -9.705736, 0.005161, 0.398940
] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [
-1.810435, -6.920519, 0.014614, 1.020100
] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [
-4.351102, -8.919996, -1.275200, -2.541400
] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [
-2.888858, -8.085710, 4.545700, 0.109650
] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [
-6.049647, -6.004696, 0.010909, 0.000000
] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [
-2.352353, -2.851967, -0.048345, 0.000000
] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119, 2.854417, -4.439628, 0.000188]
ramc.su2_exec = "SU2_CFD"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.545249, -0.083220, -0.007449, -14.207933]
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.743171, -1.295111, 6.846763, 0.823335]
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.542160, 0.048661, 1.398952, 2.196894]
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### Real_Gas ###
######################################
# Supersonic_turbine
supersonic_turbine = TestCase('supersonic_turbine')
supersonic_turbine.cfg_dir = "real_gas/euler/supersonic_turbine"
supersonic_turbine.cfg_file = "supersonic.cfg"
supersonic_turbine.test_iter = 19
supersonic_turbine.test_vals = [-0.249215, 5.701822, 0.000000, 0.000000]
supersonic_turbine.su2_exec = "SU2_CFD"
supersonic_turbine.timeout = 1600
supersonic_turbine.tol = 0.00001
test_list.append(square_cylinder)
# Supersonic_turbine
supersonic_nozzle = TestCase('supersonic_nozzle')
supersonic_nozzle.cfg_dir = "real_gas/euler/2Dnozzle"
supersonic_nozzle.cfg_file = "nozzle_MDM_shockwave.cfg"
supersonic_nozzle.test_iter = 559
supersonic_nozzle.test_vals = [-0.371019, 4.755257, 0.000000, 0.000000]
supersonic_nozzle.su2_exec = "SU2_CFD"
supersonic_nozzle.timeout = 1600
supersonic_nozzle.tol = 0.00001
test_list.append(square_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.559002, -8.926022, -0.000000, 0.005588] #last 4 columns
discadj_naca0012.su2_exec = "parallel_computation.py -f"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.724803, -3.838647, 0.000000, 0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "parallel_computation.py -f"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
# Arina nozzle 2D
discadj_arina2k = TestCase('discadj_arina2k')
discadj_arina2k.cfg_dir = "disc_adj_euler/arina2k"
discadj_arina2k.cfg_file = "Arina2KRS.cfg"
discadj_arina2k.test_iter = 20
discadj_arina2k.test_vals = [2.438813, 1.976484, 47258.000000, 0.000000] #last 4 columns
discadj_arina2k.su2_exec = "parallel_computation.py -f"
discadj_arina2k.timeout = 8400
discadj_arina2k.tol = 0.00001
test_list.append(discadj_arina2k)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-2.230578, 0.678810, 0.181780, -0.000018] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-2.223209, -0.496681, 0.154390, -0.000022] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "disc_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [20.000000, -3.566362, -2.541739, 0.000000] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder (Heated)
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "disc_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "heated_cylinder.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [20.000000, -2.188743, -2.068616, 0.000000] #last 4 columns
discadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012 SA
discadj_incomp_turb_NACA0012_sa = TestCase('discadj_incomp_turb_NACA0012_sa')
discadj_incomp_turb_NACA0012_sa.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sa.cfg_file = "turb_naca0012_sa.cfg"
discadj_incomp_turb_NACA0012_sa.test_iter = 10
discadj_incomp_turb_NACA0012_sa.test_vals = [10.000000, -3.846036, -1.031071, 0.000000] #last 4 columns
discadj_incomp_turb_NACA0012_sa.su2_exec = "parallel_computation.py -f"
discadj_incomp_turb_NACA0012_sa.timeout = 1600
discadj_incomp_turb_NACA0012_sa.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sa)
# Adjoint Incompressible Turbulent NACA 0012 SST
discadj_incomp_turb_NACA0012_sst = TestCase('discadj_incomp_turb_NACA0012_sst')
discadj_incomp_turb_NACA0012_sst.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sst.cfg_file = "turb_naca0012_sst.cfg"
discadj_incomp_turb_NACA0012_sst.test_iter = 10
discadj_incomp_turb_NACA0012_sst.test_vals = [-3.845625, -2.413047, -8.419973, 0.000000] #last 4 columns
discadj_incomp_turb_NACA0012_sst.su2_exec = "parallel_computation.py -f"
discadj_incomp_turb_NACA0012_sst.timeout = 1600
discadj_incomp_turb_NACA0012_sst.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746900, -1.544893, -8.3447e-03, 1.3808e-05] #last 4 columns
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##########################################################################
### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order ###
##########################################################################
# Turbulent Cylinder
discadj_DT_1ST_cylinder = TestCase('unsteady_cylinder_DT_1ST')
discadj_DT_1ST_cylinder.cfg_dir = "disc_adj_rans/cylinder_DT_1ST"
discadj_DT_1ST_cylinder.cfg_file = "cylinder.cfg"
discadj_DT_1ST_cylinder.test_iter = 9
discadj_DT_1ST_cylinder.test_vals = [3.698165, -1.607052, -2.2503e-03, 2.7212e-05] #last 4 columns
discadj_DT_1ST_cylinder.su2_exec = "parallel_computation.py -f"
discadj_DT_1ST_cylinder.timeout = 1600
discadj_DT_1ST_cylinder.tol = 0.00001
discadj_DT_1ST_cylinder.unsteady = True
test_list.append(discadj_DT_1ST_cylinder)
######################################################
### Unsteady Disc. adj. compressible pitching NACA ###
######################################################
# compressible pitching NACA0012
discadj_pitchingNACA0012 = TestCase('pitchingNACA0012')
discadj_pitchingNACA0012.cfg_dir = "disc_adj_euler/naca0012_pitching"
discadj_pitchingNACA0012.cfg_file = "inv_NACA0012_pitching.cfg"
discadj_pitchingNACA0012.test_iter = 4
discadj_pitchingNACA0012.test_vals = [-1.091129, -1.545863, -0.037418, 0.000108] #last 4 columns
discadj_pitchingNACA0012.su2_exec = "parallel_computation.py -f"
discadj_pitchingNACA0012.timeout = 1600
discadj_pitchingNACA0012.tol = 0.00001
discadj_pitchingNACA0012.unsteady = True
test_list.append(discadj_pitchingNACA0012)
#######################################################
### Disc. adj. turbomachinery ###
#######################################################
# Transonic Stator 2D
discadj_trans_stator = TestCase('transonic_stator')
discadj_trans_stator.cfg_dir = "disc_adj_turbomachinery/transonic_stator_2D"
discadj_trans_stator.cfg_file = "transonic_stator.cfg"
discadj_trans_stator.test_iter = 79
discadj_trans_stator.test_vals = [79.000000, -1.927296, -1.401205] #last 4 columns
discadj_trans_stator.su2_exec = "parallel_computation.py -f"
discadj_trans_stator.timeout = 1600
discadj_trans_stator.tol = 0.00001
test_list.append(discadj_trans_stator)
###################################
### Structural Adjoint ###
###################################
# Structural model
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 9
discadj_fea.test_vals = [-6.492475, -6.401201, -0.000364, -8.708700] #last 4 columns
discadj_fea.su2_exec = "parallel_computation.py -f"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Disc. adj. heat ###
###################################
# Discrete adjoint for heated cylinder
discadj_heat = TestCase('discadj_heat')
discadj_heat.cfg_dir = "disc_adj_heat"
discadj_heat.cfg_file = "disc_adj_heat.cfg"
discadj_heat.test_iter = 10
discadj_heat.test_vals = [-2.281765, 0.706808, -0.743990, -6.866000] #last 4 columns
discadj_heat.su2_exec = "parallel_computation.py -f"
discadj_heat.timeout = 1600
discadj_heat.tol = 0.00001
test_list.append(discadj_heat)
###################################
### Coupled FSI Adjoint ###
###################################
# Legacy driver
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "config.cfg"
discadj_fsi.test_iter = 3000
discadj_fsi.test_vals = [0.958848,-0.157601,2.726147,1.798362] #last 4 columns
discadj_fsi.su2_exec = "mpirun -n 2 SU2_CFD_AD"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
# Multi physics framework
discadj_fsi2 = TestCase('discadj_fsi_airfoil')
discadj_fsi2.cfg_dir = "disc_adj_fsi/Airfoil_2d"
discadj_fsi2.cfg_file = "config.cfg"
discadj_fsi2.test_iter = 8
discadj_fsi2.test_vals = [-5.070991, -2.5239e-13] #last 2 columns
discadj_fsi2.su2_exec = "mpirun -n 2 SU2_CFD_AD"
discadj_fsi2.timeout = 1600
discadj_fsi2.tol = 1e-16
test_list.append(discadj_fsi2)
###################################
### Coupled CHT Adjoint ###
###################################
# Coupled discrete adjoint for heatflux in heated cylinder array
discadj_cht = TestCase('discadj_cht')
discadj_cht.cfg_dir = "coupled_cht/disc_adj_incomp_2d"
discadj_cht.cfg_file = "cht_2d_3cylinders.cfg"
discadj_cht.test_iter = 10
discadj_cht.test_vals = [-2.381654, -3.099873, -3.099844, -3.099841] #last 4 columns
discadj_cht.su2_exec = "parallel_computation.py -f"
discadj_cht.timeout = 1600
discadj_cht.tol = 0.00001
test_list.append(discadj_cht)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
##################################################
### Structural Adjoint - Topology Optimization ###
##################################################
# test discrete_adjoint.py
discadj_topol_optim = TestCase('discadj_topol_optim')
discadj_topol_optim.cfg_dir = "fea_topology"
discadj_topol_optim.cfg_file = "config.cfg"
discadj_topol_optim.test_iter = 0
discadj_topol_optim.su2_exec = "parallel_computation.py -f"
discadj_topol_optim.timeout = 1600
discadj_topol_optim.reference_file = "grad_ref_node.dat.ref"
discadj_topol_optim.test_file = "grad_ref_node.dat"
pass_list.append(discadj_topol_optim.run_filediff())
test_list.append(discadj_topol_optim)
# Tests summary
print('==================================================================')
print('Summary of the parallel tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s'%test.tag)
else:
print('* FAILED - %s'%test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['TEST_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work'
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync Test Cases repo
os.chdir( os.environ['TEST_HOME'] )
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# Build SU2_CFD in serial using autoconf
os.system('./configure --prefix=$SU2_HOME CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.110240, 2.263506, 0.008686, 0.029098] #last 4 columns
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.191618, -5.592802, 0.334809, 0.022197] #last 4 columns
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.711318, 3.913749, -0.252131, 0.044402] #last 4 columns
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.704347, -4.159916, 0.271678, 0.018869] #last 4 columns
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231916, 0.261866, -0.166832, 0.012717] #last 4 columns
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765426, -1.297422, 0.019496, 0.310082] #last 4 columns
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.442524, -5.441383, 0.884279, 0.024730] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.185243, 4.018464, 0.886786, 0.024927] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.069447, -7.354601, -0.187187, 0.010831] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438, 0.155815]#last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 20
turb_naca0012_sa.test_vals = [-6.607227, -9.778334, 1.098508, 0.012417] #last 4 columns
turb_naca0012_sa.su2_exec = "SU2_CFD"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 20
turb_naca0012_sst.test_vals = [-8.290782, -1.743121, 1.084189, 0.012583] #last 4 columns
turb_naca0012_sst.su2_exec = "SU2_CFD"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710052, -11.007500, -0.000001, 0.210445] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.787555, -15.192503, 0.300920, 0.536870] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.009929, -6.251311, -0.106940, 0.149230] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.677184, -9.141850, -2.056700, 4.497000] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.229160] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.620880] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, -19.169000, -2.994100] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.377843, -10.882446, -0.212470, 0.269390] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.980272, -12.146779, 1.9399, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718622, -7.027366, -2.932100, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.643029, 2.849441, -4.443852, 0.000313] #last 4 columns
ramc.su2_exec = "SU2_CFD"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.627934, -0.164470, 0.051972, 2.547034] #last 4 columns
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.709662, -2.274900, 1.418422, 1.734206] #last 4 columns
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.544603, 0.048578, 1.398951, 2.196894] #last 4 columns
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### Real_Gas ###
######################################
# ls89_sa
ls89_sa = TestCase('ls89_sa')
ls89_sa.cfg_dir = "nicf/LS89"
ls89_sa.cfg_file = "turb_SA_PR.cfg"
ls89_sa.test_iter = 100
ls89_sa.test_vals = [-6.383111, -13.350395, 0.069071, 0.160893] #last 4 columns
ls89_sa.su2_exec = "SU2_CFD"
ls89_sa.timeout = 1600
ls89_sa.tol = 0.00001
test_list.append(ls89_sa)
# # ls89_sst
# ls89_sst = TestCase('ls89_sst')
# ls89_sst.cfg_dir = "nicf/LS89"
# ls89_sst.cfg_file = "turb_SST_PR.cfg"
# ls89_sst.test_iter = 100
# ls89_sst.test_vals = [-8.548266, -1.449437, 0.067986, 0.151168] #last 4 columns
# ls89_sst.su2_exec = "SU2_CFD"
# ls89_sst.timeout = 1600
# ls89_sst.tol = 0.00001
# test_list.append(ls89_sst)
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-1.448271, 4.749156, -0.000046, 0.000000] #last 4 columns
edge_VW.su2_exec = "SU2_CFD"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-1.998238, 4.172451, -0.000056, 0.000000] #last 4 columns
edge_PPR.su2_exec = "SU2_CFD"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.071007, 2.301191, 0.008562, 0.028922] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.690232, 3.924432, -0.252221, 0.044419] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.400678, -12.932056, 0.282557, 0.012706] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231727, 0.261637, -0.166869, 0.012707] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948, 0.625438] #last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase('cylinder_lowmach')
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.861860, -1.399846, -1.557250, 110.230719] #last 4 columns
cylinder_lowmach.su2_exec = "parallel_computation.py -f"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.647743, -5.442583, 0.903159, 0.025800] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.198777, 4.013989, 0.904265, 0.025941] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.071289, -7.366446, -0.187145, 0.010957] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438, 0.155815] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000764, -9.145363, 1.070528, 0.019417] #last 4 columns
turb_naca0012_sa.su2_exec = "parallel_computation.py -f"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039645, -7.220177, 1.059622, 0.019138] #last 4 columns
turb_naca0012_sst.su2_exec = "parallel_computation.py -f"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710048, -11.007498, 0.000002, 0.210441] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.783712, -15.192812, 0.300920, 0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.131587, -12.703243, 0.685900, 0.140920] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
# Inviscid WEDGE: generalized adjoint and custom DV
contadj_wedge = TestCase('contadj_wedge')
contadj_wedge.cfg_dir = "cont_adj_euler/wedge"
contadj_wedge.cfg_file = "inv_wedge_ROE.cfg"
contadj_wedge.test_iter = 10
contadj_wedge.test_vals = [2.780403, -3.223266, -1448300.000000, -0.000004] #last 4 columns
contadj_wedge.su2_exec = "parallel_computation.py -f"
contadj_wedge.timeout = 1600
contadj_wedge.tol = 0.00001
test_list.append(contadj_wedge)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.659040, -9.117773, 2.056700, 4.497000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.229160] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.620880] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, 19.169000, -2.994100] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.380929, -10.886092, -0.212470, 0.269390] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.968536, -12.133235, 1.939900, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718840, -7.012324, 2.932100, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.597018, -0.133158, 0.169034, 0.821371] #last 4 columns
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.648320, -2.202753, 1.236836, 1.609040] #last 4 columns
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.166422,0.076751,1.398549,2.197047] #last 4 columns
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
square_cylinder.unsteady = True
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.014552, -0.004969] #last 4 columns
sine_gust.su2_exec = "parallel_computation.py -f"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077169, 0.036452, -0.001685, -0.000113] #last 4 columns
aeroelastic.su2_exec = "parallel_computation.py -f"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.058481, 1.115321, -0.000009, 0.000000] #last 4 columns
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.486409, 0.654417, -0.000037, 0.000000] #last 4 columns
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase('statbeam3d')
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-8.520066, -8.069308, -8.062384, 64095.000000] #last 4 columns
statbeam3d.su2_exec = "parallel_computation_fsi.py -f"
statbeam3d.timeout = 1600
statbeam3d.tol = 0.00001
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase('dynbeam2d')
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-9.420641, -5.365871, -12.430382, 6.5210e+04] #last 4 columns
dynbeam2d.su2_exec = "parallel_computation_fsi.py -f"
dynbeam2d.timeout = 1600
dynbeam2d.tol = 0.00001
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase('fsi2d')
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI_2D.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [2.000000, 0.500000, -7.777910, -1.139830] #last 4 columns
fsi2d.su2_exec = "parallel_computation_fsi.py -f"
fsi2d.timeout = 1600
fsi2d.tol = 0.00001
test_list.append(fsi2d)
##########################
### Python wrapper ###
##########################
# NACA0012
pywrapper_naca0012 = TestCase('pywrapper_naca0012')
pywrapper_naca0012.cfg_dir = "euler/naca0012"
pywrapper_naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
pywrapper_naca0012.test_iter = 100
pywrapper_naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
pywrapper_naca0012.su2_exec = "mpirun -np 2 pyWrap_SU2_CFD.py -f"
pywrapper_naca0012.timeout = 1600
pywrapper_naca0012.tol = 0.00001
test_list.append(pywrapper_naca0012)
# NACA0012 (SST, FUN3D results for finest grid: CL=1.0840, CD=0.01253)
pywrapper_turb_naca0012_sst = TestCase('pywrapper_turb_naca0012_sst')
pywrapper_turb_naca0012_sst.cfg_dir = "rans/naca0012"
pywrapper_turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
pywrapper_turb_naca0012_sst.test_iter = 10
pywrapper_turb_naca0012_sst.test_vals = [-15.039645, -7.220177, 1.059622, 0.019138] #last 4 columns
pywrapper_turb_naca0012_sst.su2_exec = "mpirun -np 2 pyWrap_SU2_CFD.py -f"
pywrapper_turb_naca0012_sst.timeout = 3200
pywrapper_turb_naca0012_sst.tol = 0.00001
test_list.append(pywrapper_turb_naca0012_sst)
# Square cylinder
pywrapper_square_cylinder = TestCase('pywrapper_square_cylinder')
pywrapper_square_cylinder.cfg_dir = "unsteady/square_cylinder"
pywrapper_square_cylinder.cfg_file = "turb_square.cfg"
pywrapper_square_cylinder.test_iter = 3
pywrapper_square_cylinder.test_vals = [-1.166422,0.076751,1.398549,2.197047] #last 4 columns
pywrapper_square_cylinder.su2_exec = "mpirun -np 2 pyWrap_SU2_CFD.py -f"
pywrapper_square_cylinder.timeout = 1600
pywrapper_square_cylinder.tol = 0.00001
pywrapper_square_cylinder.unsteady = True
test_list.append(pywrapper_square_cylinder)
# Aeroelastic
pywrapper_aeroelastic = TestCase('pywrapper_aeroelastic')
pywrapper_aeroelastic.cfg_dir = "aeroelastic"
pywrapper_aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
pywrapper_aeroelastic.test_iter = 2
pywrapper_aeroelastic.test_vals = [0.077169, 0.036452, -0.001685, -0.000113] #last 4 columns
pywrapper_aeroelastic.su2_exec = "mpirun -np 2 pyWrap_SU2_CFD.py -f"
pywrapper_aeroelastic.timeout = 1600
pywrapper_aeroelastic.tol = 0.000001
pywrapper_aeroelastic.unsteady = True
test_list.append(pywrapper_aeroelastic)
# FSI, 2d
pywrapper_fsi2d = TestCase('pywrapper_fsi2d')
pywrapper_fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
pywrapper_fsi2d.cfg_file = "configFSI_2D.cfg"
pywrapper_fsi2d.test_iter = 4
pywrapper_fsi2d.test_vals = [2.000000, 0.500000, -7.777910, -1.139830] #last 4 columns
pywrapper_fsi2d.su2_exec = "mpirun -np 2 pyWrap_SU2_CFD.py --nZone 2 --fsi True -f"
pywrapper_fsi2d.timeout = 1600
pywrapper_fsi2d.tol = 0.00001
test_list.append(pywrapper_fsi2d)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
######################################
### RUN SU2_DEF TESTS ###
######################################
# Inviscid NACA0012 (triangles)
naca0012_def = TestCase('naca0012_def')
naca0012_def.cfg_dir = "deformation/naca0012"
naca0012_def.cfg_file = "def_NACA0012.cfg"
naca0012_def.test_iter = 250
naca0012_def.test_vals = [5.44754e-15] #residual
naca0012_def.su2_exec = "mpirun -n 2 SU2_DEF"
naca0012_def.timeout = 1600
naca0012_def.tol = 1e-15
pass_list.append(naca0012_def.run_def())
test_list.append(naca0012_def)
# RAE2822 (mixed tris + quads)
rae2822_def = TestCase('rae2822_def')
rae2822_def.cfg_dir = "deformation/rae2822"
rae2822_def.cfg_file = "def_RAE2822.cfg"
rae2822_def.test_iter = 150
rae2822_def.test_vals = [1.47076e-15] #residual
rae2822_def.su2_exec = "mpirun -n 2 SU2_DEF"
rae2822_def.timeout = 1600
rae2822_def.tol = 1e-16
pass_list.append(rae2822_def.run_def())
test_list.append(rae2822_def)
# Turb NACA4412 (quads, wall distance)
naca4412_def = TestCase('naca4412_def')
naca4412_def.cfg_dir = "deformation/naca4412"
naca4412_def.cfg_file = "def_NACA4412.cfg"
naca4412_def.test_iter = 300
naca4412_def.test_vals = [4.46129e-15] #residual
naca4412_def.su2_exec = "mpirun -n 2 SU2_DEF"
naca4412_def.timeout = 1600
naca4412_def.tol = 1e-15
pass_list.append(naca4412_def.run_def())
test_list.append(naca4412_def)
# Brick of tets (inverse volume)
brick_tets_def = TestCase('brick_tets_def')
brick_tets_def.cfg_dir = "deformation/brick_tets"
brick_tets_def.cfg_file = "def_brick_tets.cfg"
brick_tets_def.test_iter = 1000
brick_tets_def.test_vals = [9.35558e-16] #residual
brick_tets_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_tets_def.timeout = 1600
brick_tets_def.tol = 1e-15
pass_list.append(brick_tets_def.run_def())
test_list.append(brick_tets_def)
# Brick of isotropic hexas (inverse volume)
brick_hex_def = TestCase('brick_hex_def')
brick_hex_def.cfg_dir = "deformation/brick_hex"
brick_hex_def.cfg_file = "def_brick_hex.cfg"
brick_hex_def.test_iter = 1000
brick_hex_def.test_vals = [1.46423e-15] #residual
brick_hex_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_hex_def.timeout = 1600
brick_hex_def.tol = 1e-15
pass_list.append(brick_hex_def.run_def())
test_list.append(brick_hex_def)
# Brick with a pyramid layer (inverse volume)
brick_pyra_def = TestCase('brick_pyra_def')
brick_pyra_def.cfg_dir = "deformation/brick_pyra"
brick_pyra_def.cfg_file = "def_brick_pyra.cfg"
brick_pyra_def.test_iter = 100
brick_pyra_def.test_vals = [5.97202e-15] #residual
brick_pyra_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_pyra_def.timeout = 1600
brick_pyra_def.tol = 1e-15
pass_list.append(brick_pyra_def.run_def())
test_list.append(brick_pyra_def)
# Brick of isotropic prisms (inverse volume)
brick_prism_def = TestCase('brick_prism_def')
brick_prism_def.cfg_dir = "deformation/brick_prism"
brick_prism_def.cfg_file = "def_brick_prism.cfg"
brick_prism_def.test_iter = 100
brick_prism_def.test_vals = [2.80867e-14] #residual
brick_prism_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_prism_def.timeout = 1600
brick_prism_def.tol = 1e-15
pass_list.append(brick_prism_def.run_def())
test_list.append(brick_prism_def)
# Brick of prisms with high aspect ratio cells near the wall (wall distance)
brick_prism_rans_def = TestCase('brick_prism_rans_def')
brick_prism_rans_def.cfg_dir = "deformation/brick_prism_rans"
brick_prism_rans_def.cfg_file = "def_brick_prism_rans.cfg"
brick_prism_rans_def.test_iter = 50
brick_prism_rans_def.test_vals = [3.5265e-15] #residual
brick_prism_rans_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_prism_rans_def.timeout = 1600
brick_prism_rans_def.tol = 1e-15
pass_list.append(brick_prism_rans_def.run_def())
test_list.append(brick_prism_rans_def)
# Brick of hexas with high aspect ratio cells near the wall (inverse volume)
brick_hex_rans_def = TestCase('brick_hex_rans_def')
brick_hex_rans_def.cfg_dir = "deformation/brick_hex_rans"
brick_hex_rans_def.cfg_file = "def_brick_hex_rans.cfg"
brick_hex_rans_def.test_iter = 600
brick_hex_rans_def.test_vals = [2.75292e-14] #residual
brick_hex_rans_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_hex_rans_def.timeout = 1600
brick_hex_rans_def.tol = 1e-16
pass_list.append(brick_hex_rans_def.run_def())
test_list.append(brick_hex_rans_def)
######################################
### RUN EXTERNAL FSI COUPLING TEST ###
######################################
# Pitch-plunge NACA 0012 (external FSI coupling)
coupled_FSI = TestCase('coupled_FSI')
coupled_FSI.cfg_dir = "coupled_fsi/2d_aeroelasticity"
coupled_FSI.cfg_file = "FSICoupler_config.cfg"
coupled_FSI.test_iter = 1
coupled_FSI.su2_exec = "mpirun -np 2 fsi_computation.py"
coupled_FSI.timeout = 1600
coupled_FSI.reference_file = "StructHistory.dat.ref_parallel"
coupled_FSI.test_file = "StructHistory.dat"
pass_list.append(coupled_FSI.run_filediff())
test_list.append(coupled_FSI)
# Tests summary
print '=================================================================='
print 'Summary of the parallel tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s'%test.tag
else:
print '* FAILED - %s'%test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606839,-9.035212,-3.3386e-07,1.8777e-01] #last 4 columns
discadj_naca0012.su2_exec = "SU2_CFD_AD"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
#######################################################
### Disc. adj. compressible RANS ###
#######################################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-1.751947, 0.485758, 0.181440, -0.385110] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-1.658566, -0.487694, 0.087556, -0.537010] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 10
discadj_cylinder.test_vals = [3.522068,-1.787841,-1.2030e-02,1.1156e-03] #last 4 columns
discadj_cylinder.su2_exec = "SU2_CFD_AD"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
######################################
### RUN PYTHON TESTS ###
######################################
# test discrete_adjoint.py
discadj_euler_py = TestCase('discadj_euler_py')
discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
discadj_euler_py.cfg_file = "inv_NACA0012.cfg"
discadj_euler_py.test_iter = 10
discadj_euler_py.su2_exec = "discrete_adjoint.py"
discadj_euler_py.timeout = 1600
discadj_euler_py.reference_file = "of_grad_cd_disc.dat.ref"
discadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_euler_py.run_filediff())
test_list.append(discadj_euler_py)
# test direct_differentiation.py
directdiff_euler_py = TestCase('directdiff_euler_py')
directdiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
directdiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
directdiff_euler_py.test_iter = 10
directdiff_euler_py.su2_exec = "direct_differentiation.py"
directdiff_euler_py.timeout = 1600
directdiff_euler_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_euler_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_euler_py.run_filediff())
test_list.append(directdiff_euler_py)
# Tests summary
print '=================================================================='
print 'Summary of the serial tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s'%test.tag
else:
print '* FAILED - %s'%test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.071007, 2.301191, 0.008562, 0.028922] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.690232, 3.924432, -0.252221, 0.044419] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.400678, -12.932056, 0.282557, 0.012706] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
# Fixed CL NACA0012
fixedCL_naca0012 = TestCase('fixedcl_naca0012')
fixedCL_naca0012.cfg_dir = "fixed_cl/naca0012"
fixedCL_naca0012.cfg_file = "inv_NACA0012.cfg"
fixedCL_naca0012.test_iter = 500
fixedCL_naca0012.test_vals = [-5.930145,-0.546310,0.300089,0.019393] #last 4 columns
fixedCL_naca0012.su2_exec = "parallel_computation.py -f"
fixedCL_naca0012.timeout = 1600
fixedCL_naca0012.tol = 0.00001
test_list.append(fixedCL_naca0012)
# Polar sweep of the inviscid NACA0012
polar_naca0012 = TestCase('polar_naca0012')
polar_naca0012.cfg_dir = "polar/naca0012"
polar_naca0012.cfg_file = "inv_NACA0012.cfg"
polar_naca0012.polar = True
polar_naca0012.test_iter = 10
polar_naca0012.test_vals = [-1.298373, 4.139860, 0.010703, 0.008932] #last 4 columns
polar_naca0012.su2_exec = "compute_polar.py -i 11"
polar_naca0012.timeout = 1600
polar_naca0012.tol = 0.00001
test_list.append(polar_naca0012)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231727, 0.261637, -0.166869, 0.012707] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948, 0.625438] #last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase('cylinder_lowmach')
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.861860, -1.399846, -1.557250, 110.230719] #last 4 columns
cylinder_lowmach.su2_exec = "parallel_computation.py -f"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.647743, -5.442583, 0.903159, 0.025800] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.198777, 4.013989, 0.904265, 0.025941] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.071289, -7.366446, -0.187145, 0.010957] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438, 0.155815] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000764, -9.145363, 1.070528, 0.019417] #last 4 columns
turb_naca0012_sa.su2_exec = "parallel_computation.py -f"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039645, -7.220177, 1.059622, 0.019138] #last 4 columns
turb_naca0012_sst.su2_exec = "parallel_computation.py -f"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
# PROPELLER
propeller = TestCase('propeller')
propeller.cfg_dir = "rans/propeller"
propeller.cfg_file = "propeller.cfg"
propeller.test_iter = 10
propeller.test_vals = [-3.380312, -8.129519, 0.000043, 0.056159] #last 4 columns
propeller.su2_exec = "parallel_computation.py -f"
propeller.timeout = 3200
propeller.tol = 0.00001
test_list.append(propeller)
#############################
### Incompressible Euler ###
#############################
# NACA0012 Hydrofoil
inc_euler_naca0012 = TestCase('inc_euler_naca0012')
inc_euler_naca0012.cfg_dir = "incomp_euler/naca0012"
inc_euler_naca0012.cfg_file = "incomp_NACA0012.cfg"
inc_euler_naca0012.test_iter = 20
inc_euler_naca0012.test_vals = [-3.544713,-3.135163,0.968231,0.010161] #last 4 columns
inc_euler_naca0012.su2_exec = "parallel_computation.py -f"
inc_euler_naca0012.timeout = 1600
inc_euler_naca0012.tol = 0.00001
test_list.append(inc_euler_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710048, -11.007498, 0.000002, 0.210441] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
############################
### Transition ###
############################
# Schubauer-Klebanoff Natural Transition Case
schubauer_klebanoff_transition = TestCase('Schubauer_Klebanoff')
schubauer_klebanoff_transition.cfg_dir = "transition/Schubauer_Klebanoff"
schubauer_klebanoff_transition.cfg_file = "transitional_BC_model_ConfigFile.cfg"
schubauer_klebanoff_transition.test_iter = 250
schubauer_klebanoff_transition.test_vals = [-9.467876, -15.630835, 0.000520, 0.001062] #last 4 columns
schubauer_klebanoff_transition.su2_exec = "parallel_computation.py -f"
schubauer_klebanoff_transition.timeout = 1600
schubauer_klebanoff_transition.tol = 0.00001
test_list.append(schubauer_klebanoff_transition)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.783712, -15.192812, 0.300920, 0.019552] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.131587, -12.703243, 0.685900, 0.007594] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
# Inviscid WEDGE: generalized adjoint and custom DV
contadj_wedge = TestCase('contadj_wedge')
contadj_wedge.cfg_dir = "cont_adj_euler/wedge"
contadj_wedge.cfg_file = "inv_wedge_ROE.cfg"
contadj_wedge.test_iter = 10
contadj_wedge.test_vals = [2.780403, -3.223266, -1448300.000000, -0.000000] #last 4 columns
contadj_wedge.su2_exec = "parallel_computation.py -f"
contadj_wedge.timeout = 1600
contadj_wedge.tol = 0.00001
test_list.append(contadj_wedge)
# Inviscid fixed CL NACA0012
contadj_fixed_CL_naca0012 = TestCase('contadj_fixedcl_naca0012')
contadj_fixed_CL_naca0012.cfg_dir = "fixed_cl/naca0012"
contadj_fixed_CL_naca0012.cfg_file = "inv_NACA0012_ContAdj.cfg"
contadj_fixed_CL_naca0012.test_iter = 500
contadj_fixed_CL_naca0012.test_vals = [-2.921695, -8.474107, 0.250530, 0.000003] #last 4 columns
contadj_fixed_CL_naca0012.su2_exec = "parallel_computation.py -f"
contadj_fixed_CL_naca0012.timeout = 1600
contadj_fixed_CL_naca0012.tol = 0.00001
test_list.append(contadj_fixed_CL_naca0012)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.659040, -9.117773, 2.056700, -0.000000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.001210] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.012494] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, 19.169000, -0.000000] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.380929, -10.886092, -0.212470, 0.005448] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.968536, -12.133235, 1.939900, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718840, -7.012324, 2.932100, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Harmonic Balance ###
######################################
# Description of the regression test
harmonic_balance = TestCase('harmonic_balance')
harmonic_balance.cfg_dir = "harmonic_balance"
harmonic_balance.cfg_file = "HB.cfg"
harmonic_balance.test_iter = 25
harmonic_balance.test_vals = [-1.569573, 3.941896, 0.008780, 0.079775] #last 4 columns
harmonic_balance.su2_exec = "parallel_computation.py -f"
harmonic_balance.timeout = 1600
harmonic_balance.tol = 0.00001
test_list.append(harmonic_balance)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.597018, -0.133158, 0.169034, 0.821371] #last 4 columns
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.648320, -2.202753, 1.236836, 1.609040] #last 4 columns
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.166422,0.076751,1.398549,2.197047] #last 4 columns
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
square_cylinder.unsteady = True
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.014552, -0.004969] #last 4 columns
sine_gust.su2_exec = "parallel_computation.py -f"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077169, 0.036452, -0.001685, -0.000113] #last 4 columns
aeroelastic.su2_exec = "parallel_computation.py -f"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.058481, 1.115321, -0.000009, 0.000000] #last 4 columns
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.486409, 0.654417, -0.000037, 0.000000] #last 4 columns
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### Sliding Mesh ###
######################################
# Uniform flow
uniform_flow = TestCase('uniform_flow')
uniform_flow.cfg_dir = "sliding_interface/uniform_flow"
uniform_flow.cfg_file = "uniform_NN.cfg"
uniform_flow.test_iter = 50
uniform_flow.test_vals = [-0.368836, 5.156090, 0.000000, 0.000000] #last 4 columns
uniform_flow.su2_exec = "parallel_computation.py -f"
uniform_flow.timeout = 1600
uniform_flow.tol = 0.000001
uniform_flow.unsteady = True
test_list.append(uniform_flow)
# Channel_2D
channel_2D = TestCase('channel_2D')
channel_2D.cfg_dir = "sliding_interface/channel_2D"
channel_2D.cfg_file = "channel_2D_NN.cfg"
channel_2D.test_iter = 4
channel_2D.test_vals = [-1.498340, 4.541397, 0.000000, 0.000000] #last 4 columns
channel_2D.su2_exec = "parallel_computation.py -f"
channel_2D.timeout = 100
channel_2D.tol = 0.00001
channel_2D.unsteady = True
test_list.append(channel_2D)
# Channel_3D
channel_3D = TestCase('channel_3D')
channel_3D.cfg_dir = "sliding_interface/channel_3D"
channel_3D.cfg_file = "channel_3D_NN.cfg"
channel_3D.test_iter = 2
channel_3D.test_vals = [-1.998330, 3.957669, 0.000000, 0.000000] #last 4 columns
channel_3D.su2_exec = "parallel_computation.py -f"
channel_3D.timeout = 1600
channel_3D.tol = 0.00001
channel_3D.unsteady = True
test_list.append(channel_3D)
# # Pipe
# pipe = TestCase('pipe')
# pipe.cfg_dir = "sliding_interface/pipe"
# pipe.cfg_file = "pipe_NN.cfg"
# pipe.test_iter = 2
# pipe.test_vals = [-3.503708, 3.194241, 0.000000, 0.000000] #last 4 columns
# pipe.su2_exec = "parallel_computation.py -f"
# pipe.timeout = 1600
# pipe.tol = 0.00001
# pipe.unsteady = True
# test_list.append(pipe)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase('statbeam3d')
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-8.520066, -8.069308, -8.062384, 64095.000000] #last 4 columns
statbeam3d.su2_exec = "parallel_computation_fsi.py -f"
statbeam3d.timeout = 1600
statbeam3d.tol = 0.00001
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase('dynbeam2d')
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-9.420641, -5.365871, -12.430382, 6.5210e+04] #last 4 columns
dynbeam2d.su2_exec = "parallel_computation_fsi.py -f"
dynbeam2d.timeout = 1600
dynbeam2d.tol = 0.00001
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase('fsi2d')
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI_2D.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [2.000000, 0.500000, -7.777910, -1.139830] #last 4 columns
fsi2d.su2_exec = "parallel_computation_fsi.py -f"
fsi2d.timeout = 1600
fsi2d.tol = 0.00001
test_list.append(fsi2d)
##########################
### Python wrapper ###
##########################
# NACA0012
pywrapper_naca0012 = TestCase('pywrapper_naca0012')
pywrapper_naca0012.cfg_dir = "euler/naca0012"
pywrapper_naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
pywrapper_naca0012.test_iter = 100
pywrapper_naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
pywrapper_naca0012.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"
pywrapper_naca0012.timeout = 1600
pywrapper_naca0012.tol = 0.00001
test_list.append(pywrapper_naca0012)
# NACA0012 (SST, FUN3D results for finest grid: CL=1.0840, CD=0.01253)
pywrapper_turb_naca0012_sst = TestCase('pywrapper_turb_naca0012_sst')
pywrapper_turb_naca0012_sst.cfg_dir = "rans/naca0012"
pywrapper_turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
pywrapper_turb_naca0012_sst.test_iter = 10
pywrapper_turb_naca0012_sst.test_vals = [-15.039645, -7.220177, 1.059622, 0.019138] #last 4 columns
pywrapper_turb_naca0012_sst.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"
pywrapper_turb_naca0012_sst.timeout = 3200
pywrapper_turb_naca0012_sst.tol = 0.00001
test_list.append(pywrapper_turb_naca0012_sst)
# Square cylinder
pywrapper_square_cylinder = TestCase('pywrapper_square_cylinder')
pywrapper_square_cylinder.cfg_dir = "unsteady/square_cylinder"
pywrapper_square_cylinder.cfg_file = "turb_square.cfg"
pywrapper_square_cylinder.test_iter = 3
pywrapper_square_cylinder.test_vals = [-1.166422,0.076751,1.398549,2.197047] #last 4 columns
pywrapper_square_cylinder.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"
pywrapper_square_cylinder.timeout = 1600
pywrapper_square_cylinder.tol = 0.00001
pywrapper_square_cylinder.unsteady = True
test_list.append(pywrapper_square_cylinder)
# Aeroelastic
pywrapper_aeroelastic = TestCase('pywrapper_aeroelastic')
pywrapper_aeroelastic.cfg_dir = "aeroelastic"
pywrapper_aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
pywrapper_aeroelastic.test_iter = 2
pywrapper_aeroelastic.test_vals = [0.077169, 0.036452, -0.001685, -0.000113] #last 4 columns
pywrapper_aeroelastic.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"
pywrapper_aeroelastic.timeout = 1600
pywrapper_aeroelastic.tol = 0.000001
pywrapper_aeroelastic.unsteady = True
test_list.append(pywrapper_aeroelastic)
# FSI, 2d
pywrapper_fsi2d = TestCase('pywrapper_fsi2d')
pywrapper_fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
pywrapper_fsi2d.cfg_file = "configFSI_2D.cfg"
pywrapper_fsi2d.test_iter = 4
pywrapper_fsi2d.test_vals = [2.000000, 0.500000, -7.777910, -1.139830] #last 4 columns
pywrapper_fsi2d.su2_exec = "mpirun -np 2 SU2_CFD.py --nZone 2 --fsi True --parallel -f"
pywrapper_fsi2d.timeout = 1600
pywrapper_fsi2d.tol = 0.00001
test_list.append(pywrapper_fsi2d)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
######################################
### RUN SU2_DEF TESTS ###
######################################
# Inviscid NACA0012 (triangles)
naca0012_def = TestCase('naca0012_def')
naca0012_def.cfg_dir = "deformation/naca0012"
naca0012_def.cfg_file = "def_NACA0012.cfg"
naca0012_def.test_iter = 250
naca0012_def.test_vals = [5.44754e-15] #residual
naca0012_def.su2_exec = "mpirun -n 2 SU2_DEF"
naca0012_def.timeout = 1600
naca0012_def.tol = 1e-15
pass_list.append(naca0012_def.run_def())
test_list.append(naca0012_def)
# RAE2822 (mixed tris + quads)
rae2822_def = TestCase('rae2822_def')
rae2822_def.cfg_dir = "deformation/rae2822"
rae2822_def.cfg_file = "def_RAE2822.cfg"
rae2822_def.test_iter = 150
rae2822_def.test_vals = [1.47076e-15] #residual
rae2822_def.su2_exec = "mpirun -n 2 SU2_DEF"
rae2822_def.timeout = 1600
rae2822_def.tol = 1e-16
pass_list.append(rae2822_def.run_def())
test_list.append(rae2822_def)
# Turb NACA4412 (quads, wall distance)
naca4412_def = TestCase('naca4412_def')
naca4412_def.cfg_dir = "deformation/naca4412"
naca4412_def.cfg_file = "def_NACA4412.cfg"
naca4412_def.test_iter = 300
naca4412_def.test_vals = [4.46129e-15] #residual
naca4412_def.su2_exec = "mpirun -n 2 SU2_DEF"
naca4412_def.timeout = 1600
naca4412_def.tol = 1e-15
pass_list.append(naca4412_def.run_def())
test_list.append(naca4412_def)
# Brick of tets (inverse volume)
brick_tets_def = TestCase('brick_tets_def')
brick_tets_def.cfg_dir = "deformation/brick_tets"
brick_tets_def.cfg_file = "def_brick_tets.cfg"
brick_tets_def.test_iter = 1000
brick_tets_def.test_vals = [9.35558e-16] #residual
brick_tets_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_tets_def.timeout = 1600
brick_tets_def.tol = 1e-15
pass_list.append(brick_tets_def.run_def())
test_list.append(brick_tets_def)
# Brick of isotropic hexas (inverse volume)
brick_hex_def = TestCase('brick_hex_def')
brick_hex_def.cfg_dir = "deformation/brick_hex"
brick_hex_def.cfg_file = "def_brick_hex.cfg"
brick_hex_def.test_iter = 1000
brick_hex_def.test_vals = [1.46423e-15] #residual
brick_hex_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_hex_def.timeout = 1600
brick_hex_def.tol = 1e-15
pass_list.append(brick_hex_def.run_def())
test_list.append(brick_hex_def)
# Brick with a pyramid layer (inverse volume)
brick_pyra_def = TestCase('brick_pyra_def')
brick_pyra_def.cfg_dir = "deformation/brick_pyra"
brick_pyra_def.cfg_file = "def_brick_pyra.cfg"
brick_pyra_def.test_iter = 100
brick_pyra_def.test_vals = [5.97202e-15] #residual
brick_pyra_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_pyra_def.timeout = 1600
brick_pyra_def.tol = 1e-15
pass_list.append(brick_pyra_def.run_def())
test_list.append(brick_pyra_def)
# Brick of isotropic prisms (inverse volume)
brick_prism_def = TestCase('brick_prism_def')
brick_prism_def.cfg_dir = "deformation/brick_prism"
brick_prism_def.cfg_file = "def_brick_prism.cfg"
brick_prism_def.test_iter = 100
brick_prism_def.test_vals = [2.80867e-14] #residual
brick_prism_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_prism_def.timeout = 1600
brick_prism_def.tol = 1e-15
pass_list.append(brick_prism_def.run_def())
test_list.append(brick_prism_def)
# Brick of prisms with high aspect ratio cells near the wall (wall distance)
brick_prism_rans_def = TestCase('brick_prism_rans_def')
brick_prism_rans_def.cfg_dir = "deformation/brick_prism_rans"
brick_prism_rans_def.cfg_file = "def_brick_prism_rans.cfg"
brick_prism_rans_def.test_iter = 50
brick_prism_rans_def.test_vals = [3.5265e-15] #residual
brick_prism_rans_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_prism_rans_def.timeout = 1600
brick_prism_rans_def.tol = 1e-15
pass_list.append(brick_prism_rans_def.run_def())
test_list.append(brick_prism_rans_def)
# Brick of hexas with high aspect ratio cells near the wall (inverse volume)
brick_hex_rans_def = TestCase('brick_hex_rans_def')
brick_hex_rans_def.cfg_dir = "deformation/brick_hex_rans"
brick_hex_rans_def.cfg_file = "def_brick_hex_rans.cfg"
brick_hex_rans_def.test_iter = 600
brick_hex_rans_def.test_vals = [2.75292e-14] #residual
brick_hex_rans_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_hex_rans_def.timeout = 1600
brick_hex_rans_def.tol = 1e-16
pass_list.append(brick_hex_rans_def.run_def())
test_list.append(brick_hex_rans_def)
# Cylindrical FFD test
cylinder_ffd_def = TestCase('cylinder_ffd_def')
cylinder_ffd_def.cfg_dir = "deformation/cylindrical_ffd"
cylinder_ffd_def.cfg_file = "def_cylindrical.cfg"
cylinder_ffd_def.test_iter = 50
cylinder_ffd_def.test_vals = [2.31204e-10] #residual
cylinder_ffd_def.su2_exec = "mpirun -n 2 SU2_DEF"
cylinder_ffd_def.timeout = 1600
cylinder_ffd_def.tol = 1e-16
pass_list.append(cylinder_ffd_def.run_def())
test_list.append(cylinder_ffd_def)
# Spherical FFD test
sphere_ffd_def = TestCase('sphere_ffd_def')
sphere_ffd_def.cfg_dir = "deformation/spherical_ffd"
sphere_ffd_def.cfg_file = "def_spherical.cfg"
sphere_ffd_def.test_iter = 50
sphere_ffd_def.test_vals = [2.0062e-10] #residual
sphere_ffd_def.su2_exec = "mpirun -n 2 SU2_DEF"
sphere_ffd_def.timeout = 1600
sphere_ffd_def.tol = 1e-16
pass_list.append(sphere_ffd_def.run_def())
test_list.append(sphere_ffd_def)
# Spherical FFD test using BSplines
sphere_ffd_def_bspline = TestCase('sphere_ffd_def_bspline')
sphere_ffd_def_bspline.cfg_dir = "deformation/spherical_ffd"
sphere_ffd_def_bspline.cfg_file = "def_spherical_bspline.cfg"
sphere_ffd_def_bspline.test_iter = 50
sphere_ffd_def_bspline.test_vals = [1.20429e-10] #residual
sphere_ffd_def_bspline.su2_exec = "mpirun -n 2 SU2_DEF"
sphere_ffd_def_bspline.timeout = 1600
sphere_ffd_def_bspline.tol = 1e-16
pass_list.append(sphere_ffd_def_bspline.run_def())
test_list.append(sphere_ffd_def_bspline)
# Tests summary
print '=================================================================='
print 'Summary of the parallel tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s'%test.tag
else:
print '* FAILED - %s'%test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.071007, 2.301191, 0.008562, 0.028922] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.690232, 3.924432, -0.252221, 0.044419] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.400678, -12.932056, 0.282557, 0.012706] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
# Fixed CL NACA0012
fixedCL_naca0012 = TestCase('fixedcl_naca0012')
fixedCL_naca0012.cfg_dir = "fixed_cl/naca0012"
fixedCL_naca0012.cfg_file = "inv_NACA0012.cfg"
fixedCL_naca0012.test_iter = 500
fixedCL_naca0012.test_vals = [-5.930145,-0.546310,0.300089,0.019393] #last 4 columns
fixedCL_naca0012.su2_exec = "parallel_computation.py -f"
fixedCL_naca0012.timeout = 1600
fixedCL_naca0012.tol = 0.00001
test_list.append(fixedCL_naca0012)
# Polar sweep of the inviscid NACA0012
polar_naca0012 = TestCase('polar_naca0012')
polar_naca0012.cfg_dir = "polar/naca0012"
polar_naca0012.cfg_file = "inv_NACA0012.cfg"
polar_naca0012.polar = True
polar_naca0012.test_iter = 10
polar_naca0012.test_vals = [-1.298373, 4.139860, 0.010703, 0.008932] #last 4 columns
polar_naca0012.su2_exec = "compute_polar.py -i 11"
polar_naca0012.timeout = 1600
polar_naca0012.tol = 0.00001
test_list.append(polar_naca0012)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231727, 0.261637, -0.166869, 0.012707] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948, 0.625438] #last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase('cylinder_lowmach')
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.861860, -1.399846, -1.557250, 110.230719] #last 4 columns
cylinder_lowmach.su2_exec = "parallel_computation.py -f"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.647743, -5.442583, 0.903159, 0.025800] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.198777, 4.013989, 0.904265, 0.025941] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.071289, -7.366446, -0.187145, 0.010957] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438, 0.155815] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000764, -9.145363, 1.070528, 0.019417] #last 4 columns
turb_naca0012_sa.su2_exec = "parallel_computation.py -f"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039645, -7.220177, 1.059622, 0.019138] #last 4 columns
turb_naca0012_sst.su2_exec = "parallel_computation.py -f"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
# PROPELLER
propeller = TestCase('propeller')
propeller.cfg_dir = "rans/propeller"
propeller.cfg_file = "propeller.cfg"
propeller.test_iter = 10
propeller.test_vals = [-3.380312, -8.129519, 0.000043, 0.056159] #last 4 columns
propeller.su2_exec = "parallel_computation.py -f"
propeller.timeout = 3200
propeller.tol = 0.00001
test_list.append(propeller)
#############################
### Incompressible Euler ###
#############################
# NACA0012 Hydrofoil
inc_euler_naca0012 = TestCase('inc_euler_naca0012')
inc_euler_naca0012.cfg_dir = "incomp_euler/naca0012"
inc_euler_naca0012.cfg_file = "incomp_NACA0012.cfg"
inc_euler_naca0012.test_iter = 20
inc_euler_naca0012.test_vals = [-3.544713,-3.135163,0.968231,0.010161] #last 4 columns
inc_euler_naca0012.su2_exec = "parallel_computation.py -f"
inc_euler_naca0012.timeout = 1600
inc_euler_naca0012.tol = 0.00001
test_list.append(inc_euler_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710048, -11.007498, 0.000002, 0.210441] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
############################
### Transition ###
############################
# Schubauer-Klebanoff Natural Transition Case
schubauer_klebanoff_transition = TestCase('Schubauer_Klebanoff')
schubauer_klebanoff_transition.cfg_dir = "transition/Schubauer_Klebanoff"
schubauer_klebanoff_transition.cfg_file = "transitional_BC_model_ConfigFile.cfg"
schubauer_klebanoff_transition.test_iter = 250
schubauer_klebanoff_transition.test_vals = [-9.467876, -15.630835, 0.000520, 0.001062] #last 4 columns
schubauer_klebanoff_transition.su2_exec = "parallel_computation.py -f"
schubauer_klebanoff_transition.timeout = 1600
schubauer_klebanoff_transition.tol = 0.00001
test_list.append(schubauer_klebanoff_transition)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.783712, -15.192812, 0.300920, 0.019552] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.131587, -12.703243, 0.685900, 0.007594] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
# Inviscid WEDGE: generalized adjoint and custom DV
contadj_wedge = TestCase('contadj_wedge')
contadj_wedge.cfg_dir = "cont_adj_euler/wedge"
contadj_wedge.cfg_file = "inv_wedge_ROE.cfg"
contadj_wedge.test_iter = 10
contadj_wedge.test_vals = [2.780403, -3.223266, -1448300.000000, -0.000000] #last 4 columns
contadj_wedge.su2_exec = "parallel_computation.py -f"
contadj_wedge.timeout = 1600
contadj_wedge.tol = 0.00001
test_list.append(contadj_wedge)
# Inviscid fixed CL NACA0012
contadj_fixed_CL_naca0012 = TestCase('contadj_fixedcl_naca0012')
contadj_fixed_CL_naca0012.cfg_dir = "fixed_cl/naca0012"
contadj_fixed_CL_naca0012.cfg_file = "inv_NACA0012_ContAdj.cfg"
contadj_fixed_CL_naca0012.test_iter = 500
contadj_fixed_CL_naca0012.test_vals = [-2.921695, -8.474107, 0.250530, 0.000003] #last 4 columns
contadj_fixed_CL_naca0012.su2_exec = "parallel_computation.py -f"
contadj_fixed_CL_naca0012.timeout = 1600
contadj_fixed_CL_naca0012.tol = 0.00001
test_list.append(contadj_fixed_CL_naca0012)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.659040, -9.117773, 2.056700, -0.000000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.001210] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.012494] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, 19.169000, -0.000000] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.380929, -10.886092, -0.212470, 0.005448] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.968536, -12.133235, 1.939900, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718840, -7.012324, 2.932100, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Harmonic Balance ###
######################################
# Description of the regression test
harmonic_balance = TestCase('harmonic_balance')
harmonic_balance.cfg_dir = "harmonic_balance"
harmonic_balance.cfg_file = "HB.cfg"
harmonic_balance.test_iter = 25
harmonic_balance.test_vals = [-1.569573, 3.941896, 0.008780, 0.079775] #last 4 columns
harmonic_balance.su2_exec = "parallel_computation.py -f"
harmonic_balance.timeout = 1600
harmonic_balance.tol = 0.00001
test_list.append(harmonic_balance)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.597018, -0.133158, 0.169034, 0.821371] #last 4 columns
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.648320, -2.202753, 1.236836, 1.609040] #last 4 columns
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.166422,0.076751,1.398549,2.197047] #last 4 columns
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
square_cylinder.unsteady = True
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.014552, -0.004969] #last 4 columns
sine_gust.su2_exec = "parallel_computation.py -f"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077169, 0.036452, -0.001685, -0.000113] #last 4 columns
aeroelastic.su2_exec = "parallel_computation.py -f"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.058481, 1.115321, -0.000009, 0.000000] #last 4 columns
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.486409, 0.654417, -0.000037, 0.000000] #last 4 columns
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### Sliding Mesh ###
######################################
# Uniform flow
uniform_flow = TestCase('uniform_flow')
uniform_flow.cfg_dir = "sliding_interface/uniform_flow"
uniform_flow.cfg_file = "uniform_NN.cfg"
uniform_flow.test_iter = 50
uniform_flow.test_vals = [-0.368836, 5.156090, 0.000000, 0.000000] #last 4 columns
uniform_flow.su2_exec = "parallel_computation.py -f"
uniform_flow.timeout = 1600
uniform_flow.tol = 0.000001
uniform_flow.unsteady = True
test_list.append(uniform_flow)
# Channel_2D
channel_2D = TestCase('channel_2D')
channel_2D.cfg_dir = "sliding_interface/channel_2D"
channel_2D.cfg_file = "channel_2D_NN.cfg"
channel_2D.test_iter = 4
channel_2D.test_vals = [-1.498340, 4.541397, 0.000000, 0.000000] #last 4 columns
channel_2D.su2_exec = "parallel_computation.py -f"
channel_2D.timeout = 100
channel_2D.tol = 0.00001
channel_2D.unsteady = True
test_list.append(channel_2D)
# Channel_3D
channel_3D = TestCase('channel_3D')
channel_3D.cfg_dir = "sliding_interface/channel_3D"
channel_3D.cfg_file = "channel_3D_NN.cfg"
channel_3D.test_iter = 2
channel_3D.test_vals = [-1.998330, 3.957669, 0.000000, 0.000000] #last 4 columns
channel_3D.su2_exec = "parallel_computation.py -f"
channel_3D.timeout = 1600
channel_3D.tol = 0.00001
channel_3D.unsteady = True
test_list.append(channel_3D)
# # Pipe
# pipe = TestCase('pipe')
# pipe.cfg_dir = "sliding_interface/pipe"
# pipe.cfg_file = "pipe_NN.cfg"
# pipe.test_iter = 2
# pipe.test_vals = [-3.503708, 3.194241, 0.000000, 0.000000] #last 4 columns
# pipe.su2_exec = "parallel_computation.py -f"
# pipe.timeout = 1600
# pipe.tol = 0.00001
# pipe.unsteady = True
# test_list.append(pipe)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase('statbeam3d')
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-8.520066, -8.069308, -8.062384, 64095.000000] #last 4 columns
statbeam3d.su2_exec = "parallel_computation_fsi.py -f"
statbeam3d.timeout = 1600
statbeam3d.tol = 0.00001
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase('dynbeam2d')
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-9.420641, -5.365871, -12.430382, 6.5210e+04] #last 4 columns
dynbeam2d.su2_exec = "parallel_computation_fsi.py -f"
dynbeam2d.timeout = 1600
dynbeam2d.tol = 0.00001
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase('fsi2d')
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI_2D.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [2.000000, 0.500000, -7.777910, -1.139830] #last 4 columns
fsi2d.su2_exec = "parallel_computation_fsi.py -f"
fsi2d.timeout = 1600
fsi2d.tol = 0.00001
test_list.append(fsi2d)
##########################
### Python wrapper ###
##########################
# NACA0012
pywrapper_naca0012 = TestCase('pywrapper_naca0012')
pywrapper_naca0012.cfg_dir = "euler/naca0012"
pywrapper_naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
pywrapper_naca0012.test_iter = 100
pywrapper_naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
pywrapper_naca0012.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"
pywrapper_naca0012.timeout = 1600
pywrapper_naca0012.tol = 0.00001
test_list.append(pywrapper_naca0012)
# NACA0012 (SST, FUN3D results for finest grid: CL=1.0840, CD=0.01253)
pywrapper_turb_naca0012_sst = TestCase('pywrapper_turb_naca0012_sst')
pywrapper_turb_naca0012_sst.cfg_dir = "rans/naca0012"
pywrapper_turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
pywrapper_turb_naca0012_sst.test_iter = 10
pywrapper_turb_naca0012_sst.test_vals = [-15.039645, -7.220177, 1.059622, 0.019138] #last 4 columns
pywrapper_turb_naca0012_sst.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"
pywrapper_turb_naca0012_sst.timeout = 3200
pywrapper_turb_naca0012_sst.tol = 0.00001
test_list.append(pywrapper_turb_naca0012_sst)
# Square cylinder
pywrapper_square_cylinder = TestCase('pywrapper_square_cylinder')
pywrapper_square_cylinder.cfg_dir = "unsteady/square_cylinder"
pywrapper_square_cylinder.cfg_file = "turb_square.cfg"
pywrapper_square_cylinder.test_iter = 3
pywrapper_square_cylinder.test_vals = [-1.166422,0.076751,1.398549,2.197047] #last 4 columns
pywrapper_square_cylinder.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"
pywrapper_square_cylinder.timeout = 1600
pywrapper_square_cylinder.tol = 0.00001
pywrapper_square_cylinder.unsteady = True
test_list.append(pywrapper_square_cylinder)
# Aeroelastic
pywrapper_aeroelastic = TestCase('pywrapper_aeroelastic')
pywrapper_aeroelastic.cfg_dir = "aeroelastic"
pywrapper_aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
pywrapper_aeroelastic.test_iter = 2
pywrapper_aeroelastic.test_vals = [0.077169, 0.036452, -0.001685, -0.000113] #last 4 columns
pywrapper_aeroelastic.su2_exec = "mpirun -np 2 SU2_CFD.py --parallel -f"
pywrapper_aeroelastic.timeout = 1600
pywrapper_aeroelastic.tol = 0.000001
pywrapper_aeroelastic.unsteady = True
test_list.append(pywrapper_aeroelastic)
# FSI, 2d
pywrapper_fsi2d = TestCase('pywrapper_fsi2d')
pywrapper_fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
pywrapper_fsi2d.cfg_file = "configFSI_2D.cfg"
pywrapper_fsi2d.test_iter = 4
pywrapper_fsi2d.test_vals = [2.000000, 0.500000, -7.777910, -1.139830] #last 4 columns
pywrapper_fsi2d.su2_exec = "mpirun -np 2 SU2_CFD.py --nZone 2 --fsi True --parallel -f"
pywrapper_fsi2d.timeout = 1600
pywrapper_fsi2d.tol = 0.00001
test_list.append(pywrapper_fsi2d)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
######################################
### RUN SU2_DEF TESTS ###
######################################
# Inviscid NACA0012 (triangles)
naca0012_def = TestCase('naca0012_def')
naca0012_def.cfg_dir = "deformation/naca0012"
naca0012_def.cfg_file = "def_NACA0012.cfg"
naca0012_def.test_iter = 250
naca0012_def.test_vals = [5.44754e-15] #residual
naca0012_def.su2_exec = "mpirun -n 2 SU2_DEF"
naca0012_def.timeout = 1600
naca0012_def.tol = 1e-15
pass_list.append(naca0012_def.run_def())
test_list.append(naca0012_def)
# RAE2822 (mixed tris + quads)
rae2822_def = TestCase('rae2822_def')
rae2822_def.cfg_dir = "deformation/rae2822"
rae2822_def.cfg_file = "def_RAE2822.cfg"
rae2822_def.test_iter = 150
rae2822_def.test_vals = [1.47076e-15] #residual
rae2822_def.su2_exec = "mpirun -n 2 SU2_DEF"
rae2822_def.timeout = 1600
rae2822_def.tol = 1e-16
pass_list.append(rae2822_def.run_def())
test_list.append(rae2822_def)
# Turb NACA4412 (quads, wall distance)
naca4412_def = TestCase('naca4412_def')
naca4412_def.cfg_dir = "deformation/naca4412"
naca4412_def.cfg_file = "def_NACA4412.cfg"
naca4412_def.test_iter = 300
naca4412_def.test_vals = [4.46129e-15] #residual
naca4412_def.su2_exec = "mpirun -n 2 SU2_DEF"
naca4412_def.timeout = 1600
naca4412_def.tol = 1e-15
pass_list.append(naca4412_def.run_def())
test_list.append(naca4412_def)
# Brick of tets (inverse volume)
brick_tets_def = TestCase('brick_tets_def')
brick_tets_def.cfg_dir = "deformation/brick_tets"
brick_tets_def.cfg_file = "def_brick_tets.cfg"
brick_tets_def.test_iter = 1000
brick_tets_def.test_vals = [9.35558e-16] #residual
brick_tets_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_tets_def.timeout = 1600
brick_tets_def.tol = 1e-15
pass_list.append(brick_tets_def.run_def())
test_list.append(brick_tets_def)
# Brick of isotropic hexas (inverse volume)
brick_hex_def = TestCase('brick_hex_def')
brick_hex_def.cfg_dir = "deformation/brick_hex"
brick_hex_def.cfg_file = "def_brick_hex.cfg"
brick_hex_def.test_iter = 1000
brick_hex_def.test_vals = [1.46423e-15] #residual
brick_hex_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_hex_def.timeout = 1600
brick_hex_def.tol = 1e-15
pass_list.append(brick_hex_def.run_def())
test_list.append(brick_hex_def)
# Brick with a pyramid layer (inverse volume)
brick_pyra_def = TestCase('brick_pyra_def')
brick_pyra_def.cfg_dir = "deformation/brick_pyra"
brick_pyra_def.cfg_file = "def_brick_pyra.cfg"
brick_pyra_def.test_iter = 100
brick_pyra_def.test_vals = [5.97202e-15] #residual
brick_pyra_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_pyra_def.timeout = 1600
brick_pyra_def.tol = 1e-15
pass_list.append(brick_pyra_def.run_def())
test_list.append(brick_pyra_def)
# Brick of isotropic prisms (inverse volume)
brick_prism_def = TestCase('brick_prism_def')
brick_prism_def.cfg_dir = "deformation/brick_prism"
brick_prism_def.cfg_file = "def_brick_prism.cfg"
brick_prism_def.test_iter = 100
brick_prism_def.test_vals = [2.80867e-14] #residual
brick_prism_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_prism_def.timeout = 1600
brick_prism_def.tol = 1e-15
pass_list.append(brick_prism_def.run_def())
test_list.append(brick_prism_def)
# Brick of prisms with high aspect ratio cells near the wall (wall distance)
brick_prism_rans_def = TestCase('brick_prism_rans_def')
brick_prism_rans_def.cfg_dir = "deformation/brick_prism_rans"
brick_prism_rans_def.cfg_file = "def_brick_prism_rans.cfg"
brick_prism_rans_def.test_iter = 50
brick_prism_rans_def.test_vals = [3.5265e-15] #residual
brick_prism_rans_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_prism_rans_def.timeout = 1600
brick_prism_rans_def.tol = 1e-15
pass_list.append(brick_prism_rans_def.run_def())
test_list.append(brick_prism_rans_def)
# Brick of hexas with high aspect ratio cells near the wall (inverse volume)
brick_hex_rans_def = TestCase('brick_hex_rans_def')
brick_hex_rans_def.cfg_dir = "deformation/brick_hex_rans"
brick_hex_rans_def.cfg_file = "def_brick_hex_rans.cfg"
brick_hex_rans_def.test_iter = 600
brick_hex_rans_def.test_vals = [2.75292e-14] #residual
brick_hex_rans_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_hex_rans_def.timeout = 1600
brick_hex_rans_def.tol = 1e-16
pass_list.append(brick_hex_rans_def.run_def())
test_list.append(brick_hex_rans_def)
# Cylindrical FFD test
cylinder_ffd_def = TestCase('cylinder_ffd_def')
cylinder_ffd_def.cfg_dir = "deformation/cylindrical_ffd"
cylinder_ffd_def.cfg_file = "def_cylindrical.cfg"
cylinder_ffd_def.test_iter = 50
cylinder_ffd_def.test_vals = [2.31204e-10] #residual
cylinder_ffd_def.su2_exec = "mpirun -n 2 SU2_DEF"
cylinder_ffd_def.timeout = 1600
cylinder_ffd_def.tol = 1e-16
pass_list.append(cylinder_ffd_def.run_def())
test_list.append(cylinder_ffd_def)
# Spherical FFD test
sphere_ffd_def = TestCase('sphere_ffd_def')
sphere_ffd_def.cfg_dir = "deformation/spherical_ffd"
sphere_ffd_def.cfg_file = "def_spherical.cfg"
sphere_ffd_def.test_iter = 50
sphere_ffd_def.test_vals = [2.0062e-10] #residual
sphere_ffd_def.su2_exec = "mpirun -n 2 SU2_DEF"
sphere_ffd_def.timeout = 1600
sphere_ffd_def.tol = 1e-16
pass_list.append(sphere_ffd_def.run_def())
test_list.append(sphere_ffd_def)
# Spherical FFD test using BSplines
sphere_ffd_def_bspline = TestCase('sphere_ffd_def_bspline')
sphere_ffd_def_bspline.cfg_dir = "deformation/spherical_ffd"
sphere_ffd_def_bspline.cfg_file = "def_spherical_bspline.cfg"
sphere_ffd_def_bspline.test_iter = 50
sphere_ffd_def_bspline.test_vals = [1.20429e-10] #residual
sphere_ffd_def_bspline.su2_exec = "mpirun -n 2 SU2_DEF"
sphere_ffd_def_bspline.timeout = 1600
sphere_ffd_def_bspline.tol = 1e-16
pass_list.append(sphere_ffd_def_bspline.run_def())
test_list.append(sphere_ffd_def_bspline)
# Tests summary
print '=================================================================='
print 'Summary of the parallel tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s'%test.tag
else:
print '* FAILED - %s'%test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606839, -9.035212, -0.000000, 0.005688] #last 4 columns
discadj_naca0012.su2_exec = "SU2_CFD_AD"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.724711, -4.052467, -0.000000, 0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "SU2_CFD_AD"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
# Arina nozzle 2D
discadj_arina2k = TestCase('discadj_arina2k')
discadj_arina2k.cfg_dir = "disc_adj_euler/arina2k"
discadj_arina2k.cfg_file = "Arina2KRS.cfg"
discadj_arina2k.test_iter = 20
discadj_arina2k.test_vals = [-0.774805, -0.801209, 3.1979e+02, 0.0000e+00] #last 4 columns
discadj_arina2k.su2_exec = "SU2_CFD_AD"
discadj_arina2k.timeout = 8400
discadj_arina2k.tol = 0.00001
test_list.append(discadj_arina2k)
#######################################################
### Disc. adj. compressible RANS ###
#######################################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-1.751962, 0.485751, 0.182121, -0.000018] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-1.654903, -0.491485, 0.109157, 0.000011] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "disc_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [-3.633197, -2.544956, 0.000000, 0.000000] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "SU2_CFD_AD"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder (Heated)
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "disc_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "heated_cylinder.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [-2.374306, -2.371564, 0.000000, 0.000000] #last 4 columns
discadj_incomp_cylinder.su2_exec = "SU2_CFD_AD"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012 SA
discadj_incomp_turb_NACA0012_sa = TestCase('discadj_incomp_turb_NACA0012_sa')
discadj_incomp_turb_NACA0012_sa.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sa.cfg_file = "turb_naca0012_sa.cfg"
discadj_incomp_turb_NACA0012_sa.test_iter = 10
discadj_incomp_turb_NACA0012_sa.test_vals = [-3.845979, -1.031094, 0.000000, 0.000000] #last 4 columns
discadj_incomp_turb_NACA0012_sa.su2_exec = "SU2_CFD_AD"
discadj_incomp_turb_NACA0012_sa.timeout = 1600
discadj_incomp_turb_NACA0012_sa.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sa)
# Adjoint Incompressible Turbulent NACA 0012 SST
discadj_incomp_turb_NACA0012_sst = TestCase('discadj_incomp_turb_NACA0012_sst')
discadj_incomp_turb_NACA0012_sst.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sst.cfg_file = "turb_naca0012_sst.cfg"
discadj_incomp_turb_NACA0012_sst.test_iter = 10
discadj_incomp_turb_NACA0012_sst.test_vals = [-3.845759, -2.416668, 0.000000, 0.000000] #last 4 columns
discadj_incomp_turb_NACA0012_sst.su2_exec = "SU2_CFD_AD"
discadj_incomp_turb_NACA0012_sst.timeout = 1600
discadj_incomp_turb_NACA0012_sst.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746904, -1.544886, -0.008345, 0.000014] #last 4 columns
discadj_cylinder.su2_exec = "SU2_CFD_AD"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##########################################################################
### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order ###
##########################################################################
# Turbulent Cylinder
discadj_DT_1ST_cylinder = TestCase('unsteady_cylinder_DT_1ST')
discadj_DT_1ST_cylinder.cfg_dir = "disc_adj_rans/cylinder_DT_1ST"
discadj_DT_1ST_cylinder.cfg_file = "cylinder.cfg"
discadj_DT_1ST_cylinder.test_iter = 9
discadj_DT_1ST_cylinder.test_vals = [3.698165, -1.607052, -2.2500e-03, 2.7211e-05] #last 4 columns
discadj_DT_1ST_cylinder.su2_exec = "SU2_CFD_AD"
discadj_DT_1ST_cylinder.timeout = 1600
discadj_DT_1ST_cylinder.tol = 0.00001
discadj_DT_1ST_cylinder.unsteady = True
test_list.append(discadj_DT_1ST_cylinder)
###################################
### Structural Adjoint ###
###################################
# Structural model
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 9
discadj_fea.test_vals = [-6.282767, -6.361594, -3.6413e-04, -8.7087e+00] #last 4 columns
discadj_fea.su2_exec = "SU2_CFD_AD"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Disc. adj. heat ###
###################################
# Discrete adjoint for heated cylinder
discadj_heat = TestCase('discadj_heat')
discadj_heat.cfg_dir = "disc_adj_heat"
discadj_heat.cfg_file = "disc_adj_heat.cfg"
discadj_heat.test_iter = 10
discadj_heat.test_vals = [3.176483, 1.144873, -1040.512028, -3277.663739] #last 4 columns
discadj_heat.su2_exec = "SU2_CFD_AD"
discadj_heat.timeout = 1600
discadj_heat.tol = 0.00001
test_list.append(discadj_heat)
###################################
### Coupled FSI Adjoint ###
###################################
# Structural model
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "configAD_fsi.cfg"
discadj_fsi.test_iter = 3000
discadj_fsi.test_vals = [0.958848,-0.157183,0.658415,1.302076] #last 4 columns
discadj_fsi.su2_exec = "SU2_CFD_AD"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
######################################
### RUN PYTHON TESTS ###
######################################
# test discrete_adjoint.py
discadj_euler_py = TestCase('discadj_euler_py')
discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
discadj_euler_py.cfg_file = "inv_NACA0012.cfg"
discadj_euler_py.test_iter = 10
discadj_euler_py.su2_exec = "discrete_adjoint.py"
discadj_euler_py.timeout = 1600
discadj_euler_py.reference_file = "of_grad_cd_disc.dat.ref"
discadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_euler_py.run_filediff())
test_list.append(discadj_euler_py)
# test discrete_adjoint with multiple ffd boxes
discadj_multiple_ffd_py = TestCase('discadj_multiple_ffd_py')
discadj_multiple_ffd_py.cfg_dir = "multiple_ffd/naca0012"
discadj_multiple_ffd_py.cfg_file = "inv_NACA0012_ffd.cfg"
discadj_multiple_ffd_py.test_iter = 9
discadj_multiple_ffd_py.su2_exec = "discrete_adjoint.py"
discadj_multiple_ffd_py.timeout = 1600
discadj_multiple_ffd_py.reference_file = "of_grad_cd.dat.ref"
discadj_multiple_ffd_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_multiple_ffd_py.run_filediff())
test_list.append(discadj_multiple_ffd_py)
# test direct_differentiation.py
directdiff_euler_py = TestCase('directdiff_euler_py')
directdiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
directdiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
directdiff_euler_py.test_iter = 10
directdiff_euler_py.su2_exec = "direct_differentiation.py"
directdiff_euler_py.timeout = 1600
directdiff_euler_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_euler_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_euler_py.run_filediff())
test_list.append(directdiff_euler_py)
# test direct_differentiation.py with multiple ffd boxes
directdiff_multiple_ffd_py = TestCase('directdiff_multiple_ffd_py')
directdiff_multiple_ffd_py.cfg_dir = "multiple_ffd/naca0012"
directdiff_multiple_ffd_py.cfg_file = "inv_NACA0012_ffd.cfg"
directdiff_multiple_ffd_py.test_iter = 9
directdiff_multiple_ffd_py.su2_exec = "direct_differentiation.py"
directdiff_multiple_ffd_py.timeout = 1600
directdiff_multiple_ffd_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_multiple_ffd_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_multiple_ffd_py.run_filediff())
test_list.append(directdiff_multiple_ffd_py)
# test continuous_adjoint.py, with multiple objectives
discadj_multi_py = TestCase('discadj_multi_py')
discadj_multi_py.cfg_dir = "cont_adj_euler/wedge"
discadj_multi_py.cfg_file = "inv_wedge_ROE_multiobj.cfg"
discadj_multi_py.test_iter = 10
discadj_multi_py.su2_exec = "discrete_adjoint.py"
discadj_multi_py.timeout = 1600
discadj_multi_py.reference_file = "of_grad_combo.dat.refdiscrete"
discadj_multi_py.test_file = "of_grad_combo.dat"
pass_list.append(discadj_multi_py.run_filediff())
test_list.append(discadj_multi_py)
# Tests summary
print('==================================================================')
print('Summary of the serial tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s'%test.tag)
else:
print('* FAILED - %s'%test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ[
'TEST_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work'
os.environ[
'SU2_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2'
os.environ[
'SU2_RUN'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync Test Cases repo
os.chdir(os.environ['TEST_HOME'])
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# sync SU2 repo
os.chdir(os.environ['SU2_HOME'])
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# Build SU2_CFD in serial using autoconf
os.system('./configure --prefix=$SU2_HOME CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.110240, 2.263506, 0.008686,
0.029098] #last 4 columns
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.191618, -5.592802, 0.334809,
0.022197] #last 4 columns
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.711318, 3.913749, -0.252131,
0.044402] #last 4 columns
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.704347, -4.159916, 0.271678,
0.018869] #last 4 columns
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231916, 0.261866, -0.166832,
0.012717] #last 4 columns
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765426, -1.297422, 0.019496,
0.310082] #last 4 columns
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.442524, -5.441383, 0.884279,
0.024730] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.185243, 4.018464, 0.886786,
0.024927] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.069447, -7.354601, -0.187187,
0.010831] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438,
0.155815] #last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 20
turb_naca0012_sa.test_vals = [-6.607227, -9.778334, 1.098508,
0.012417] #last 4 columns
turb_naca0012_sa.su2_exec = "SU2_CFD"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 20
turb_naca0012_sst.test_vals = [-8.290782, -1.743121, 1.084189,
0.012583] #last 4 columns
turb_naca0012_sst.su2_exec = "SU2_CFD"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710052, -11.007500, -0.000001,
0.210445] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.787555, -15.192503, 0.300920,
0.536870] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.009929, -6.251311, -0.106940,
0.149230] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [
-3.677184, -9.141850, -2.056700, 4.497000
] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [
-2.744551, -8.216469, 0.518810, 0.229160
] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [
-1.041539, -6.578524, 1.772300, 0.620880
] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [
-0.814757, -5.726517, -19.169000, -2.994100
] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [
-5.377843, -10.882446, -0.212470, 0.269390
] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [
-11.980272, -12.146779, 1.9399, 0.000000
] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [
-5.718622, -7.027366, -2.932100, 0.000000
] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.643029, 2.849441, -4.443852,
0.000313] #last 4 columns
ramc.su2_exec = "SU2_CFD"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.627934, -0.164470, 0.051972,
2.547034] #last 4 columns
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.709662, -2.274900, 1.418422,
1.734206] #last 4 columns
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.544603, 0.048578, 1.398951,
2.196894] #last 4 columns
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### Real_Gas ###
######################################
# ls89_sa
ls89_sa = TestCase('ls89_sa')
ls89_sa.cfg_dir = "nicf/LS89"
ls89_sa.cfg_file = "turb_SA_PR.cfg"
ls89_sa.test_iter = 100
ls89_sa.test_vals = [-6.383111, -13.350395, 0.069071,
0.160893] #last 4 columns
ls89_sa.su2_exec = "SU2_CFD"
ls89_sa.timeout = 1600
ls89_sa.tol = 0.00001
test_list.append(ls89_sa)
# # ls89_sst
# ls89_sst = TestCase('ls89_sst')
# ls89_sst.cfg_dir = "nicf/LS89"
# ls89_sst.cfg_file = "turb_SST_PR.cfg"
# ls89_sst.test_iter = 100
# ls89_sst.test_vals = [-8.548266, -1.449437, 0.067986, 0.151168] #last 4 columns
# ls89_sst.su2_exec = "SU2_CFD"
# ls89_sst.timeout = 1600
# ls89_sst.tol = 0.00001
# test_list.append(ls89_sst)
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-1.448271, 4.749156, -0.000046,
0.000000] #last 4 columns
edge_VW.su2_exec = "SU2_CFD"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-1.998238, 4.172451, -0.000056,
0.000000] #last 4 columns
edge_PPR.su2_exec = "SU2_CFD"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git pull')
# Build SU2_CFD in serial using autoconf
os.system('./configure --prefix=$SU2_HOME CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.991375,2.388702,-0.042177,0.068520]
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-5.932646,-5.394328,0.335205,0.022232]
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.838548,3.781222,-0.252690,0.044489]
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.744759,-4.182702,0.281122,0.018310]
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.230001,0.252184,-0.163706,0.013547]
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.409812,-0.945306,0.088160,-5.192708]
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-2.729166,-5.506935,0.860798,0.023704] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.151533,4.144621,0.861331,0.023855] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.021253,-7.365210,-0.185394,0.015273] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327517,-6.563378,0.230436,0.155816]#last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.826334,-7.364207,-0.000025,0.803037] #last 4 columns
turb_naca0012.su2_exec = "SU2_CFD"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709986,-11.007545,0.000008,0.210347] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-12.214678,-16.000000,0.005483,0.536870] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.370788,-6.545955,-0.000023,0.147730] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-0.597482,-6.063713,-0.032305,25.115000] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-4.234330,-9.705736,0.005161,0.398940 ] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.810435,-6.920519,0.014614,1.020100] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-4.351102,-8.919996,-1.275200,-2.541400] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-2.888858,-8.085710,4.545700,0.109650] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [-6.049647,-6.004696,0.010909,0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-2.352353,-2.851967,-0.048345,0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119,2.854417,-4.439628,0.000188]
ramc.su2_exec = "SU2_CFD"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.545249,-0.083220,-0.007449,-14.207933]
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.743171,-1.295111,6.846763,0.823335]
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.542160,0.048661,1.398952,2.196894 ]
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### Real_Gas ###
######################################
# Supersonic_turbine
supersonic_turbine = TestCase('supersonic_turbine')
supersonic_turbine.cfg_dir = "real_gas/euler/supersonic_turbine"
supersonic_turbine.cfg_file = "supersonic.cfg"
supersonic_turbine.test_iter = 19
supersonic_turbine.test_vals = [-0.249215,5.701822,0.000000,0.000000 ]
supersonic_turbine.su2_exec = "SU2_CFD"
supersonic_turbine.timeout = 1600
supersonic_turbine.tol = 0.00001
test_list.append(square_cylinder)
# Supersonic_turbine
supersonic_nozzle = TestCase('supersonic_nozzle')
supersonic_nozzle.cfg_dir = "real_gas/euler/2Dnozzle"
supersonic_nozzle.cfg_file = "nozzle_MDM_shockwave.cfg"
supersonic_nozzle.test_iter = 559
supersonic_nozzle.test_vals = [-0.371019,4.755257,0.000000,0.000000 ]
supersonic_nozzle.su2_exec = "SU2_CFD"
supersonic_nozzle.timeout = 1600
supersonic_nozzle.tol = 0.00001
test_list.append(square_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.110240, 2.263506, 0.008686, 0.029098] #last 4 columns
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.191618, -5.592802, 0.334809, 0.022197] #last 4 columns
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.711318, 3.913749, -0.252131, 0.044402] #last 4 columns
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.393130, -12.928941, 0.282557, 0.012706] #last 4 columns
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231916, 0.261866, -0.166832, 0.012717] #last 4 columns
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765426, -1.297422, 0.019496, 0.310082] #last 4 columns
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.442524, -5.441383, 0.884279, 0.024730] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.185243, 4.018464, 0.886786, 0.024927] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.069447, -7.354601, -0.187187, 0.010831] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438, 0.155815]#last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D results for finest grid: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000763, -9.145363, 1.070528, 0.019417] #last 4 columns
turb_naca0012_sa.su2_exec = "SU2_CFD"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D results for finest grid: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039675, -7.219913, 1.059622, 0.019138] #last 4 columns
turb_naca0012_sst.su2_exec = "SU2_CFD"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710052, -11.007500, -0.000001, 0.210445] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.787554, -15.192510, 0.300920, 0.536870] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.133352, -12.707213, 6.8590e-01, 1.4092e-01] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.677184, -9.141850, -2.056700, 4.497000] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.229160] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.620880] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, -19.169000, -2.994100] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.377843, -10.882446, -0.212470, 0.269390] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.980272, -12.146779, 1.9399, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718622, -7.027366, -2.932100, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.643029, 2.849441, -4.443852, 0.000313] #last 4 columns
ramc.su2_exec = "SU2_CFD"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.627934, -0.164470, 0.051972, 2.547034] #last 4 columns
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.709662, -2.274900, 1.418422, 1.734206] #last 4 columns
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.544603, 0.048578, 1.398951, 2.196894] #last 4 columns
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.006222, -0.001342] #last 4 columns
sine_gust.su2_exec = "SU2_CFD"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077106, 0.036449, -1.684915e-03, -1.131746e-04] #last 4 columns
aeroelastic.su2_exec = "SU2_CFD"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# ls89_sa
ls89_sa = TestCase('ls89_sa')
ls89_sa.cfg_dir = "nicf/LS89"
ls89_sa.cfg_file = "turb_SA_PR.cfg"
ls89_sa.test_iter = 100
ls89_sa.test_vals = [-6.383146, -13.350551, 0.069079, 0.160886] #last 4 columns
ls89_sa.su2_exec = "SU2_CFD"
ls89_sa.timeout = 1600
ls89_sa.tol = 0.00001
test_list.append(ls89_sa)
# # ls89_sst
# ls89_sst = TestCase('ls89_sst')
# ls89_sst.cfg_dir = "nicf/LS89"
# ls89_sst.cfg_file = "turb_SST_PR.cfg"
# ls89_sst.test_iter = 100
# ls89_sst.test_vals = [-8.548266, -1.449437, 0.067986, 0.151168] #last 4 columns
# ls89_sst.su2_exec = "SU2_CFD"
# ls89_sst.timeout = 1600
# ls89_sst.tol = 0.00001
# test_list.append(ls89_sst)
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-1.448387, 4.749040, -0.000046, 0.000000] #last 4 columns
edge_VW.su2_exec = "SU2_CFD"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-1.998340, 4.172354, -0.000056, 0.000000] #last 4 columns
edge_PPR.su2_exec = "SU2_CFD"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
# Tests summary
print '=================================================================='
print 'Summary of the serial tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s'%test.tag
else:
print '* FAILED - %s'%test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606841, -9.035214, -0.000000, 0.005688] #last 4 columns
discadj_naca0012.su2_exec = "parallel_computation.py -f"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.720476, -4.039256, 0.000000, 0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "parallel_computation.py -f"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-1.751965, 0.485796, 0.182895, -0.000018] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-1.654193, -0.499281, 0.145545, -0.000018] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [-2.917789, -2.714752, 0.000000, 0.000000] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder_disc.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [-2.727423, -2.272530, 0.000000, 0.000000] #last 4 columns
discadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012
discadj_incomp_turb_NACA0012 = TestCase('discadj_incomp_turb_NACA0012')
discadj_incomp_turb_NACA0012.cfg_dir = "incomp_rans/naca0012"
discadj_incomp_turb_NACA0012.cfg_file = "naca0012_disc.cfg"
discadj_incomp_turb_NACA0012.test_iter = 100
discadj_incomp_turb_NACA0012.test_vals = [-3.645810, -1.625922, 0.000000, 0.000000] #last 4 columns
discadj_incomp_turb_NACA0012.su2_exec = "parallel_computation.py -f"
discadj_incomp_turb_NACA0012.timeout = 1600
discadj_incomp_turb_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746900, -1.544893, -8.3447e-03, 1.3808e-05] #last 4 columns
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
#######################################################
### Disc. adj. turbomachinery ###
#######################################################
# Transonic Stator 2D
discadj_trans_stator = TestCase('transonic_stator')
discadj_trans_stator.cfg_dir = "disc_adj_turbomachinery/transonic_stator_2D"
discadj_trans_stator.cfg_file = "transonic_stator.cfg"
discadj_trans_stator.test_iter = 79
discadj_trans_stator.test_vals = [-2.001081, -2.115303, -0.450996, -15.778175] #last 4 columns
discadj_trans_stator.su2_exec = "parallel_computation.py -f"
discadj_trans_stator.timeout = 1600
discadj_trans_stator.tol = 0.00001
test_list.append(discadj_trans_stator)
###################################
### Structural Adjoint ###
###################################
# Turbulent Cylinder
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 9
discadj_fea.test_vals = [-4.872191, -5.131614, -3.6413e-04, -8.7087e+00] #last 4 columns
discadj_fea.su2_exec = "parallel_computation.py -f"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Coupled FSI Adjoint ###
###################################
# Structural model
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "configAD_fsi.cfg"
discadj_fsi.test_iter = 3000
discadj_fsi.test_vals = [0.958848,-0.157183,0.658415,1.302076] #last 4 columns
discadj_fsi.su2_exec = "parallel_computation.py -f"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
# Tests summary
print('==================================================================')
print('Summary of the parallel tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s'%test.tag)
else:
print('* FAILED - %s'%test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.559002, -8.926022, -0.000000,
0.005588] #last 4 columns
discadj_naca0012.su2_exec = "parallel_computation.py -f"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.755976, -3.858734, 0.000000,
0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "parallel_computation.py -f"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
# Arina nozzle 2D
discadj_arina2k = TestCase('discadj_arina2k')
discadj_arina2k.cfg_dir = "disc_adj_euler/arina2k"
discadj_arina2k.cfg_file = "Arina2KRS.cfg"
discadj_arina2k.test_iter = 20
discadj_arina2k.test_vals = [2.190119, 1.635847, 47258.0,
0.0] #last 4 columns
discadj_arina2k.su2_exec = "parallel_computation.py -f"
discadj_arina2k.timeout = 8400
discadj_arina2k.tol = 0.00001
test_list.append(discadj_arina2k)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [
-2.230573, 0.696562, 0.181780, -0.000018
] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [
-2.221040, -0.491759, 0.557480, 0.000027
] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "disc_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [20.0, -4.107713, -2.670916,
0.0] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder (Heated)
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "disc_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "heated_cylinder.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [
20.000000, -2.188743, -2.068616, 0.000000
] #last 4 columns
discadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012 SA
discadj_incomp_turb_NACA0012_sa = TestCase(
'discadj_incomp_turb_NACA0012_sa')
discadj_incomp_turb_NACA0012_sa.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sa.cfg_file = "turb_naca0012_sa.cfg"
discadj_incomp_turb_NACA0012_sa.test_iter = 10
discadj_incomp_turb_NACA0012_sa.test_vals = [
10.000000, -3.846036, -1.031071, 0.000000
] #last 4 columns
discadj_incomp_turb_NACA0012_sa.su2_exec = "parallel_computation.py -f"
discadj_incomp_turb_NACA0012_sa.timeout = 1600
discadj_incomp_turb_NACA0012_sa.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sa)
# Adjoint Incompressible Turbulent NACA 0012 SST
discadj_incomp_turb_NACA0012_sst = TestCase(
'discadj_incomp_turb_NACA0012_sst')
discadj_incomp_turb_NACA0012_sst.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sst.cfg_file = "turb_naca0012_sst.cfg"
discadj_incomp_turb_NACA0012_sst.test_iter = 10
discadj_incomp_turb_NACA0012_sst.test_vals = [
-3.845624, -2.413044, -8.419978, 0.000000
] #last 4 columns
discadj_incomp_turb_NACA0012_sst.su2_exec = "parallel_computation.py -f"
discadj_incomp_turb_NACA0012_sst.timeout = 1600
discadj_incomp_turb_NACA0012_sst.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746909, -1.544883, -0.008321,
0.000014] #last 4 columns
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##############################################################
### Unsteady Disc. adj. compressible RANS Windowed Average ###
##############################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder_windowed_average_AD')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder_Windowing_AD.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.004406] #last column
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##############################################################
### Unsteady Disc. adj. compressible RANS Windowed Average ###
##############################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder_windowed_average')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder_Windowing.cfg"
discadj_cylinder.test_iter = 6
discadj_cylinder.test_vals = [
0.202376, -0.000030, 2.688758, -0.000032, 1.0679e+00
] #last 5 columns
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.0001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##########################################################################
### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order ###
##########################################################################
# Turbulent Cylinder
discadj_DT_1ST_cylinder = TestCase('unsteady_cylinder_DT_1ST')
discadj_DT_1ST_cylinder.cfg_dir = "disc_adj_rans/cylinder_DT_1ST"
discadj_DT_1ST_cylinder.cfg_file = "cylinder.cfg"
discadj_DT_1ST_cylinder.test_iter = 9
discadj_DT_1ST_cylinder.test_vals = [
3.698168, -1.607050, -0.002159, 0.000028
] #last 4 columns
discadj_DT_1ST_cylinder.su2_exec = "parallel_computation.py -f"
discadj_DT_1ST_cylinder.timeout = 1600
discadj_DT_1ST_cylinder.tol = 0.00001
discadj_DT_1ST_cylinder.unsteady = True
test_list.append(discadj_DT_1ST_cylinder)
######################################################
### Unsteady Disc. adj. compressible pitching NACA ###
######################################################
# compressible pitching NACA0012
discadj_pitchingNACA0012 = TestCase('pitchingNACA0012')
discadj_pitchingNACA0012.cfg_dir = "disc_adj_euler/naca0012_pitching"
discadj_pitchingNACA0012.cfg_file = "inv_NACA0012_pitching.cfg"
discadj_pitchingNACA0012.test_iter = 4
discadj_pitchingNACA0012.test_vals = [
-1.225570, -1.643131, -0.007597, 0.000013
] #last 4 columns
discadj_pitchingNACA0012.su2_exec = "parallel_computation.py -f"
discadj_pitchingNACA0012.timeout = 1600
discadj_pitchingNACA0012.tol = 0.00001
discadj_pitchingNACA0012.unsteady = True
test_list.append(discadj_pitchingNACA0012)
#######################################################
### Disc. adj. turbomachinery ###
#######################################################
# Transonic Stator 2D
discadj_trans_stator = TestCase('transonic_stator')
discadj_trans_stator.cfg_dir = "disc_adj_turbomachinery/transonic_stator_2D"
discadj_trans_stator.cfg_file = "transonic_stator.cfg"
discadj_trans_stator.test_iter = 79
discadj_trans_stator.test_vals = [79.000000, -1.942123,
-1.998834] #last 4 columns
discadj_trans_stator.su2_exec = "parallel_computation.py -f"
discadj_trans_stator.timeout = 1600
discadj_trans_stator.tol = 0.00001
test_list.append(discadj_trans_stator)
###################################
### Structural Adjoint ###
###################################
# Structural model
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 4
discadj_fea.test_vals = [-2.849526, -3.238467, -3.6413e-04,
-8.7087] #last 4 columns
discadj_fea.su2_exec = "parallel_computation.py -f"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Disc. adj. heat ###
###################################
# Discrete adjoint for heated cylinder
discadj_heat = TestCase('discadj_heat')
discadj_heat.cfg_dir = "disc_adj_heat"
discadj_heat.cfg_file = "disc_adj_heat.cfg"
discadj_heat.test_iter = 10
discadj_heat.test_vals = [-2.281765, 0.706808, -0.743990,
-6.866000] #last 4 columns
discadj_heat.su2_exec = "parallel_computation.py -f"
discadj_heat.timeout = 1600
discadj_heat.tol = 0.00001
test_list.append(discadj_heat)
###################################
### Coupled FSI Adjoint ###
###################################
# Legacy driver
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "config.cfg"
discadj_fsi.test_iter = 6
discadj_fsi.test_vals = [6, -1.563852, -3.075167, 4.3991e-04,
-1.0631] #last 5 columns
discadj_fsi.su2_exec = "mpirun -n 2 SU2_CFD_AD"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
# Multi physics framework
discadj_fsi2 = TestCase('discadj_fsi_airfoil')
discadj_fsi2.cfg_dir = "disc_adj_fsi/Airfoil_2d"
discadj_fsi2.cfg_file = "config.cfg"
discadj_fsi2.test_iter = 8
discadj_fsi2.test_vals = [-5.320965, -2.4380e-13] #last 2 columns
discadj_fsi2.su2_exec = "mpirun -n 2 SU2_CFD_AD"
discadj_fsi2.timeout = 1600
discadj_fsi2.tol = 1e-16
test_list.append(discadj_fsi2)
###################################
### Coupled CHT Adjoint ###
###################################
# Coupled discrete adjoint for heatflux in heated cylinder array
discadj_cht = TestCase('discadj_cht')
discadj_cht.cfg_dir = "coupled_cht/disc_adj_incomp_2d"
discadj_cht.cfg_file = "cht_2d_3cylinders.cfg"
discadj_cht.test_iter = 10
discadj_cht.test_vals = [-2.381654, -3.099873, -3.099844,
-3.099841] #last 4 columns
discadj_cht.su2_exec = "mpirun -n 2 SU2_CFD_AD"
discadj_cht.timeout = 1600
discadj_cht.tol = 0.00001
test_list.append(discadj_cht)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
##################################################
### Structural Adjoint - Topology Optimization ###
##################################################
# test discrete_adjoint.py
discadj_topol_optim = TestCase('discadj_topol_optim')
discadj_topol_optim.cfg_dir = "fea_topology"
discadj_topol_optim.cfg_file = "config.cfg"
discadj_topol_optim.test_iter = 0
discadj_topol_optim.su2_exec = "parallel_computation.py -f"
discadj_topol_optim.timeout = 1600
discadj_topol_optim.reference_file = "grad_ref_node.dat.ref"
discadj_topol_optim.test_file = "grad_ref_node.dat"
pass_list.append(discadj_topol_optim.run_filediff())
test_list.append(discadj_topol_optim)
####################################################################################
### Unsteady Disc. adj. compressible RANS Windowed Average with restart solution ###
####################################################################################
# NACA0012 Airfoil
unsteady_naca0012 = TestCase('unsteady_NACA0012_restart_adjoint')
unsteady_naca0012.cfg_dir = "disc_adj_rans/naca0012"
unsteady_naca0012.cfg_file = "naca0012.cfg"
unsteady_naca0012.test_iter = 14
unsteady_naca0012.su2_exec = "discrete_adjoint.py -f"
unsteady_naca0012.timeout = 1600
unsteady_naca0012.reference_file = "of_grad_cd.csv.ref"
unsteady_naca0012.test_file = "of_grad_cd.csv"
unsteady_naca0012.unsteady = True
pass_list.append(unsteady_naca0012.run_filediff())
test_list.append(unsteady_naca0012)
####################################################################################
### Unsteady Disc. adj. compressible RANS Windowed Average only adjoint ###
####################################################################################
# NACA0012 Airfoil (Test depends on results of "unsteady_NACA0012_restart_adjoint")
unsteady_naca0012 = TestCase('unsteady_NACA0012_adjoint_only')
unsteady_naca0012.cfg_dir = "disc_adj_rans/naca0012"
unsteady_naca0012.cfg_file = "naca0012.cfg"
unsteady_naca0012.test_iter = 14
unsteady_naca0012.su2_exec = "discrete_adjoint.py -m adj -f"
unsteady_naca0012.timeout = 1600
unsteady_naca0012.reference_file = "of_grad_cd.csv.ref"
unsteady_naca0012.test_file = "of_grad_cd.csv"
unsteady_naca0012.unsteady = True
pass_list.append(unsteady_naca0012.run_filediff())
test_list.append(unsteady_naca0012)
####################################################################
### Unsteady Disc. adj. compressible RANS restart optimization ###
####################################################################
# test shape_optimization.py
naca_restart_shape_opt = TestCase('restart_shape_optimization')
naca_restart_shape_opt.cfg_dir = "optimization_rans/naca0012"
naca_restart_shape_opt.cfg_file = "naca0012.cfg"
naca_restart_shape_opt.test_iter = 1
naca_restart_shape_opt.test_vals = [
1.000000, 1.000000, 0.007046, 0.196883
] #last 4 columns
naca_restart_shape_opt.su2_exec = "shape_optimization.py -f"
naca_restart_shape_opt.timeout = 1600
naca_restart_shape_opt.tol = 0.00001
pass_list.append(naca_restart_shape_opt.run_opt())
test_list.append(naca_restart_shape_opt)
# Tests summary
print('==================================================================')
print('Summary of the parallel tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s' % test.tag)
else:
print('* FAILED - %s' % test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git pull')
# Build SU2_CFD in serial using autoconf
os.system('./configure --prefix=$SU2_HOME CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.489214,2.821231,0.008730,0.053947]
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.203359,-5.582393,0.334818,0.022197]
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-2.703316,3.192215,-0.252410,0.044446]
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.830417,-4.273125,0.290066,0.015809]
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.227537,0.267007,-0.167233,0.012854]
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.764866,-1.296840,-0.024986,0.974669]
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.542705,-5.430675,0.884353,0.024153] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.214015,4.020029,0.884881,0.024141] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.068405,-7.340795,-0.187223,0.010395] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327517,-6.563378,0.230436,0.155816]#last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.826334,-7.364207,-0.000025,0.803037] #last 4 columns
turb_naca0012.su2_exec = "SU2_CFD"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709986,-11.007545,0.000008,0.210347] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-12.206764,-16.000000,0.005483,0.536870] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.353629,-6.525887,-0.000023,0.147720] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-0.599698,-6.065249,-0.032305,25.115000] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-4.234330,-9.705736,0.005161,0.398940 ] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.810435,-6.920519,0.014614,1.020100] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-4.351102,-8.919996,-1.275200,-2.541400] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-2.870304,-8.350308,4.5270e+00,3.5527e-01] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [-7.551025,-7.377690,0.010910,0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-2.423636,-2.916834,-0.048414,0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119,2.854417,-4.439628,0.000188]
ramc.su2_exec = "SU2_CFD"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.940515,-0.480469,0.018068,-3.926360]
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.744370,-1.298814,8.697757,0.133608]
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.542160,0.048661,1.398952,2.196894 ]
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# Build SU2_CFD in serial using autoconf
os.system('./configure --prefix=$SU2_HOME CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.110240, 2.263506, 0.008686, 0.029098]
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.198537, -5.577721, 0.334810, 0.022197]
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.711318, 3.913749, -0.252131, 0.044402]
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.711345, -4.145530, 0.271737, 0.018904]
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.228462, 0.265581, -0.166503, 0.013013]
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765426, -1.297422, 0.019501, 0.310134]
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.442525, -5.441383, 0.884279, 0.024730] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.186943, 4.023140, 0.886788, 0.024927] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.067553, -7.354291, -0.187192, 0.010831] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327516, -6.563376, 0.230437, 0.155816]#last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.826358, -7.364211, -0.000020, 0.803040] #last 4 columns
turb_naca0012.su2_exec = "SU2_CFD"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710052, -11.007500, -0.000001, 0.210445] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-12.208788, -17.722752, 0.300920, 0.536870] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.356212, -6.530823, -0.132860, 0.147720] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-0.607160, -6.072872, -2.056900, 25.115000] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-4.234330, -9.705735, 0.516750, 0.398940] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.810435, -6.920519, 1.756200, 1.020100] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-4.351102, -8.919996, -72.511000, -2.541400] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-2.959224, -8.349094, 354.120000, 0.106450] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [-7.326112, -7.153756, 1.892600, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-2.423970, -2.907687, -3.082900, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119, 2.854417, -4.439628, 0.000188]
ramc.su2_exec = "SU2_CFD"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.627883, -0.164418, 0.051983, 2.546202]
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.905504, -1.452746, 9.120908, 0.087763]
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.542156, 0.048662, 1.398952, 2.196893]
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### Real_Gas ###
######################################
# ls89_sa
ls89_sa = TestCase('ls89_sa')
ls89_sa.cfg_dir = "nicf/LS89"
ls89_sa.cfg_file = "turb_SA_PR.cfg"
ls89_sa.test_iter = 100
ls89_sa.test_vals = [-7.038263, -11.990177, 0.068730, 0.152379]
ls89_sa.su2_exec = "SU2_CFD"
ls89_sa.timeout = 1600
ls89_sa.tol = 0.00001
test_list.append(ls89_sa)
# ls89_sst
ls89_sst = TestCase('ls89_sst')
ls89_sst.cfg_dir = "nicf/LS89"
ls89_sst.cfg_file = "turb_SST_PR.cfg"
ls89_sst.test_iter = 100
ls89_sst.test_vals = [-8.906245, -1.629702, 0.068978, 0.153799]
ls89_sst.su2_exec = "SU2_CFD"
ls89_sst.timeout = 1600
ls89_sst.tol = 0.00001
test_list.append(ls89_sst)
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.728637, -3.272400, -0.000046, 0.000000]
edge_VW.su2_exec = "SU2_CFD"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-6.254324, -3.823322, -0.002054, 0.000000]
edge_PPR.su2_exec = "SU2_CFD"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# Build SU2_CFD in parallel using autoconf
os.system('./configure --prefix=$SU2_HOME --with-MPI=mpicxx CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.007228, 2.358896, 0.008339, 0.028541]
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.157022, -5.537399, 0.334831, 0.022209]
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.647184, 3.989725, -0.251604, 0.044317]
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.707461, -4.138449, 0.269324, 0.018891]
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.232930, 0.260877, -0.166066, 0.013093]
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.759579, -1.292062, 0.047262, 0.139916]
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.454436, -5.440827, 0.892572, 0.024842] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.178534, 4.029258, 0.894386, 0.024992] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.057092, -7.373256, -0.187140, 0.011347] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327515, -6.563376, 0.230436, 0.155816] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.826376, -7.364213, -0.000093, 0.803146] #last 4 columns
turb_naca0012.su2_exec = "parallel_computation.py -f"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709973, -11.007322, -0.000001, 0.211093] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-12.168676, -17.674195, 0.300920, 0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.354703, -6.527803, -0.133910, 0.147720] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-0.585239, -6.048475, -2.056900, 25.115000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-4.234330, -9.705735, 0.516750, 0.398940] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.810435, -6.920519, 1.756200, 1.020100] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-4.351102, -8.919996, -72.511000, -2.541400] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-2.903360, -8.331847, 354.020000, 0.128700] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [-7.275605, -7.111247, 1.892600, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-2.471344, -2.947390, -3.086500, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
# RAM-C II Sphere-Cone -- 61km Altitude
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119, 2.854417, -4.439628, 0.000188]
ramc.su2_exec = "parallel_computation.py -f"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.569056, -0.103736, 0.465430, 0.399409]
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.601720, -1.146034, 8.586054, 0.271493]
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.542156, 0.048663, 1.398952, 2.196894]
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### Real_Gas ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.723975, -3.267743, -0.000046, 0.000000]
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-6.275801, -3.846499, -0.000056, 0.000000]
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git pull')
# Build SU2_CFD in parallel using autoconf
os.system('./configure --prefix=$SU2_HOME --with-MPI=mpicxx CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.413846,2.965840,0.007590,0.051651]
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.145865,-5.547701,0.334821,0.022211]
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-2.694577,3.148295,-0.252137,0.044398]
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.825465,-4.290835,0.287910,0.015977]
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.232884,0.263297,0.020756,0.012889]
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.764733,-1.319817,0.096432,-1.542095]
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822
rae2822 = TestCase('rae2822')
rae2822.cfg_dir = "rans/rae2822"
rae2822.cfg_file = "turb_SA_RAE2822.cfg"
rae2822.test_iter = 100
rae2822.test_vals = [-3.650797,-5.455693,0.886602,0.024346 ] #last 4 columns
rae2822.su2_exec = "parallel_computation.py -f"
rae2822.timeout = 1600
rae2822.tol = 0.00001
test_list.append(rae2822)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.079817,-7.339735,0.000536,0.010776] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.343660,-6.584582,0.230390,0.155770] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.824685,-7.364142,-0.000065,0.803140] #last 4 columns
turb_naca0012.su2_exec = "parallel_computation.py -f"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709959,-11.007389,0.000012,0.211081] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012 (To be validated with finite differences)
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-10.108904,-15.604585,0.006153,0.522960] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.385873,-6.531040,-0.000023,0.147770] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-0.236174,-5.631193,0.031920,25.060000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012
contadj_ns_naca0012 = TestCase('contadj_ns_naca0012')
contadj_ns_naca0012.cfg_dir = "cont_adj_navierstokes/naca0012"
contadj_ns_naca0012.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012.test_iter = 100
contadj_ns_naca0012.test_vals = [-4.686123,-10.145232,0.013057,0.184800] #last 4 columns
contadj_ns_naca0012.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012.timeout = 1600
contadj_ns_naca0012.tol = 0.00001
test_list.append(contadj_ns_naca0012)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012 (To be validated with finite differences)
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-4.351187,-8.921444,1.181000,-2.540200] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [-7.613876,-7.157641,0.011112,0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-9.002264,-10.002274,0.048091,0.000000 ] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
# RAM-C II Sphere-Cone -- 61km Altitude
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119,2.854417,-4.439634,0.000188]
ramc.su2_exec = "parallel_computation.py -f"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.756437,-0.316355,-0.152010,-3.755979]
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.629674,-1.200221,8.693302,0.326125]
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.585044,-1.425751,1.490389,2.340439]
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['TEST_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work'
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync Test Cases repo
os.chdir( os.environ['TEST_HOME'] )
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# Build SU2_CFD in parallel using autoconf
os.system('./configure --prefix=$SU2_HOME --enable-mpi --with-cc=`which mpicc` --with-cxx=`which mpicxx` CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.984481, 2.389875, 0.008865, 0.027854] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.702502, 3.923373, -0.252116, 0.044396] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.701280, -4.154921, 0.270257, 0.019095] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.233923, 0.259801, -0.166790, 0.012722] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948, 0.625438] #last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.637762, -5.450251, 0.890401, 0.025056] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.217020, 4.023774, 0.892665, 0.025209] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.061518, -7.362119, -0.187139, 0.011230] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327508, -6.563372, 0.230438, 0.155815] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 20
turb_naca0012_sa.test_vals = [-6.607223, -9.778334, 1.098508, 0.012417] #last 4 columns
turb_naca0012_sa.su2_exec = "parallel_computation.py -f"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 20
turb_naca0012_sst.test_vals = [-8.290777, -1.743118, 1.084186, 0.012583] #last 4 columns
turb_naca0012_sst.su2_exec = "parallel_computation.py -f"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709508, -11.006161, -0.000017, 0.211696] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.783724, -15.192804, 0.300920, 0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.001400, -6.242615, -0.105160, 0.149240] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.658396, -9.117436, -2.056700, 4.497000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.229160] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.620880] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, -19.169000, -2.994100] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.381632, -10.887032, -0.212470, 0.269390] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.968536, -12.133234, 1.939900, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718776, -7.020714, -2.932100, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
# RAM-C II Sphere-Cone -- 61km Altitude
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.643029, 2.849441, -4.443852, 0.000313] #last 4 columns
ramc.su2_exec = "parallel_computation.py -f"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.594283, -0.130745, -0.510607, 0.061921] #last 4 columns
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.637313, -2.194229, 1.212769, 1.605369] #last 4 columns
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.544602, 0.048576, 1.398951, 2.196894] #last 4 columns
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### Real_Gas ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-1.446069, 4.751345, -0.000046, 0.000000] #last 4 columns
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-1.994951, 4.175777, -0.000056, 0.000000] #last 4 columns
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.071007, 2.301191, 0.008562,
0.028922] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843,
0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.690232, 3.924432, -0.252221,
0.044419] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.400678, -12.932056, 0.282557,
0.012706] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231743, 0.261628, -0.166871,
0.012706] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948,
0.625438] #last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase('cylinder_lowmach')
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.861860, -1.399846, -1.557250,
110.230719] #last 4 columns
cylinder_lowmach.su2_exec = "parallel_computation.py -f"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.647743, -5.442583, 0.903159,
0.025800] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.198777, 4.013989, 0.904265,
0.025941] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.071289, -7.366446, -0.187145,
0.010957] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438,
0.155815] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000764, -9.145363, 1.070528,
0.019417] #last 4 columns
turb_naca0012_sa.su2_exec = "parallel_computation.py -f"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039645, -7.220177, 1.059622,
0.019138] #last 4 columns
turb_naca0012_sst.su2_exec = "parallel_computation.py -f"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710048, -11.007498, 0.000002,
0.210441] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.783712, -15.192812, 0.300920,
0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.131587, -12.703243, 0.685900,
0.140920] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
# Inviscid WEDGE: generalized adjoint and custom DV
contadj_wedge = TestCase('contadj_wedge')
contadj_wedge.cfg_dir = "cont_adj_euler/wedge"
contadj_wedge.cfg_file = "inv_wedge_ROE.cfg"
contadj_wedge.test_iter = 10
contadj_wedge.test_vals = [-7.364977, -13.301134, 0.000266,
0.000000] #last 4 columns
contadj_wedge.su2_exec = "parallel_computation.py -f"
contadj_wedge.timeout = 1600
contadj_wedge.tol = 0.00001
test_list.append(contadj_wedge)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [
-3.659040, -9.117773, -2.056700, 4.497000
] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [
-2.744551, -8.216469, 0.518810, 0.229160
] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [
-1.041539, -6.578524, 1.772300, 0.620880
] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [
-0.814757, -5.726517, -19.169000, -2.994100
] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [
-5.380929, -10.886092, -0.212470, 0.269390
] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [
-11.968536, -12.133235, 1.939900, 0.000000
] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [
-5.718840, -7.012324, -2.932100, 0.000000
] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.597018, -0.133158, 0.169034,
0.821371] #last 4 columns
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.648320, -2.202753, 1.236836,
1.609040] #last 4 columns
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.544602, 0.048576, 1.398951,
2.196894] #last 4 columns
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.014552,
-0.004969] #last 4 columns
sine_gust.su2_exec = "parallel_computation.py -f"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077169, 0.036452, -0.001685,
-0.000113] #last 4 columns
aeroelastic.su2_exec = "parallel_computation.py -f"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.058481, 1.115321, -0.000009,
0.000000] #last 4 columns
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.486409, 0.654417, -0.000037,
0.000000] #last 4 columns
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase('statbeam3d')
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-8.520066, -8.069308, -8.062384,
64095.000000] #last 4 columns
statbeam3d.su2_exec = "parallel_computation_fsi.py -f"
statbeam3d.timeout = 1600
statbeam3d.tol = 0.00001
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase('dynbeam2d')
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-9.420641, -5.365871, -12.430382,
6.5210e+04] #last 4 columns
dynbeam2d.su2_exec = "parallel_computation_fsi.py -f"
dynbeam2d.timeout = 1600
dynbeam2d.tol = 0.00001
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase('fsi2d')
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI_2D.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [2, 0.500000, -7.779707, -1.141608] #last 4 columns
fsi2d.su2_exec = "parallel_computation_fsi.py -f"
fsi2d.timeout = 1600
fsi2d.tol = 0.00001
test_list.append(fsi2d)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
# Tests summary
print '=================================================================='
print 'Summary of the parallel tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s' % test.tag
else:
print '* FAILED - %s' % test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ[
'TEST_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work'
os.environ[
'SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ[
'SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync Test Cases repo
os.chdir(os.environ['TEST_HOME'])
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# sync SU2 repo
os.chdir(os.environ['SU2_HOME'])
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# Build SU2_CFD in parallel using autoconf
os.system(
'./configure --prefix=$SU2_HOME --enable-mpi --with-cc=`which mpicc` --with-cxx=`which mpicxx` CXXFLAGS="-O3"'
)
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.984481, 2.389875, 0.008865,
0.027854] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843,
0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.702502, 3.923373, -0.252116,
0.044396] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.701280, -4.154921, 0.270257,
0.019095] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.233923, 0.259801, -0.166790,
0.012722] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948,
0.625438] #last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.637762, -5.450251, 0.890401,
0.025056] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.217020, 4.023774, 0.892665,
0.025209] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.061518, -7.362119, -0.187139,
0.011230] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327508, -6.563372, 0.230438,
0.155815] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 20
turb_naca0012_sa.test_vals = [-6.607223, -9.778334, 1.098508,
0.012417] #last 4 columns
turb_naca0012_sa.su2_exec = "parallel_computation.py -f"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 20
turb_naca0012_sst.test_vals = [-8.290777, -1.743118, 1.084186,
0.012583] #last 4 columns
turb_naca0012_sst.su2_exec = "parallel_computation.py -f"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709508, -11.006161, -0.000017,
0.211696] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.783724, -15.192804, 0.300920,
0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.001400, -6.242615, -0.105160,
0.149240] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [
-3.658396, -9.117436, -2.056700, 4.497000
] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [
-2.744551, -8.216469, 0.518810, 0.229160
] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [
-1.041539, -6.578524, 1.772300, 0.620880
] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [
-0.814757, -5.726517, -19.169000, -2.994100
] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [
-5.381632, -10.887032, -0.212470, 0.269390
] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [
-11.968536, -12.133234, 1.939900, 0.000000
] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [
-5.718776, -7.020714, -2.932100, 0.000000
] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
# RAM-C II Sphere-Cone -- 61km Altitude
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.643029, 2.849441, -4.443852,
0.000313] #last 4 columns
ramc.su2_exec = "parallel_computation.py -f"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.594283, -0.130745, -0.510607,
0.061921] #last 4 columns
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.637313, -2.194229, 1.212769,
1.605369] #last 4 columns
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.544602, 0.048576, 1.398951,
2.196894] #last 4 columns
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### Real_Gas ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-1.446069, 4.751345, -0.000046,
0.000000] #last 4 columns
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-1.994951, 4.175777, -0.000056,
0.000000] #last 4 columns
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.984481, 2.389875, 0.008865,
0.027854] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843,
0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.702502, 3.923373, -0.252116,
0.044396] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.398374, -12.928436, 0.282557,
0.012706] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.233923, 0.259801, -0.166790,
0.012722] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948,
0.625438] #last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.637762, -5.450251, 0.890401,
0.025056] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.217020, 4.023774, 0.892665,
0.025209] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.073540, -7.354716, -0.187154,
0.011105] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438,
0.155815] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000764, -9.145363, 1.070528,
0.019417] #last 4 columns
turb_naca0012_sa.su2_exec = "parallel_computation.py -f"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039665, -7.220109, 1.059622,
0.019138] #last 4 columns
turb_naca0012_sst.su2_exec = "parallel_computation.py -f"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709508, -11.006161, -0.000017,
0.211696] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.783712, -15.192812, 0.300920,
0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.132862, -12.704820, 0.685900,
0.140920] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [
-3.658396, -9.117436, -2.056700, 4.497000
] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [
-2.744551, -8.216469, 0.518810, 0.229160
] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [
-1.041539, -6.578524, 1.772300, 0.620880
] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [
-0.814757, -5.726517, -19.169000, -2.994100
] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [
-5.381632, -10.887032, -0.212470, 0.269390
] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [
-11.968536, -12.133235, 1.939900, 0.000000
] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [
-5.718776, -7.020714, -2.932100, 0.000000
] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
# RAM-C II Sphere-Cone -- 61km Altitude
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.643029, 2.849441, -4.443852,
0.000313] #last 4 columns
ramc.su2_exec = "parallel_computation.py -f"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.594283, -0.130745, -0.510607,
0.061921] #last 4 columns
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.637313, -2.194229, 1.212769,
1.605369] #last 4 columns
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.544602, 0.048576, 1.398951,
2.196894] #last 4 columns
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.014552,
-0.004969] #last 4 columns
sine_gust.su2_exec = "parallel_computation.py -f"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077319, 0.036428, -1.685289e-03,
-1.129111e-04] #last 4 columns
aeroelastic.su2_exec = "parallel_computation.py -f"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-1.446201, 4.751213, -0.000046,
0.000000] #last 4 columns
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-1.995058, 4.175675, -0.000056,
0.000000] #last 4 columns
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
# Tests summary
print '=================================================================='
print 'Summary of the parallel tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s' % test.tag
else:
print '* FAILED - %s' % test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.071007, 2.301191, 0.008562, 0.028922] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.690232, 3.924432, -0.252221, 0.044419] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.400678, -12.932056, 0.282557, 0.012706] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231743, 0.261628, -0.166871, 0.012706] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948, 0.625438] #last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase('cylinder_lowmach')
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.861860, -1.399846, -1.557250, 110.230719] #last 4 columns
cylinder_lowmach.su2_exec = "parallel_computation.py -f"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.647743, -5.442583, 0.903159, 0.025800] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.198777, 4.013989, 0.904265, 0.025941] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.071289, -7.366446, -0.187145, 0.010957] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438, 0.155815] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000764, -9.145363, 1.070528, 0.019417] #last 4 columns
turb_naca0012_sa.su2_exec = "parallel_computation.py -f"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039645, -7.220177, 1.059622, 0.019138] #last 4 columns
turb_naca0012_sst.su2_exec = "parallel_computation.py -f"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710048, -11.007498, 0.000002, 0.210441] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.783712, -15.192812, 0.300920, 0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.131587, -12.703243, 0.685900, 0.140920] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
# Inviscid WEDGE: generalized adjoint and custom DV
contadj_wedge = TestCase('contadj_wedge')
contadj_wedge.cfg_dir = "cont_adj_euler/wedge"
contadj_wedge.cfg_file = "inv_wedge_ROE.cfg"
contadj_wedge.test_iter = 10
contadj_wedge.test_vals = [-7.364977, -13.301134, 0.000266, 0.000000] #last 4 columns
contadj_wedge.su2_exec = "parallel_computation.py -f"
contadj_wedge.timeout = 1600
contadj_wedge.tol = 0.00001
test_list.append(contadj_wedge)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.659040, -9.117773, -2.056700, 4.497000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.229160] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.620880] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, -19.169000, -2.994100] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.380929, -10.886092, -0.212470, 0.269390] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.968536, -12.133235, 1.939900, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718840, -7.012324, -2.932100, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.597018, -0.133158, 0.169034, 0.821371] #last 4 columns
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.648320, -2.202753, 1.236836, 1.609040] #last 4 columns
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.544602, 0.048576, 1.398951, 2.196894] #last 4 columns
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.014552, -0.004969] #last 4 columns
sine_gust.su2_exec = "parallel_computation.py -f"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077169, 0.036452, -0.001685, -0.000113] #last 4 columns
aeroelastic.su2_exec = "parallel_computation.py -f"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.058481, 1.115321, -0.000009, 0.000000] #last 4 columns
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.486409, 0.654417, -0.000037, 0.000000] #last 4 columns
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase('statbeam3d')
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-8.520066, -8.069308, -8.062384, 64095.000000] #last 4 columns
statbeam3d.su2_exec = "parallel_computation_fsi.py -f"
statbeam3d.timeout = 1600
statbeam3d.tol = 0.00001
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase('dynbeam2d')
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-9.420641, -5.365871, -12.430382, 6.5210e+04] #last 4 columns
dynbeam2d.su2_exec = "parallel_computation_fsi.py -f"
dynbeam2d.timeout = 1600
dynbeam2d.tol = 0.00001
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase('fsi2d')
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI_2D.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [2, 0.500000, -7.779707, -1.141608] #last 4 columns
fsi2d.su2_exec = "parallel_computation_fsi.py -f"
fsi2d.timeout = 1600
fsi2d.tol = 0.00001
test_list.append(fsi2d)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
# Tests summary
print '=================================================================='
print 'Summary of the parallel tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s'%test.tag
else:
print '* FAILED - %s'%test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
######################################
### RUN TUTORIAL CASES ###
######################################
### CHT
# CHT incompressible unsteady
cht_incompressible_unsteady = TestCase('cht_incompressible_unsteady')
cht_incompressible_unsteady.cfg_dir = "../Tutorials/multiphysics/unsteady_cht/"
cht_incompressible_unsteady.cfg_file = "cht_2d_3cylinders.cfg"
cht_incompressible_unsteady.test_iter = 2
cht_incompressible_unsteady.test_vals = [
-2.659390, -2.533160, -0.080399, -0.080399, -0.080399, -12.421450,
0.0000e+00, 0.0000e+00, 2.3824e+02
] #last 9 columns
cht_incompressible_unsteady.su2_exec = "mpirun -n 2 SU2_CFD"
cht_incompressible_unsteady.timeout = 1600
cht_incompressible_unsteady.multizone = True
cht_incompressible_unsteady.unsteady = True
cht_incompressible_unsteady.tol = 0.00001
test_list.append(cht_incompressible_unsteady)
# CHT incompressible, 2D, 3 pins in crossflow
cht_incompressible = TestCase('cht_incompressible')
cht_incompressible.cfg_dir = "../Tutorials/multiphysics/steady_cht"
cht_incompressible.cfg_file = "cht_2d_3cylinders.cfg"
cht_incompressible.test_iter = 10
cht_incompressible.test_vals = [
-2.128826, -0.588813, -0.588813, -0.588813
] #last 4 columns
cht_incompressible.su2_exec = "SU2_CFD"
cht_incompressible.timeout = 1600
cht_incompressible.multizone = True
cht_incompressible.tol = 0.00001
test_list.append(cht_incompressible)
### Incompressible Flow
# 2D pin case massflow periodic with heatflux BC and prescribed extracted outlet heat
sp_pinArray_2d_mf_hf = TestCase('sp_pinArray_2d_mf_hf')
sp_pinArray_2d_mf_hf.cfg_dir = "../Tutorials/incompressible_flow/Inc_Streamwise_Periodic"
sp_pinArray_2d_mf_hf.cfg_file = "sp_pinArray_2d_mf_hf.cfg"
sp_pinArray_2d_mf_hf.test_iter = 25
sp_pinArray_2d_mf_hf.test_vals = [
-4.600340, 1.470386, -0.778623, 266.569743
] #last 4 lines
sp_pinArray_2d_mf_hf.su2_exec = "mpirun -n 2 SU2_CFD"
sp_pinArray_2d_mf_hf.timeout = 1600
sp_pinArray_2d_mf_hf.tol = 0.00001
test_list.append(sp_pinArray_2d_mf_hf)
# 2D pin case pressure drop periodic with heatflux BC and temperature periodicity
sp_pinArray_2d_dp_hf_tp = TestCase('sp_pinArray_2d_dp_hf_tp')
sp_pinArray_2d_dp_hf_tp.cfg_dir = "../Tutorials/incompressible_flow/Inc_Streamwise_Periodic"
sp_pinArray_2d_dp_hf_tp.cfg_file = "sp_pinArray_2d_dp_hf_tp.cfg"
sp_pinArray_2d_dp_hf_tp.test_iter = 25
sp_pinArray_2d_dp_hf_tp.test_vals = [
-4.667133, 1.395801, -0.709306, 208.023676
] #last 4 lines
sp_pinArray_2d_dp_hf_tp.su2_exec = "mpirun -n 2 SU2_CFD"
sp_pinArray_2d_dp_hf_tp.timeout = 1600
sp_pinArray_2d_dp_hf_tp.tol = 0.00001
test_list.append(sp_pinArray_2d_dp_hf_tp)
### Compressible Flow
# Inviscid Bump
tutorial_inv_bump = TestCase('inviscid_bump_tutorial')
tutorial_inv_bump.cfg_dir = "../Tutorials/compressible_flow/Inviscid_Bump"
tutorial_inv_bump.cfg_file = "inv_channel.cfg"
tutorial_inv_bump.test_iter = 0
tutorial_inv_bump.test_vals = [-1.437425, 4.075857, 0.005439, 0.012998]
tutorial_inv_bump.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_inv_bump.timeout = 1600
tutorial_inv_bump.tol = 0.00001
tutorial_inv_bump.no_restart = True
test_list.append(tutorial_inv_bump)
# Inviscid Wedge
tutorial_inv_wedge = TestCase('inviscid_wedge_tutorial')
tutorial_inv_wedge.cfg_dir = "../Tutorials/compressible_flow/Inviscid_Wedge"
tutorial_inv_wedge.cfg_file = "inv_wedge_HLLC.cfg"
tutorial_inv_wedge.test_iter = 0
tutorial_inv_wedge.test_vals = [-0.481460, 5.253008, -0.291747, 0.052515]
tutorial_inv_wedge.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_inv_wedge.timeout = 1600
tutorial_inv_wedge.tol = 0.00001
tutorial_inv_wedge.no_restart = True
test_list.append(tutorial_inv_wedge)
# Inviscid ONERA M6
tutorial_inv_onera = TestCase('inviscid_onera_tutorial')
tutorial_inv_onera.cfg_dir = "../Tutorials/compressible_flow/Inviscid_ONERAM6"
tutorial_inv_onera.cfg_file = "inv_ONERAM6.cfg"
tutorial_inv_onera.test_iter = 0
tutorial_inv_onera.test_vals = [-5.204928, -4.597762, 0.247451, 0.085770]
tutorial_inv_onera.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_inv_onera.timeout = 1600
tutorial_inv_onera.tol = 0.00001
tutorial_inv_onera.no_restart = True
test_list.append(tutorial_inv_onera)
# Laminar Cylinder
tutorial_lam_cylinder = TestCase('laminar_cylinder_tutorial')
tutorial_lam_cylinder.cfg_dir = "../Tutorials/compressible_flow/Laminar_Cylinder"
tutorial_lam_cylinder.cfg_file = "lam_cylinder.cfg"
tutorial_lam_cylinder.test_iter = 0
tutorial_lam_cylinder.test_vals = [
-6.162141, -0.699617, 0.125776, 69.613563
]
tutorial_lam_cylinder.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_lam_cylinder.timeout = 1600
tutorial_lam_cylinder.tol = 0.00001
tutorial_lam_cylinder.no_restart = True
test_list.append(tutorial_lam_cylinder)
# Laminar Flat Plate
tutorial_lam_flatplate = TestCase('laminar_flatplate_tutorial')
tutorial_lam_flatplate.cfg_dir = "../Tutorials/compressible_flow/Laminar_Flat_Plate"
tutorial_lam_flatplate.cfg_file = "lam_flatplate.cfg"
tutorial_lam_flatplate.test_iter = 0
tutorial_lam_flatplate.test_vals = [
-2.821818, 2.657591, -0.400044, 0.029413
] #last 4 columns
tutorial_lam_flatplate.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_lam_flatplate.timeout = 1600
tutorial_lam_flatplate.tol = 0.00001
tutorial_lam_flatplate.no_restart = True
test_list.append(tutorial_lam_flatplate)
# Turbulent Flat Plate
tutorial_turb_flatplate = TestCase('turbulent_flatplate_tutorial')
tutorial_turb_flatplate.cfg_dir = "../Tutorials/compressible_flow/Turbulent_Flat_Plate"
tutorial_turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
tutorial_turb_flatplate.test_iter = 0
tutorial_turb_flatplate.test_vals = [
-2.258584, -4.899502, -0.429375, 0.201236
]
tutorial_turb_flatplate.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_turb_flatplate.timeout = 1600
tutorial_turb_flatplate.tol = 0.00001
tutorial_turb_flatplate.no_restart = True
test_list.append(tutorial_turb_flatplate)
# Transitional FlatPlate
tutorial_trans_flatplate = TestCase('transitional_flatplate_tutorial')
tutorial_trans_flatplate.cfg_dir = "../Tutorials/compressible_flow/Transitional_Flat_Plate"
tutorial_trans_flatplate.cfg_file = "transitional_BC_model_ConfigFile.cfg"
tutorial_trans_flatplate.test_iter = 0
tutorial_trans_flatplate.test_vals = [
-22.021786, -15.330766, 0.000000, 0.023952
] #last 4 columns
tutorial_trans_flatplate.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_trans_flatplate.timeout = 1600
tutorial_trans_flatplate.tol = 0.00001
tutorial_trans_flatplate.no_restart = True
test_list.append(tutorial_trans_flatplate)
# Turbulent ONERA M6
tutorial_turb_oneram6 = TestCase('turbulent_oneram6_tutorial')
tutorial_turb_oneram6.cfg_dir = "../Tutorials/compressible_flow/Turbulent_ONERAM6"
tutorial_turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
tutorial_turb_oneram6.test_iter = 0
tutorial_turb_oneram6.test_vals = [
-4.564441, -11.524277, 0.327954, 0.097349
]
tutorial_turb_oneram6.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_turb_oneram6.timeout = 1600
tutorial_turb_oneram6.tol = 0.00001
test_list.append(tutorial_turb_oneram6)
# NICD Nozzle
tutorial_nicfd_nozzle = TestCase('nicfd_nozzle')
tutorial_nicfd_nozzle.cfg_dir = "../Tutorials/compressible_flow/NICFD_nozzle"
tutorial_nicfd_nozzle.cfg_file = "NICFD_nozzle.cfg"
tutorial_nicfd_nozzle.test_iter = 20
tutorial_nicfd_nozzle.test_vals = [
-2.187400, -9.409241, 3.477513, 0.000000, 0.000000
]
tutorial_nicfd_nozzle.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_nicfd_nozzle.timeout = 1600
tutorial_nicfd_nozzle.tol = 0.00001
tutorial_nicfd_nozzle.no_restart = True
test_list.append(tutorial_nicfd_nozzle)
# Unsteady NACA0012
tutorial_unst_naca0012 = TestCase('unsteady_naca0012')
tutorial_unst_naca0012.cfg_dir = "../Tutorials/compressible_flow/Unsteady_NACA0012"
tutorial_unst_naca0012.cfg_file = "unsteady_naca0012.cfg"
tutorial_unst_naca0012.test_iter = 500
tutorial_unst_naca0012.test_vals = [
500, 0, 0.302003, 0.665069, -5.300141, 0.000000, 0.0000e+00, 0.0000e+00
]
tutorial_unst_naca0012.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_unst_naca0012.timeout = 1600
tutorial_unst_naca0012.tol = 0.00001
tutorial_unst_naca0012.unsteady = True
test_list.append(tutorial_unst_naca0012)
# PROPELLER VARIBLE LOAD
propeller_var_load = TestCase('propeller_variable_load')
propeller_var_load.cfg_dir = "../Tutorials/compressible_flow/ActuatorDisk_VariableLoad"
propeller_var_load.cfg_file = "propeller_variable_load.cfg"
propeller_var_load.test_iter = 20
propeller_var_load.test_vals = [-1.830252, -4.535038, -0.000323, 0.171648]
propeller_var_load.su2_exec = "mpirun -np 2 SU2_CFD"
propeller_var_load.timeout = 3200
propeller_var_load.tol = 0.00001
test_list.append(propeller_var_load)
### Design
# Inviscid NACA 0012 Design
tutorial_design_inv_naca0012 = TestCase('design_inv_naca0012')
tutorial_design_inv_naca0012.cfg_dir = "../Tutorials/design/Inviscid_2D_Unconstrained_NACA0012"
tutorial_design_inv_naca0012.cfg_file = "inv_NACA0012_basic.cfg"
tutorial_design_inv_naca0012.test_iter = 0
tutorial_design_inv_naca0012.test_vals = [
-3.585391, -2.989014, 0.135070, 0.208565
]
tutorial_design_inv_naca0012.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_design_inv_naca0012.timeout = 1600
tutorial_design_inv_naca0012.tol = 0.00001
tutorial_design_inv_naca0012.no_restart = True
test_list.append(tutorial_design_inv_naca0012)
# Turbulent RAE 2822 Design
tutorial_design_turb_rae2822 = TestCase('design_turb_rae2822')
tutorial_design_turb_rae2822.cfg_dir = "../Tutorials/design/Turbulent_2D_Constrained_RAE2822"
tutorial_design_turb_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
tutorial_design_turb_rae2822.test_iter = 0
tutorial_design_turb_rae2822.test_vals = [
-1.700114, -4.941305, 0.218348, 0.190357
]
tutorial_design_turb_rae2822.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_design_turb_rae2822.timeout = 1600
tutorial_design_turb_rae2822.tol = 0.00001
tutorial_design_turb_rae2822.no_restart = True
test_list.append(tutorial_design_turb_rae2822)
# Multi Objective Design
tutorial_design_multiobj = TestCase('design_multiobj')
tutorial_design_multiobj.cfg_dir = "../Tutorials/design/Multi_Objective_Shape_Design"
tutorial_design_multiobj.cfg_file = "inv_wedge_ROE_multiobj_combo.cfg"
tutorial_design_multiobj.test_iter = 0
tutorial_design_multiobj.test_vals = [
2.657333, -3.020635, 324840.000000, 0.000000
] #last 4 columns
tutorial_design_multiobj.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_design_multiobj.timeout = 1600
tutorial_design_multiobj.tol = 0.00001
tutorial_design_multiobj.no_restart = True
test_list.append(tutorial_design_multiobj)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
# Tests summary
print('==================================================================')
print('Summary of the parallel tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s' % test.tag)
else:
print('* FAILED - %s' % test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
######################################
### RUN TUTORIAL CASES ###
######################################
### Compressible Flow
# Inviscid Bump
tutorial_inv_bump = TestCase('inviscid_bump_tutorial')
tutorial_inv_bump.cfg_dir = "../Tutorials/compressible_flow/Inviscid_Bump"
tutorial_inv_bump.cfg_file = "inv_channel.cfg"
tutorial_inv_bump.test_iter = 0
tutorial_inv_bump.test_vals = [-1.437425, 4.075857, 0.003000,
0.012720] #last 4 columns
tutorial_inv_bump.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_inv_bump.timeout = 1600
tutorial_inv_bump.tol = 0.00001
tutorial_inv_bump.no_restart = True
test_list.append(tutorial_inv_bump)
# Inviscid Wedge
tutorial_inv_wedge = TestCase('inviscid_wedge_tutorial')
tutorial_inv_wedge.cfg_dir = "../Tutorials/compressible_flow/Inviscid_Wedge"
tutorial_inv_wedge.cfg_file = "inv_wedge_HLLC.cfg"
tutorial_inv_wedge.test_iter = 0
tutorial_inv_wedge.test_vals = [-0.481460, 5.253008, -0.292159,
0.052922] #last 4 columns
tutorial_inv_wedge.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_inv_wedge.timeout = 1600
tutorial_inv_wedge.tol = 0.00001
tutorial_inv_wedge.no_restart = True
test_list.append(tutorial_inv_wedge)
# Inviscid ONERA M6
tutorial_inv_onera = TestCase('inviscid_onera_tutorial')
tutorial_inv_onera.cfg_dir = "../Tutorials/compressible_flow/Inviscid_ONERAM6"
tutorial_inv_onera.cfg_file = "inv_ONERAM6.cfg"
tutorial_inv_onera.test_iter = 0
tutorial_inv_onera.test_vals = [-5.204928, -4.597762, 0.247124,
0.085734] #last 4 columns
tutorial_inv_onera.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_inv_onera.timeout = 1600
tutorial_inv_onera.tol = 0.00001
tutorial_inv_onera.no_restart = True
test_list.append(tutorial_inv_onera)
# Laminar Cylinder
tutorial_lam_cylinder = TestCase('laminar_cylinder_tutorial')
tutorial_lam_cylinder.cfg_dir = "../Tutorials/compressible_flow/Laminar_Cylinder"
tutorial_lam_cylinder.cfg_file = "lam_cylinder.cfg"
tutorial_lam_cylinder.test_iter = 0
tutorial_lam_cylinder.test_vals = [
-6.162141, -0.699617, 0.186570, 69.267308
] #last 4 columns
tutorial_lam_cylinder.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_lam_cylinder.timeout = 1600
tutorial_lam_cylinder.tol = 0.00001
tutorial_lam_cylinder.no_restart = True
test_list.append(tutorial_lam_cylinder)
# Laminar Flat Plate
tutorial_lam_flatplate = TestCase('laminar_flatplate_tutorial')
tutorial_lam_flatplate.cfg_dir = "../Tutorials/compressible_flow/Laminar_Flat_Plate"
tutorial_lam_flatplate.cfg_file = "lam_flatplate.cfg"
tutorial_lam_flatplate.test_iter = 0
tutorial_lam_flatplate.test_vals = [
-2.821818, 2.657591, -0.400044, 0.029413
] #last 4 columns
tutorial_lam_flatplate.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_lam_flatplate.timeout = 1600
tutorial_lam_flatplate.tol = 0.00001
tutorial_lam_flatplate.no_restart = True
test_list.append(tutorial_lam_flatplate)
# Turbulent Flat Plate
tutorial_turb_flatplate = TestCase('turbulent_flatplate_tutorial')
tutorial_turb_flatplate.cfg_dir = "../Tutorials/compressible_flow/Turbulent_Flat_Plate"
tutorial_turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
tutorial_turb_flatplate.test_iter = 0
tutorial_turb_flatplate.test_vals = [
-2.258584, -4.899502, -0.429387, 0.201236
] #last 4 columns
tutorial_turb_flatplate.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_turb_flatplate.timeout = 1600
tutorial_turb_flatplate.tol = 0.00001
tutorial_turb_flatplate.no_restart = True
test_list.append(tutorial_turb_flatplate)
# Transitional FlatPlate
tutorial_trans_flatplate = TestCase('transitional_flatplate_tutorial')
tutorial_trans_flatplate.cfg_dir = "../Tutorials/compressible_flow/Transitional_Flat_Plate"
tutorial_trans_flatplate.cfg_file = "transitional_BC_model_ConfigFile.cfg"
tutorial_trans_flatplate.test_iter = 0
tutorial_trans_flatplate.test_vals = [
-22.021786, -15.330906, 0.000000, 0.023952
] #last 4 columns
tutorial_trans_flatplate.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_trans_flatplate.timeout = 1600
tutorial_trans_flatplate.tol = 0.00001
tutorial_trans_flatplate.no_restart = True
test_list.append(tutorial_trans_flatplate)
# Turbulent ONERA M6
tutorial_turb_oneram6 = TestCase('turbulent_oneram6_tutorial')
tutorial_turb_oneram6.cfg_dir = "../Tutorials/compressible_flow/Turbulent_ONERAM6"
tutorial_turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
tutorial_turb_oneram6.test_iter = 0
tutorial_turb_oneram6.test_vals = [
-4.499497, -11.473637, 0.332666, 0.098280
] #last 4 columns
tutorial_turb_oneram6.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_turb_oneram6.timeout = 1600
tutorial_turb_oneram6.tol = 0.00001
test_list.append(tutorial_turb_oneram6)
# NICD Nozzle
tutorial_nicfd_nozzle = TestCase('nicfd_nozzle')
tutorial_nicfd_nozzle.cfg_dir = "../Tutorials/compressible_flow/NICFD_nozzle"
tutorial_nicfd_nozzle.cfg_file = "NICFD_nozzle.cfg"
tutorial_nicfd_nozzle.test_iter = 20
tutorial_nicfd_nozzle.test_vals = [
-1.909272, -6.407306, 4.284191, 0.000000, 0.000000
]
tutorial_nicfd_nozzle.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_nicfd_nozzle.timeout = 1600
tutorial_nicfd_nozzle.tol = 0.00001
tutorial_nicfd_nozzle.no_restart = True
test_list.append(tutorial_nicfd_nozzle)
# Unsteady NACA0012
tutorial_unst_naca0012 = TestCase('unsteady_naca0012')
tutorial_unst_naca0012.cfg_dir = "../Tutorials/compressible_flow/Unsteady_NACA0012"
tutorial_unst_naca0012.cfg_file = "unsteady_naca0012.cfg"
tutorial_unst_naca0012.test_iter = 500
tutorial_unst_naca0012.test_vals = [
500, 0, 0.302003, 0.665069, -5.300141, 0.000000, 0.0000e+00, 0.0000e+00
]
tutorial_unst_naca0012.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_unst_naca0012.timeout = 1600
tutorial_unst_naca0012.tol = 0.00001
tutorial_unst_naca0012.unsteady = True
test_list.append(tutorial_unst_naca0012)
### Design
# Inviscid NACA 0012 Design
tutorial_design_inv_naca0012 = TestCase('design_inv_naca0012')
tutorial_design_inv_naca0012.cfg_dir = "../Tutorials/design/Inviscid_2D_Unconstrained_NACA0012"
tutorial_design_inv_naca0012.cfg_file = "inv_NACA0012_basic.cfg"
tutorial_design_inv_naca0012.test_iter = 0
tutorial_design_inv_naca0012.test_vals = [
-3.585391, -2.989014, 0.134515, 0.208523
] #last 4 columns
tutorial_design_inv_naca0012.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_design_inv_naca0012.timeout = 1600
tutorial_design_inv_naca0012.tol = 0.00001
tutorial_design_inv_naca0012.no_restart = True
test_list.append(tutorial_design_inv_naca0012)
# Turbulent RAE 2822 Design
tutorial_design_turb_rae2822 = TestCase('design_turb_rae2822')
tutorial_design_turb_rae2822.cfg_dir = "../Tutorials/design/Turbulent_2D_Constrained_RAE2822"
tutorial_design_turb_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
tutorial_design_turb_rae2822.test_iter = 0
tutorial_design_turb_rae2822.test_vals = [
-1.700114, -4.941261, 0.218432, 0.190639
] #last 4 columns
tutorial_design_turb_rae2822.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_design_turb_rae2822.timeout = 1600
tutorial_design_turb_rae2822.tol = 0.00001
tutorial_design_turb_rae2822.no_restart = True
test_list.append(tutorial_design_turb_rae2822)
# Multi Objective Design
tutorial_design_multiobj = TestCase('design_multiobj')
tutorial_design_multiobj.cfg_dir = "../Tutorials/design/Multi_Objective_Shape_Design"
tutorial_design_multiobj.cfg_file = "inv_wedge_ROE_multiobj_combo.cfg"
tutorial_design_multiobj.test_iter = 0
tutorial_design_multiobj.test_vals = [
2.657333, -3.020635, 324840.000000, 0.000000
] #last 4 columns
tutorial_design_multiobj.su2_exec = "mpirun -np 2 SU2_CFD"
tutorial_design_multiobj.timeout = 1600
tutorial_design_multiobj.tol = 0.00001
tutorial_design_multiobj.no_restart = True
test_list.append(tutorial_design_multiobj)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
# Tests summary
print('==================================================================')
print('Summary of the parallel tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s' % test.tag)
else:
print('* FAILED - %s' % test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git pull')
# Build SU2_CFD in parallel using autoconf
os.system('./configure --prefix=$SU2_HOME --with-MPI=mpicxx CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.413232,2.965227,0.007590,0.051651]
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.149012,-5.528869,0.334821,0.022212]
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-2.680761,3.156839,-0.252403,0.044445]
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.830407,-4.275436,0.288842,0.016334]
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.234581,0.260131,-0.167010,0.012885]
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.748270,-1.281365,0.096480,-1.541539]
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.634245,-5.433694,0.886579,0.024338] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.214299,4.029754,0.888047,0.024408] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.057473,-7.347789,-0.187197,0.010819] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327518,-6.563377,0.230436,0.155816] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.826348,-7.364208,-0.000065,0.803130] #last 4 columns
turb_naca0012.su2_exec = "parallel_computation.py -f"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709964,-11.007318,0.000012,0.211084] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-12.135515,-16.000000,0.005483,0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.352088,-6.532237,-0.000023,0.147720] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-0.586316,-6.050120,-0.032305,25.115000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-4.234330,-9.705736,0.005161,0.398940] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.810435,-6.920519,0.014614,1.020100] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-4.351102,-8.919996,-1.275200,-2.541400] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-2.872467,-8.347153,4.525800,0.360080] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [-7.501598,-7.335538,0.010910,0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-2.471178,-2.957206,-0.048458,0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
# RAM-C II Sphere-Cone -- 61km Altitude
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119,2.854417,-4.439628,0.000188]
ramc.su2_exec = "parallel_computation.py -f"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.739930,-0.277880,-0.151798,-3.745224]
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.621605,-1.171604,8.512933,0.300307]
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.542162,0.048674,1.398952,2.196894]
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git pull')
# Build SU2_CFD in parallel using autoconf
os.system('./configure --prefix=$SU2_HOME --with-MPI=mpicxx CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.413846,2.965840,0.007590,0.051651]
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-3.751809,-3.271265,0.136604,0.066791]
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-2.694577,3.148295,-0.252137,0.044398]
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.819412,-4.286432,0.288842,0.016334]
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.142353,0.347570,0.029870,0.015971]
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-9.727830,-9.107325,-0.047634,3.804844]
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822
rae2822 = TestCase('rae2822')
rae2822.cfg_dir = "rans/rae2822"
rae2822.cfg_file = "turb_SA_RAE2822.cfg"
rae2822.test_iter = 100
rae2822.test_vals = [-3.650797,-5.455693,0.886602,0.024346 ] #last 4 columns
rae2822.su2_exec = "parallel_computation.py -f"
rae2822.timeout = 1600
rae2822.tol = 0.00001
test_list.append(rae2822)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.086782,-7.250991,-0.000015,0.014381] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-4.872687,-11.524700,0.238115,0.155977] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-7.508443,-9.210101,-0.000034,0.007944] #last 4 columns
turb_naca0012.su2_exec = "parallel_computation.py -f"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-9.066924,-8.386769,-0.000003,0.008181] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012 (To be validated with finite differences)
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 100
contadj_naca0012.test_vals = [-4.953138,-10.312798,0.006116,0.527890] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid RAM-C (To be validated with finite differences)
contadj_ram_c = TestCase('contadj_ram_c')
contadj_ram_c.cfg_dir = "cont_adj_euler/ram_c"
contadj_ram_c.cfg_file = "inv_RAMC.cfg"
contadj_ram_c.test_iter = 100
contadj_ram_c.test_vals = [0.776609,-7.308868,-0.001885,0.080464] #last 4 columns
contadj_ram_c.su2_exec = "parallel_computation.py -f"
contadj_ram_c.timeout = 1600
contadj_ram_c.tol = 0.00001
test_list.append(contadj_ram_c)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [2.599646,-1.977099,0.529560,179.160000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 (To be fixed)
contadj_ns_naca0012 = TestCase('contadj_ns_naca0012')
contadj_ns_naca0012.cfg_dir = "cont_adj_navierstokes/naca0012"
contadj_ns_naca0012.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012.test_iter = 100
contadj_ns_naca0012.test_vals = [1.515646,-3.816185,8.9793e-01,1.7569e-01] #last 4 columns
contadj_ns_naca0012.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012.timeout = 1600
contadj_ns_naca0012.tol = 0.00001
test_list.append(contadj_ns_naca0012)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012 (To be validated with finite differences)
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-5.356749,-8.622049,18.310000,-0.000000] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [-7.613876,-7.157641,0.011112,0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-9.002264,-10.002274,0.048091,0.000000 ] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
# RAM-C II Sphere-Cone -- 61km Altitude
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119,2.854417,-4.439634,0.000188]
ramc.su2_exec = "parallel_computation.py -f"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606839, -9.035212, -0.000000, 0.005688] #last 4 columns
discadj_naca0012.su2_exec = "SU2_CFD_AD"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
#######################################################
### Disc. adj. compressible RANS ###
#######################################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-1.751947, 0.485758, 0.181440, -0.000017] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-1.658566, -0.487694, 0.087556, 0.000023] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 10
discadj_cylinder.test_vals = [3.522068, -1.787841, -0.012030, 0.000017] #last 4 columns
discadj_cylinder.su2_exec = "SU2_CFD_AD"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
######################################
### RUN PYTHON TESTS ###
######################################
# test discrete_adjoint.py
discadj_euler_py = TestCase('discadj_euler_py')
discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
discadj_euler_py.cfg_file = "inv_NACA0012.cfg"
discadj_euler_py.test_iter = 10
discadj_euler_py.su2_exec = "discrete_adjoint.py"
discadj_euler_py.timeout = 1600
discadj_euler_py.reference_file = "of_grad_cd_disc.dat.ref"
discadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_euler_py.run_filediff())
test_list.append(discadj_euler_py)
# test direct_differentiation.py
directdiff_euler_py = TestCase('directdiff_euler_py')
directdiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
directdiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
directdiff_euler_py.test_iter = 10
directdiff_euler_py.su2_exec = "direct_differentiation.py"
directdiff_euler_py.timeout = 1600
directdiff_euler_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_euler_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_euler_py.run_filediff())
test_list.append(directdiff_euler_py)
# test continuous_adjoint.py, with multiple objectives
discadj_multi_py = TestCase('discadj_multi_py')
discadj_multi_py.cfg_dir = "cont_adj_euler/wedge"
discadj_multi_py.cfg_file = "inv_wedge_ROE_disc_multiobj.cfg"
discadj_multi_py.test_iter = 10
discadj_multi_py.su2_exec = "discrete_adjoint.py"
discadj_multi_py.timeout = 1600
discadj_multi_py.reference_file = "of_grad_combo.dat.refdiscrete"
discadj_multi_py.test_file = "of_grad_combo.dat"
pass_list.append(discadj_multi_py.run_filediff())
test_list.append(discadj_multi_py)
# Tests summary
print '=================================================================='
print 'Summary of the serial tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s'%test.tag
else:
print '* FAILED - %s'%test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606839, -9.035212, -0.000000,
0.005688] #last 4 columns
discadj_naca0012.su2_exec = "SU2_CFD_AD"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.724711, -4.052467, -0.000000,
0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "SU2_CFD_AD"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
# Arina nozzle 2D
discadj_arina2k = TestCase('discadj_arina2k')
discadj_arina2k.cfg_dir = "disc_adj_euler/arina2k"
discadj_arina2k.cfg_file = "Arina2KRS.cfg"
discadj_arina2k.test_iter = 20
discadj_arina2k.test_vals = [-0.774805, -0.801209, 3.1979e+02,
0.0000e+00] #last 4 columns
discadj_arina2k.su2_exec = "SU2_CFD_AD"
discadj_arina2k.timeout = 8400
discadj_arina2k.tol = 0.00001
test_list.append(discadj_arina2k)
#######################################################
### Disc. adj. compressible RANS ###
#######################################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [
-1.751962, 0.485751, 0.182121, -0.000018
] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [
-1.654903, -0.491485, 0.109157, 0.000011
] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "disc_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [
-3.633197, -2.544956, 0.000000, 0.000000
] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "SU2_CFD_AD"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder (Heated)
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "disc_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "heated_cylinder.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [
-2.374306, -2.371564, 0.000000, 0.000000
] #last 4 columns
discadj_incomp_cylinder.su2_exec = "SU2_CFD_AD"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012 SA
discadj_incomp_turb_NACA0012_sa = TestCase(
'discadj_incomp_turb_NACA0012_sa')
discadj_incomp_turb_NACA0012_sa.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sa.cfg_file = "turb_naca0012_sa.cfg"
discadj_incomp_turb_NACA0012_sa.test_iter = 10
discadj_incomp_turb_NACA0012_sa.test_vals = [
-3.845979, -1.031094, 0.000000, 0.000000
] #last 4 columns
discadj_incomp_turb_NACA0012_sa.su2_exec = "SU2_CFD_AD"
discadj_incomp_turb_NACA0012_sa.timeout = 1600
discadj_incomp_turb_NACA0012_sa.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sa)
# Adjoint Incompressible Turbulent NACA 0012 SST
discadj_incomp_turb_NACA0012_sst = TestCase(
'discadj_incomp_turb_NACA0012_sst')
discadj_incomp_turb_NACA0012_sst.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sst.cfg_file = "turb_naca0012_sst.cfg"
discadj_incomp_turb_NACA0012_sst.test_iter = 10
discadj_incomp_turb_NACA0012_sst.test_vals = [
-3.845759, -2.416668, 0.000000, 0.000000
] #last 4 columns
discadj_incomp_turb_NACA0012_sst.su2_exec = "SU2_CFD_AD"
discadj_incomp_turb_NACA0012_sst.timeout = 1600
discadj_incomp_turb_NACA0012_sst.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746904, -1.544886, -0.008345,
0.000014] #last 4 columns
discadj_cylinder.su2_exec = "SU2_CFD_AD"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##########################################################################
### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order ###
##########################################################################
# Turbulent Cylinder
discadj_DT_1ST_cylinder = TestCase('unsteady_cylinder_DT_1ST')
discadj_DT_1ST_cylinder.cfg_dir = "disc_adj_rans/cylinder_DT_1ST"
discadj_DT_1ST_cylinder.cfg_file = "cylinder.cfg"
discadj_DT_1ST_cylinder.test_iter = 9
discadj_DT_1ST_cylinder.test_vals = [
3.698165, -1.607052, -2.2500e-03, 2.7211e-05
] #last 4 columns
discadj_DT_1ST_cylinder.su2_exec = "SU2_CFD_AD"
discadj_DT_1ST_cylinder.timeout = 1600
discadj_DT_1ST_cylinder.tol = 0.00001
discadj_DT_1ST_cylinder.unsteady = True
test_list.append(discadj_DT_1ST_cylinder)
###################################
### Structural Adjoint ###
###################################
# Structural model
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 9
discadj_fea.test_vals = [-6.282767, -6.361594, -3.6413e-04,
-8.7087e+00] #last 4 columns
discadj_fea.su2_exec = "SU2_CFD_AD"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Disc. adj. heat ###
###################################
# Discrete adjoint for heated cylinder
discadj_heat = TestCase('discadj_heat')
discadj_heat.cfg_dir = "disc_adj_heat"
discadj_heat.cfg_file = "disc_adj_heat.cfg"
discadj_heat.test_iter = 10
discadj_heat.test_vals = [3.176483, 1.144873, -1040.512028,
-3277.663739] #last 4 columns
discadj_heat.su2_exec = "SU2_CFD_AD"
discadj_heat.timeout = 1600
discadj_heat.tol = 0.00001
test_list.append(discadj_heat)
###################################
### Coupled FSI Adjoint ###
###################################
# Structural model
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "configAD_fsi.cfg"
discadj_fsi.test_iter = 3000
discadj_fsi.test_vals = [0.958848, -0.157183, 0.658415,
1.302076] #last 4 columns
discadj_fsi.su2_exec = "SU2_CFD_AD"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
######################################
### RUN PYTHON TESTS ###
######################################
# test discrete_adjoint.py
discadj_euler_py = TestCase('discadj_euler_py')
discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
discadj_euler_py.cfg_file = "inv_NACA0012.cfg"
discadj_euler_py.test_iter = 10
discadj_euler_py.su2_exec = "discrete_adjoint.py"
discadj_euler_py.timeout = 1600
discadj_euler_py.reference_file = "of_grad_cd_disc.dat.ref"
discadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_euler_py.run_filediff())
test_list.append(discadj_euler_py)
# test discrete_adjoint with multiple ffd boxes
discadj_multiple_ffd_py = TestCase('discadj_multiple_ffd_py')
discadj_multiple_ffd_py.cfg_dir = "multiple_ffd/naca0012"
discadj_multiple_ffd_py.cfg_file = "inv_NACA0012_ffd.cfg"
discadj_multiple_ffd_py.test_iter = 9
discadj_multiple_ffd_py.su2_exec = "discrete_adjoint.py"
discadj_multiple_ffd_py.timeout = 1600
discadj_multiple_ffd_py.reference_file = "of_grad_cd.dat.ref"
discadj_multiple_ffd_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_multiple_ffd_py.run_filediff())
test_list.append(discadj_multiple_ffd_py)
# test direct_differentiation.py
directdiff_euler_py = TestCase('directdiff_euler_py')
directdiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
directdiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
directdiff_euler_py.test_iter = 10
directdiff_euler_py.su2_exec = "direct_differentiation.py"
directdiff_euler_py.timeout = 1600
directdiff_euler_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_euler_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_euler_py.run_filediff())
test_list.append(directdiff_euler_py)
# test direct_differentiation.py with multiple ffd boxes
directdiff_multiple_ffd_py = TestCase('directdiff_multiple_ffd_py')
directdiff_multiple_ffd_py.cfg_dir = "multiple_ffd/naca0012"
directdiff_multiple_ffd_py.cfg_file = "inv_NACA0012_ffd.cfg"
directdiff_multiple_ffd_py.test_iter = 9
directdiff_multiple_ffd_py.su2_exec = "direct_differentiation.py"
directdiff_multiple_ffd_py.timeout = 1600
directdiff_multiple_ffd_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_multiple_ffd_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_multiple_ffd_py.run_filediff())
test_list.append(directdiff_multiple_ffd_py)
# test continuous_adjoint.py, with multiple objectives
discadj_multi_py = TestCase('discadj_multi_py')
discadj_multi_py.cfg_dir = "cont_adj_euler/wedge"
discadj_multi_py.cfg_file = "inv_wedge_ROE_multiobj.cfg"
discadj_multi_py.test_iter = 10
discadj_multi_py.su2_exec = "discrete_adjoint.py"
discadj_multi_py.timeout = 1600
discadj_multi_py.reference_file = "of_grad_combo.dat.refdiscrete"
discadj_multi_py.test_file = "of_grad_combo.dat"
pass_list.append(discadj_multi_py.run_filediff())
test_list.append(discadj_multi_py)
# Tests summary
print('==================================================================')
print('Summary of the serial tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s' % test.tag)
else:
print('* FAILED - %s' % test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.561506, -8.926634, -0.000000, 0.005587]
discadj_naca0012.su2_exec = "parallel_computation.py -f"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.734502, -3.839637, 0.000000, 0.000000]
discadj_cylinder3D.su2_exec = "parallel_computation.py -f"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
# Arina nozzle 2D
discadj_arina2k = TestCase('discadj_arina2k')
discadj_arina2k.cfg_dir = "disc_adj_euler/arina2k"
discadj_arina2k.cfg_file = "Arina2KRS.cfg"
discadj_arina2k.test_iter = 20
discadj_arina2k.test_vals = [-3.111181, -3.501516, 6.8705e-02, 0]
discadj_arina2k.su2_exec = "parallel_computation.py -f"
discadj_arina2k.timeout = 1600
discadj_arina2k.tol = 0.00001
test_list.append(discadj_arina2k)
# Equivalent area NACA64-206
ea_naca64206 = TestCase('ea_naca64206')
ea_naca64206.cfg_dir = "optimization_euler/equivalentarea_naca64206"
ea_naca64206.cfg_file = "NACA64206.cfg"
ea_naca64206.test_iter = 10
ea_naca64206.test_vals = [3.181093, 2.471539, -5487700.0, 8.3604]
ea_naca64206.su2_exec = "mpirun -n 2 SU2_CFD_AD"
ea_naca64206.timeout = 1600
ea_naca64206.tol = 0.00001
test_list.append(ea_naca64206)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-2.230578, 0.696567, 0.181590, -0.000018, 5, -3.421214, 5, -6.798877]
discadj_rans_naca0012_sa.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-2.221792, -0.491538, 0.182010, -0.000018]
discadj_rans_naca0012_sst.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "disc_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [20.000000, -4.095412, -2.690483, 0.000000]
discadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder (Heated)
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "disc_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "heated_cylinder.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [20.000000, -2.195581, -2.162081, 0.000000]
discadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012 SA
discadj_incomp_turb_NACA0012_sa = TestCase('discadj_incomp_turb_NACA0012_sa')
discadj_incomp_turb_NACA0012_sa.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sa.cfg_file = "turb_naca0012_sa.cfg"
discadj_incomp_turb_NACA0012_sa.test_iter = 10
discadj_incomp_turb_NACA0012_sa.test_vals = [10.000000, -3.846018, -1.031079, 0.000000]
discadj_incomp_turb_NACA0012_sa.su2_exec = "parallel_computation.py -f"
discadj_incomp_turb_NACA0012_sa.timeout = 1600
discadj_incomp_turb_NACA0012_sa.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sa)
# Adjoint Incompressible Turbulent NACA 0012 SST
discadj_incomp_turb_NACA0012_sst = TestCase('discadj_incomp_turb_NACA0012_sst')
discadj_incomp_turb_NACA0012_sst.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sst.cfg_file = "turb_naca0012_sst.cfg"
discadj_incomp_turb_NACA0012_sst.test_iter = 10
discadj_incomp_turb_NACA0012_sst.test_vals = [-3.845593, -2.413098, -8.419991, 0.000000]
discadj_incomp_turb_NACA0012_sst.su2_exec = "parallel_computation.py -f"
discadj_incomp_turb_NACA0012_sst.timeout = 1600
discadj_incomp_turb_NACA0012_sst.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746909, -1.544883, -0.008321, 0.000014] #last 4 columns
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##############################################################
### Unsteady Disc. adj. compressible RANS Windowed Average ###
##############################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder_windowed_average_AD')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder_Windowing_AD.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.004406] #last column
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##############################################################
### Unsteady Disc. adj. compressible RANS Windowed Average ###
##############################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder_windowed_average')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder_Windowing.cfg"
discadj_cylinder.test_iter = 6
discadj_cylinder.test_vals = [0.202349, -0.000119, 1.899933, -0.000050, 1.067900]
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.0001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##########################################################################
### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order ###
##########################################################################
# Turbulent Cylinder
discadj_DT_1ST_cylinder = TestCase('unsteady_cylinder_DT_1ST')
discadj_DT_1ST_cylinder.cfg_dir = "disc_adj_rans/cylinder_DT_1ST"
discadj_DT_1ST_cylinder.cfg_file = "cylinder.cfg"
discadj_DT_1ST_cylinder.test_iter = 9
discadj_DT_1ST_cylinder.test_vals = [3.698168, -1.607050, -0.002159, 0.000028] #last 4 columns
discadj_DT_1ST_cylinder.su2_exec = "parallel_computation.py -f"
discadj_DT_1ST_cylinder.timeout = 1600
discadj_DT_1ST_cylinder.tol = 0.00001
discadj_DT_1ST_cylinder.unsteady = True
test_list.append(discadj_DT_1ST_cylinder)
######################################################
### Unsteady Disc. adj. compressible pitching NACA ###
######################################################
# compressible pitching NACA0012
discadj_pitchingNACA0012 = TestCase('pitchingNACA0012')
discadj_pitchingNACA0012.cfg_dir = "disc_adj_euler/naca0012_pitching"
discadj_pitchingNACA0012.cfg_file = "inv_NACA0012_pitching.cfg"
discadj_pitchingNACA0012.test_iter = 4
discadj_pitchingNACA0012.test_vals = [-1.223480, -1.639387, -0.007591, 0.000013]
discadj_pitchingNACA0012.su2_exec = "parallel_computation.py -f"
discadj_pitchingNACA0012.timeout = 1600
discadj_pitchingNACA0012.tol = 0.00001
discadj_pitchingNACA0012.unsteady = True
test_list.append(discadj_pitchingNACA0012)
#######################################################
### Disc. adj. turbomachinery ###
#######################################################
# Transonic Stator 2D
discadj_trans_stator = TestCase('transonic_stator')
discadj_trans_stator.cfg_dir = "disc_adj_turbomachinery/transonic_stator_2D"
discadj_trans_stator.cfg_file = "transonic_stator.cfg"
discadj_trans_stator.test_iter = 79
discadj_trans_stator.test_vals = [79.000000, -1.941681, -1.998327]
discadj_trans_stator.su2_exec = "parallel_computation.py -f"
discadj_trans_stator.timeout = 1600
discadj_trans_stator.tol = 0.00001
test_list.append(discadj_trans_stator)
###################################
### Structural Adjoint ###
###################################
# Structural model
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 4
discadj_fea.test_vals = [-2.849774, -3.238669, -0.000364, -8.708700] #last 4 columns
discadj_fea.su2_exec = "parallel_computation.py -f"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Disc. adj. heat ###
###################################
# Discrete adjoint for heated cylinder
discadj_heat = TestCase('discadj_heat')
discadj_heat.cfg_dir = "disc_adj_heat"
discadj_heat.cfg_file = "disc_adj_heat.cfg"
discadj_heat.test_iter = 10
discadj_heat.test_vals = [-2.280433, 0.714828, -0.743730, -6.767300]
discadj_heat.su2_exec = "parallel_computation.py -f"
discadj_heat.timeout = 1600
discadj_heat.tol = 0.00001
test_list.append(discadj_heat)
###################################
### Coupled FSI Adjoint ###
###################################
# Legacy driver
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "config.cfg"
discadj_fsi.test_iter = 6
discadj_fsi.test_vals = [6.000000, -1.559957, -3.080711, 0.000440, -1.063100]
discadj_fsi.su2_exec = "mpirun -n 2 SU2_CFD_AD"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
# Multi physics framework
discadj_fsi2 = TestCase('discadj_fsi_airfoil')
discadj_fsi2.cfg_dir = "disc_adj_fsi/Airfoil_2d"
discadj_fsi2.cfg_file = "config.cfg"
discadj_fsi2.test_iter = 8
discadj_fsi2.test_vals = [-5.318452, -2.4380e-13]
discadj_fsi2.su2_exec = "mpirun -n 2 SU2_CFD_AD"
discadj_fsi2.timeout = 1600
discadj_fsi2.tol = 1e-16
test_list.append(discadj_fsi2)
###################################
### Coupled CHT Adjoint ###
###################################
# Coupled discrete adjoint for heatflux in heated cylinder array
discadj_cht = TestCase('discadj_cht')
discadj_cht.cfg_dir = "coupled_cht/disc_adj_incomp_2d"
discadj_cht.cfg_file = "cht_2d_3cylinders.cfg"
discadj_cht.test_iter = 10
discadj_cht.test_vals = [-2.364405, -3.085549, -3.085516, -3.085511]
discadj_cht.su2_exec = "mpirun -n 2 SU2_CFD_AD"
discadj_cht.timeout = 1600
discadj_cht.tol = 0.00001
test_list.append(discadj_cht)
# 2D DA cht streamwise periodic case, 2 zones, avg temp objective
da_sp_pinArray_cht_2d_dp_hf = TestCase('da_sp_pinArray_cht_2d_dp_hf')
da_sp_pinArray_cht_2d_dp_hf.cfg_dir = "incomp_navierstokes/streamwise_periodic/chtPinArray_2d"
da_sp_pinArray_cht_2d_dp_hf.cfg_file = "DA_configMaster.cfg"
da_sp_pinArray_cht_2d_dp_hf.test_iter = 100
da_sp_pinArray_cht_2d_dp_hf.test_vals = [-4.800529, -4.065499, -4.137153] #last 4 lines
da_sp_pinArray_cht_2d_dp_hf.su2_exec = "mpirun -n 2 SU2_CFD_AD"
da_sp_pinArray_cht_2d_dp_hf.timeout = 1600
da_sp_pinArray_cht_2d_dp_hf.tol = 0.00001
da_sp_pinArray_cht_2d_dp_hf.multizone = True
test_list.append(da_sp_pinArray_cht_2d_dp_hf)
# 2D unsteady CHT vortex shedding at RE=200. TAVG_Temperature OF
da_unsteadyCHT_cylinder = TestCase('da_unsteadyCHT_cylinder')
da_unsteadyCHT_cylinder.cfg_dir = "coupled_cht/disc_adj_unsteadyCHT_cylinder"
da_unsteadyCHT_cylinder.cfg_file = "chtMaster.cfg"
da_unsteadyCHT_cylinder.test_iter = 2
da_unsteadyCHT_cylinder.test_vals = [-3.521358, -4.312658, -4.271025, -9.846075, -7.967741, 0.0000e+00, 3.6840e+00, 2.9483e-01]
da_unsteadyCHT_cylinder.su2_exec = "mpirun -n 2 SU2_CFD_AD"
da_unsteadyCHT_cylinder.timeout = 1600
da_unsteadyCHT_cylinder.tol = 0.00001
da_unsteadyCHT_cylinder.unsteady = True
da_unsteadyCHT_cylinder.multizone = True
test_list.append(da_unsteadyCHT_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
##################################################
### Structural Adjoint - Topology Optimization ###
##################################################
# test discrete_adjoint.py
discadj_topol_optim = TestCase('discadj_topol_optim')
discadj_topol_optim.cfg_dir = "fea_topology"
discadj_topol_optim.cfg_file = "config.cfg"
discadj_topol_optim.test_iter = 0
discadj_topol_optim.su2_exec = "parallel_computation.py -f"
discadj_topol_optim.timeout = 1600
discadj_topol_optim.reference_file = "grad_ref_node.dat.ref"
discadj_topol_optim.test_file = "grad_ref_node.dat"
pass_list.append(discadj_topol_optim.run_filediff())
test_list.append(discadj_topol_optim)
####################################################################################
### Unsteady Disc. adj. compressible RANS Windowed Average with restart solution ###
####################################################################################
# NACA0012 Airfoil
unsteady_naca0012 = TestCase('unsteady_NACA0012_restart_adjoint')
unsteady_naca0012.cfg_dir = "disc_adj_rans/naca0012"
unsteady_naca0012.cfg_file = "naca0012.cfg"
unsteady_naca0012.test_iter = 14
unsteady_naca0012.su2_exec = "discrete_adjoint.py -f"
unsteady_naca0012.timeout = 1600
unsteady_naca0012.reference_file = "of_grad_cd.csv.ref"
unsteady_naca0012.test_file = "of_grad_cd.csv"
unsteady_naca0012.unsteady = True
pass_list.append(unsteady_naca0012.run_filediff())
test_list.append(unsteady_naca0012)
####################################################################################
### Unsteady Disc. adj. compressible RANS Windowed Average only adjoint ###
####################################################################################
# NACA0012 Airfoil (Test depends on results of "unsteady_NACA0012_restart_adjoint")
unsteady_naca0012 = TestCase('unsteady_NACA0012_adjoint_only')
unsteady_naca0012.cfg_dir = "disc_adj_rans/naca0012"
unsteady_naca0012.cfg_file = "naca0012.cfg"
unsteady_naca0012.test_iter = 14
unsteady_naca0012.su2_exec = "discrete_adjoint.py -m adj -f"
unsteady_naca0012.timeout = 1600
unsteady_naca0012.reference_file = "of_grad_cd.csv.ref"
unsteady_naca0012.test_file = "of_grad_cd.csv"
unsteady_naca0012.unsteady = True
pass_list.append(unsteady_naca0012.run_filediff())
test_list.append(unsteady_naca0012)
####################################################################
### Unsteady Disc. adj. compressible RANS restart optimization ###
####################################################################
# test shape_optimization.py
naca_restart_shape_opt = TestCase('restart_shape_optimization')
naca_restart_shape_opt.cfg_dir = "optimization_rans/naca0012"
naca_restart_shape_opt.cfg_file = "naca0012.cfg"
naca_restart_shape_opt.test_iter = 1
naca_restart_shape_opt.test_vals = [1.000000, 1.000000, 0.007046, 0.196671]
naca_restart_shape_opt.su2_exec = "shape_optimization.py -f"
naca_restart_shape_opt.timeout = 1600
naca_restart_shape_opt.tol = 0.00001
pass_list.append(naca_restart_shape_opt.run_opt())
test_list.append(naca_restart_shape_opt)
####################################################################
### Unsteady Disc. Adj. Coupled FSI ###
####################################################################
# Unsteady multi physics framework
dyn_discadj_fsi = TestCase('dyn_discadj_fsi')
dyn_discadj_fsi.cfg_dir = "disc_adj_fsi/dyn_fsi"
dyn_discadj_fsi.cfg_file = "config.cfg"
dyn_discadj_fsi.test_iter = 2
dyn_discadj_fsi.su2_exec = "mpirun -n 2 SU2_CFD_AD"
dyn_discadj_fsi.timeout = 1600
dyn_discadj_fsi.reference_file = "grad_dv.opt.ref"
dyn_discadj_fsi.test_file = "grad_young.opt"
dyn_discadj_fsi.unsteady = True
pass_list.append(dyn_discadj_fsi.run_filediff())
test_list.append(dyn_discadj_fsi)
# Tests summary
print('==================================================================')
print('Summary of the parallel tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s'%test.tag)
else:
print('* FAILED - %s'%test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 20
channel.test_vals = [-2.667326, 2.797439, 0.018717, 0.006906]
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 20
naca0012.test_vals = [-4.023999, -3.515034, 0.339426, 0.022217]
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 20
wedge.test_vals = [-0.942862, 4.784581, -0.208106, 0.036665]
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [0.281704, 0.011821]
test_list.append(oneram6)
# Fixed CL NACA0012
fixedCL_naca0012 = TestCase('fixedcl_naca0012')
fixedCL_naca0012.cfg_dir = "fixed_cl/naca0012"
fixedCL_naca0012.cfg_file = "inv_NACA0012.cfg"
fixedCL_naca0012.test_iter = 10
fixedCL_naca0012.test_vals = [-12.130189, -6.702728, 0.300000, 0.019470]
test_list.append(fixedCL_naca0012)
# HYPERSONIC FLOW PAST BLUNT BODY
bluntbody = TestCase('bluntbody')
bluntbody.cfg_dir = "euler/bluntbody"
bluntbody.cfg_file = "blunt.cfg"
bluntbody.test_iter = 20
bluntbody.test_vals = [0.540010, 6.916656, 0.000027, 1.869004]
test_list.append(bluntbody)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 20
flatplate.test_vals = [-4.680775, 0.781235, -0.135957, 0.022978]
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765432, -1.297428, 0.019596, 0.310240]
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase('cylinder_lowmach')
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.850130, -1.388096, -0.056203, 108.140819]
test_list.append(cylinder_lowmach)
# 2D Poiseuille flow (body force driven with periodic inlet / outlet)
poiseuille = TestCase('poiseuille')
poiseuille.cfg_dir = "navierstokes/poiseuille"
poiseuille.cfg_file = "lam_poiseuille.cfg"
poiseuille.test_iter = 10
poiseuille.test_vals = [-5.048282, 0.650814, 0.008714, 13.677678]
test_list.append(poiseuille)
# 2D Poiseuille flow (inlet profile file)
poiseuille_profile = TestCase('poiseuille_profile')
poiseuille_profile.cfg_dir = "navierstokes/poiseuille"
poiseuille_profile.cfg_file = "profile_poiseuille.cfg"
poiseuille_profile.test_iter = 10
poiseuille_profile.test_vals = [-12.494721, -7.712408, -0.000000, 2.085796]
test_list.append(poiseuille_profile)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 20
rae2822_sa.test_vals = [-2.021224, -5.268445, 0.807582, 0.060731]
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 20
rae2822_sst.test_vals = [-0.510637, 4.876603, 0.812485, 0.061969]
test_list.append(rae2822_sst)
# RAE2822 SST_SUST
rae2822_sst_sust = TestCase('rae2822_sst_sust')
rae2822_sst_sust.cfg_dir = "rans/rae2822"
rae2822_sst_sust.cfg_file = "turb_SST_SUST_RAE2822.cfg"
rae2822_sst_sust.test_iter = 20
rae2822_sst_sust.test_vals = [-2.429813, 4.876602, 0.812485, 0.061969]
test_list.append(rae2822_sst_sust)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 20
turb_flatplate.test_vals = [-4.157169, -6.737133, -0.176253, 0.057446]
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.388851, -6.689340, 0.230320, 0.157649]
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-11.537781, -14.899750, 1.064330, 0.019756]
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-12.797090, -5.872763, 1.049989, 0.019163]
test_list.append(turb_naca0012_sst)
# NACA0012 (SST_SUST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst_sust = TestCase('turb_naca0012_sst_sust')
turb_naca0012_sst_sust.cfg_dir = "rans/naca0012"
turb_naca0012_sst_sust.cfg_file = "turb_NACA0012_sst_sust.cfg"
turb_naca0012_sst_sust.test_iter = 10
turb_naca0012_sst_sust.test_vals = [
-12.640091, -5.751854, 1.005233, 0.019017
]
test_list.append(turb_naca0012_sst_sust)
# PROPELLER
propeller = TestCase('propeller')
propeller.cfg_dir = "rans/propeller"
propeller.cfg_file = "propeller.cfg"
propeller.test_iter = 10
propeller.test_vals = [-3.389576, -8.409529, 0.000048, 0.056329]
test_list.append(propeller)
# PROPELLER VARIBLE LOAD
propeller_var_load = TestCase('propeller_variable_load')
propeller_var_load.cfg_dir = "rans/actuatordisk_variable_load"
propeller_var_load.cfg_file = "propeller_variable_load.cfg"
propeller_var_load.test_iter = 20
propeller_var_load.test_vals = [-1.808010, -4.535613, 0.000190, 0.172483]
test_list.append(propeller_var_load)
#################################
## Compressible RANS Restart ###
#################################
# NACA0012 SST Multigrid restart
turb_naca0012_sst_restart_mg = TestCase('turb_naca0012_sst_restart_mg')
turb_naca0012_sst_restart_mg.cfg_dir = "rans/naca0012"
turb_naca0012_sst_restart_mg.cfg_file = "turb_NACA0012_sst_multigrid_restart.cfg"
turb_naca0012_sst_restart_mg.test_iter = 20
turb_naca0012_sst_restart_mg.ntest_vals = 5
turb_naca0012_sst_restart_mg.test_vals = [
-7.653296, -7.729472, -1.981061, -0.000016, 0.079062
]
test_list.append(turb_naca0012_sst_restart_mg)
#############################
### Compressibele RANS UQ ###
#############################
# NACA0012 1c
turb_naca0012_1c = TestCase('turb_naca0012_1c')
turb_naca0012_1c.cfg_dir = "rans_uq/naca0012"
turb_naca0012_1c.cfg_file = "turb_NACA0012_uq_1c.cfg"
turb_naca0012_1c.test_iter = 10
turb_naca0012_1c.test_vals = [-4.979389, 1.140070, 1.211965, 0.194237]
test_list.append(turb_naca0012_1c)
# NACA0012 2c
turb_naca0012_2c = TestCase('turb_naca0012_2c')
turb_naca0012_2c.cfg_dir = "rans_uq/naca0012"
turb_naca0012_2c.cfg_file = "turb_NACA0012_uq_2c.cfg"
turb_naca0012_2c.test_iter = 10
turb_naca0012_2c.test_vals = [-5.484195, 0.969789, 1.310525, 0.231240]
test_list.append(turb_naca0012_2c)
# NACA0012 3c
turb_naca0012_3c = TestCase('turb_naca0012_3c')
turb_naca0012_3c.cfg_dir = "rans_uq/naca0012"
turb_naca0012_3c.cfg_file = "turb_NACA0012_uq_3c.cfg"
turb_naca0012_3c.test_iter = 10
turb_naca0012_3c.test_vals = [-5.586959, 0.932359, 1.535455, 0.315820]
test_list.append(turb_naca0012_3c)
# NACA0012 p1c1
turb_naca0012_p1c1 = TestCase('turb_naca0012_p1c1')
turb_naca0012_p1c1.cfg_dir = "rans_uq/naca0012"
turb_naca0012_p1c1.cfg_file = "turb_NACA0012_uq_p1c1.cfg"
turb_naca0012_p1c1.test_iter = 10
turb_naca0012_p1c1.test_vals = [-5.132081, 1.076462, 1.178093, 0.181595]
test_list.append(turb_naca0012_p1c1)
# NACA0012 p1c2
turb_naca0012_p1c2 = TestCase('turb_naca0012_p1c2')
turb_naca0012_p1c2.cfg_dir = "rans_uq/naca0012"
turb_naca0012_p1c2.cfg_file = "turb_NACA0012_uq_p1c2.cfg"
turb_naca0012_p1c2.test_iter = 10
turb_naca0012_p1c2.test_vals = [-5.556648, 0.945129, 1.240986, 0.205071]
test_list.append(turb_naca0012_p1c2)
######################################
### Harmonic Balance ###
######################################
# Description of the regression test
harmonic_balance = TestCase('harmonic_balance')
harmonic_balance.cfg_dir = "harmonic_balance"
harmonic_balance.cfg_file = "HB.cfg"
harmonic_balance.test_iter = 25
harmonic_balance.test_vals = [-1.589755, 3.922207, 0.006725, 0.099455]
harmonic_balance.new_output = False
test_list.append(harmonic_balance)
# Turbulent pitching NACA 64a010 airfoil
hb_rans_preconditioning = TestCase('hb_rans_preconditioning')
hb_rans_preconditioning.cfg_dir = "harmonic_balance/hb_rans_preconditioning"
hb_rans_preconditioning.cfg_file = "davis.cfg"
hb_rans_preconditioning.test_iter = 25
hb_rans_preconditioning.test_vals = [
-1.902391, -5.950120, 0.007786, 0.128110
]
hb_rans_preconditioning.new_output = False
test_list.append(hb_rans_preconditioning)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.627934, -0.164469, 0.051998, 2.547065]
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.996313, -2.601764, 1.510692, 1.493876]
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.162572, 0.066371, 1.399790, 2.220393]
square_cylinder.unsteady = True
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977520, 3.481804, -0.012404, -0.007452]
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.074525, 0.033127, -0.001650, -0.000127]
aeroelastic.unsteady = True
test_list.append(aeroelastic)
# Delayed Detached Eddy Simulation
ddes_flatplate = TestCase('ddes_flatplate')
ddes_flatplate.cfg_dir = "ddes/flatplate"
ddes_flatplate.cfg_file = "ddes_flatplate.cfg"
ddes_flatplate.test_iter = 10
ddes_flatplate.test_vals = [-2.714758, -5.883004, -0.215005, 0.023783]
ddes_flatplate.unsteady = True
test_list.append(ddes_flatplate)
######################################
### NICFD ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.040283, 1.124491, -0.000009, 0.000000]
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.401640, 0.738165, -0.000035, 0.000000]
test_list.append(edge_PPR)
######################################
### Turbomachinery ###
######################################
# Jones APU Turbocharger
Jones_tc = TestCase('jones_turbocharger')
Jones_tc.cfg_dir = "turbomachinery/APU_turbocharger"
Jones_tc.cfg_file = "Jones.cfg"
Jones_tc.test_iter = 5
Jones_tc.test_vals = [-5.280316, 0.379651, 72.207590, 1.277638]
Jones_tc.new_output = False
test_list.append(Jones_tc)
# Jones APU Turbocharger restart
Jones_tc_rst = TestCase('jones_turbocharger_restart')
Jones_tc_rst.cfg_dir = "turbomachinery/APU_turbocharger"
Jones_tc_rst.cfg_file = "Jones_rst.cfg"
Jones_tc_rst.test_iter = 5
Jones_tc_rst.test_vals = [-4.625330, -1.568896, 33.995140, 10.181610]
Jones_tc_rst.new_output = False
test_list.append(Jones_tc_rst)
# 2D axial stage
axial_stage2D = TestCase('axial_stage2D')
axial_stage2D.cfg_dir = "turbomachinery/axial_stage_2D"
axial_stage2D.cfg_file = "Axial_stage2D.cfg"
axial_stage2D.test_iter = 20
axial_stage2D.test_vals = [-1.933200, 5.379973, 73.357900, 0.925878]
axial_stage2D.new_output = False
test_list.append(axial_stage2D)
# 2D transonic stator
transonic_stator = TestCase('transonic_stator')
transonic_stator.cfg_dir = "turbomachinery/transonic_stator_2D"
transonic_stator.cfg_file = "transonic_stator.cfg"
transonic_stator.test_iter = 20
transonic_stator.test_vals = [-0.562430, 5.828446, 96.436050, 0.062506]
transonic_stator.new_output = False
test_list.append(transonic_stator)
# 2D transonic stator restart
transonic_stator_rst = TestCase('transonic_stator_restart')
transonic_stator_rst.cfg_dir = "turbomachinery/transonic_stator_2D"
transonic_stator_rst.cfg_file = "transonic_stator_rst.cfg"
transonic_stator_rst.test_iter = 20
transonic_stator_rst.test_vals = [-6.621626, -0.614379, 5.002986, 0.002951]
transonic_stator_rst.new_output = False
test_list.append(transonic_stator_rst)
######################################
### Sliding Mesh ###
######################################
# Uniform flow
uniform_flow = TestCase('uniform_flow')
uniform_flow.cfg_dir = "sliding_interface/uniform_flow"
uniform_flow.cfg_file = "uniform_NN.cfg"
uniform_flow.test_iter = 5
uniform_flow.test_vals = [5.000000, 0.000000, -0.188748, -10.631530]
uniform_flow.unsteady = True
uniform_flow.multizone = True
test_list.append(uniform_flow)
# Channel_2D
channel_2D = TestCase('channel_2D')
channel_2D.cfg_dir = "sliding_interface/channel_2D"
channel_2D.cfg_file = "channel_2D_WA.cfg"
channel_2D.test_iter = 2
channel_2D.test_vals = [2.000000, 0.000000, 0.398089, 0.352762, 0.405397]
channel_2D.unsteady = True
channel_2D.multizone = True
test_list.append(channel_2D)
# Channel_3D
channel_3D = TestCase('channel_3D')
channel_3D.cfg_dir = "sliding_interface/channel_3D"
channel_3D.cfg_file = "channel_3D_WA.cfg"
channel_3D.test_iter = 2
channel_3D.test_vals = [2.000000, 0.000000, 0.620151, 0.505157, 0.415249]
channel_3D.unsteady = True
channel_3D.multizone = True
test_list.append(channel_3D)
# Pipe
pipe = TestCase('pipe')
pipe.cfg_dir = "sliding_interface/pipe"
pipe.cfg_file = "pipe_NN.cfg"
pipe.test_iter = 2
pipe.test_vals = [0.150024, 0.491949, 0.677757, 0.963990, 1.006944]
pipe.unsteady = True
pipe.multizone = True
test_list.append(pipe)
# Rotating cylinders
rotating_cylinders = TestCase('rotating_cylinders')
rotating_cylinders.cfg_dir = "sliding_interface/rotating_cylinders"
rotating_cylinders.cfg_file = "rot_cylinders_WA.cfg"
rotating_cylinders.test_iter = 3
rotating_cylinders.test_vals = [
3.000000, 0.000000, 0.777567, 1.134807, 1.224136
]
rotating_cylinders.unsteady = True
rotating_cylinders.multizone = True
test_list.append(rotating_cylinders)
# Supersonic vortex shedding
supersonic_vortex_shedding = TestCase('supersonic_vortex_shedding')
supersonic_vortex_shedding.cfg_dir = "sliding_interface/supersonic_vortex_shedding"
supersonic_vortex_shedding.cfg_file = "sup_vor_shed_WA.cfg"
supersonic_vortex_shedding.test_iter = 5
supersonic_vortex_shedding.test_vals = [
5.000000, 0.000000, 1.216554, 1.639121
]
supersonic_vortex_shedding.unsteady = True
supersonic_vortex_shedding.multizone = True
test_list.append(supersonic_vortex_shedding)
# Bars_SST_2D
bars_SST_2D = TestCase('bars_SST_2D')
bars_SST_2D.cfg_dir = "sliding_interface/bars_SST_2D"
bars_SST_2D.cfg_file = "bars.cfg"
bars_SST_2D.test_iter = 13
bars_SST_2D.test_vals = [13.000000, -0.619179, -1.564701]
bars_SST_2D.multizone = True
test_list.append(bars_SST_2D)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase('statbeam3d')
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-2.378370, -1.585252, -2.028505, 6.4359e+04]
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase('dynbeam2d')
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-3.240015, 2.895057, -0.353146, 66127.000000]
dynbeam2d.unsteady = True
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase('fsi2d')
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [4.000000, 0.000000, -3.764089, -4.081119]
fsi2d.multizone = True
fsi2d.unsteady = True
test_list.append(fsi2d)
# FSI, Static, 2D, new mesh solver
stat_fsi = TestCase('stat_fsi')
stat_fsi.cfg_dir = "fea_fsi/stat_fsi"
stat_fsi.cfg_file = "config.cfg"
stat_fsi.test_iter = 7
stat_fsi.test_vals = [-3.242834, -4.866608, 0.000000, 11.000000]
stat_fsi.multizone = True
test_list.append(stat_fsi)
# FSI, Dynamic, 2D, new mesh solver
dyn_fsi = TestCase('dyn_fsi')
dyn_fsi.cfg_dir = "fea_fsi/dyn_fsi"
dyn_fsi.cfg_file = "config.cfg"
dyn_fsi.test_iter = 4
dyn_fsi.test_vals = [-4.379823, -4.005990, 0.000000, 74.000000]
dyn_fsi.multizone = True
dyn_fsi.unsteady = True
test_list.append(dyn_fsi)
# FSI, Static, 2D, new mesh solver, restart
stat_fsi_restart = TestCase('stat_fsi_restart')
stat_fsi_restart.cfg_dir = "fea_fsi/stat_fsi"
stat_fsi_restart.cfg_file = "config_restart.cfg"
stat_fsi_restart.test_iter = 1
stat_fsi_restart.test_vals = [-3.474239, -4.250710, 0.000000, 36.000000]
stat_fsi_restart.multizone = True
test_list.append(stat_fsi_restart)
##############################################
### Method of Manufactured Solutions (MMS) ###
##############################################
# FVM, compressible, laminar N-S
mms_fvm_ns = TestCase('mms_fvm_ns')
mms_fvm_ns.cfg_dir = "mms/fvm_navierstokes"
mms_fvm_ns.cfg_file = "lam_mms_roe.cfg"
mms_fvm_ns.test_iter = 20
mms_fvm_ns.test_vals = [-2.851428, 2.192348, 0.000000, 0.000000]
test_list.append(mms_fvm_ns)
######################################
### RUN TESTS ###
######################################
for test in test_list:
test.su2_exec = "SU2_CFD -t 2"
test.timeout = 600
test.tol = 1e-4
#end
pass_list = [test.run_test() for test in test_list]
# Tests summary
print('==================================================================')
print('Summary of the parallel tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s' % test.tag)
else:
print('* FAILED - %s' % test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
"""This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. """
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase("channel")
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.110240, 2.263506, 0.008686, 0.029098] # last 4 columns
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase("naca0012")
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.191618, -5.592802, 0.334809, 0.022197] # last 4 columns
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase("wedge")
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.769374, 3.848733, -0.252191, 0.044410] # last 4 columns
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase("oneram6")
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.393130, -12.928941, 0.282557, 0.012706] # last 4 columns
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase("flatplate")
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231916, 0.261866, -0.166832, 0.012717] # last 4 columns
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase("cylinder")
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765426, -1.297422, 0.019496, 0.310082] # last 4 columns
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase("cylinder_lowmach")
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.850123, -1.388088, -0.056090, 108.140177] # last 4 columns
cylinder_lowmach.su2_exec = "SU2_CFD"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase("rae2822_sa")
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.442524, -5.441383, 0.884279, 0.024730] # last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase("rae2822_sst")
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.185243, 4.018464, 0.886786, 0.024927] # last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase("turb_flatplate")
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.069447, -7.354601, -0.187187, 0.010831] # last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase("turb_oneram6")
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438, 0.155815] # last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D results for finest grid: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase("turb_naca0012_sa")
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000763, -9.145363, 1.070528, 0.019417] # last 4 columns
turb_naca0012_sa.su2_exec = "SU2_CFD"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D results for finest grid: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase("turb_naca0012_sst")
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039675, -7.219913, 1.059622, 0.019138] # last 4 columns
turb_naca0012_sst.su2_exec = "SU2_CFD"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase("inc_turb_naca0012")
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710052, -11.007500, -0.000001, 0.210445] # last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase("contadj_naca0012")
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.787554, -15.192510, 0.300920, 0.536870] # last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase("contadj_oneram6")
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.133352, -12.707213, 6.8590e-01, 1.4092e-01] # last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
# Inviscid WEDGE: generalized adjoint and custom DV
contadj_wedge = TestCase("contadj_wedge")
contadj_wedge.cfg_dir = "cont_adj_euler/wedge"
contadj_wedge.cfg_file = "inv_wedge_ROE.cfg"
contadj_wedge.test_iter = 10
contadj_wedge.test_vals = [-7.364977, -13.301134, 0.000266, 0.000000] # last 4 columns
contadj_wedge.su2_exec = "SU2_CFD"
contadj_wedge.timeout = 1600
contadj_wedge.tol = 0.00001
test_list.append(contadj_wedge)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase("contadj_ns_cylinder")
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.677184, -9.141850, -2.056700, 4.497000] # last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase("contadj_ns_naca0012_sub")
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.229160] # last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase("contadj_ns_naca0012_trans")
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.620880] # last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase("contadj_rans_naca0012")
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, -19.169000, -2.994100] # last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase("contadj_rans_rae2822")
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.377843, -10.882446, -0.212470, 0.269390] # last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase("contadj_incomp_NACA0012")
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.980272, -12.146779, 1.9399, 0.000000] # last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase("contadj_incomp_cylinder")
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718622, -7.027366, -2.932100, 0.000000] # last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase("cavity")
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.627934, -0.164470, 0.051972, 2.547034] # last 4 columns
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase("spinning_cylinder")
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.709662, -2.274900, 1.418422, 1.734206] # last 4 columns
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase("square_cylinder")
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.544603, 0.048578, 1.398951, 2.196894] # last 4 columns
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase("sine_gust")
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.006222, -0.001342] # last 4 columns
sine_gust.su2_exec = "SU2_CFD"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase("aeroelastic")
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077106, 0.036449, -1.684916e-03, -1.131735e-04] # last 4 columns
aeroelastic.su2_exec = "SU2_CFD"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# ls89_sa
ls89_sa = TestCase("ls89_sa")
ls89_sa.cfg_dir = "nicf/LS89"
ls89_sa.cfg_file = "turb_SA_PR.cfg"
ls89_sa.test_iter = 100
ls89_sa.test_vals = [-6.383146, -13.350551, 0.069079, 0.160886] # last 4 columns
ls89_sa.su2_exec = "SU2_CFD"
ls89_sa.timeout = 1600
ls89_sa.tol = 0.00001
test_list.append(ls89_sa)
# # ls89_sst
# ls89_sst = TestCase('ls89_sst')
# ls89_sst.cfg_dir = "nicf/LS89"
# ls89_sst.cfg_file = "turb_SST_PR.cfg"
# ls89_sst.test_iter = 100
# ls89_sst.test_vals = [-8.548266, -1.449437, 0.067986, 0.151168] #last 4 columns
# ls89_sst.su2_exec = "SU2_CFD"
# ls89_sst.timeout = 1600
# ls89_sst.tol = 0.00001
# test_list.append(ls89_sst)
# Rarefaction shock wave edge_VW
edge_VW = TestCase("edge_VW")
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.055874, 1.117978, -0.000009, 0.000000] # last 4 columns
edge_VW.su2_exec = "SU2_CFD"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase("edge_PPR")
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.484387, 0.656352, -0.000037, 0.000000] # last 4 columns
edge_PPR.su2_exec = "SU2_CFD"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### turboSU2 ###
######################################
# Mini centrifugal turbine blade
centrifugal_blade = TestCase("centrifugal_blade")
centrifugal_blade.cfg_dir = "turbomachinery/centrifugal_blade"
centrifugal_blade.cfg_file = "centrifugal_blade.cfg"
centrifugal_blade.test_iter = 100
centrifugal_blade.test_vals = [-9.106943, -0.460429, 1.069070e01, 3.396010e-01] # last 4 columns
centrifugal_blade.su2_exec = "SU2_CFD"
centrifugal_blade.timeout = 1600
centrifugal_blade.tol = 0.000001
test_list.append(centrifugal_blade)
# Mini centrifugal turbine stage
centrifugal_stage = TestCase("centrifugal_stage")
centrifugal_stage.cfg_dir = "turbomachinery/centrifugal_stage"
centrifugal_stage.cfg_file = "centrifugal_stage.cfg"
centrifugal_stage.test_iter = 100
centrifugal_stage.test_vals = [-10.166364, 1.621172, 2.206476e01, 5.271075e-01] # last 4 columns
centrifugal_stage.su2_exec = "SU2_CFD"
centrifugal_stage.timeout = 1600
centrifugal_stage.tol = 0.000001
test_list.append(centrifugal_stage)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase("statbeam3d")
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-8.498274, -8.230638, -8.123824, 6.4095e04] # last 4 columns
statbeam3d.su2_exec = "SU2_CFD"
statbeam3d.timeout = 1600
statbeam3d.tol = 0.00001
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase("dynbeam2d")
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-9.420640, -5.365872, -12.430382, 6.5210e04] # last 4 columns
dynbeam2d.su2_exec = "SU2_CFD"
dynbeam2d.timeout = 1600
dynbeam2d.tol = 0.00001
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase("fsi2d")
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI_2D.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [2, 0.500000, -7.779713, -1.141613] # last 4 columns
fsi2d.su2_exec = "SU2_CFD"
fsi2d.timeout = 1600
fsi2d.tol = 0.00001
test_list.append(fsi2d)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
######################################
### RUN SU2_GEO TESTS ###
######################################
# NACA0012
naca0012_geo = TestCase("naca0012_geo")
naca0012_geo.cfg_dir = "optimization_euler/steady_naca0012"
naca0012_geo.cfg_file = "inv_NACA0012_adv.cfg"
naca0012_geo.test_vals = [0.120011, 0.0816925, 0.0, 1.0] # max thickness, area, twist, chord
naca0012_geo.su2_exec = "SU2_GEO"
naca0012_geo.timeout = 1600
naca0012_geo.tol = 0.00001
pass_list.append(naca0012_geo.run_geo())
test_list.append(naca0012_geo)
######################################
### RUN SU2_DEF TESTS ###
######################################
# RAE2822
rae2822_def = TestCase("rae2822_def")
rae2822_def.cfg_dir = "optimization_rans/steady_rae2822"
rae2822_def.cfg_file = "def_SA_RAE2822.cfg"
rae2822_def.test_iter = 100
rae2822_def.test_vals = [8.06616e-14] # residual
rae2822_def.su2_exec = "SU2_DEF"
rae2822_def.timeout = 1600
rae2822_def.tol = 1e-14
pass_list.append(rae2822_def.run_def())
test_list.append(rae2822_def)
# Inviscid ONERAM6
oneram6_sa_def = TestCase("oneram6_sa_def")
oneram6_sa_def.cfg_dir = "optimization_euler/steady_oneram6"
oneram6_sa_def.cfg_file = "def_ONERAM6.cfg"
oneram6_sa_def.test_iter = 600
oneram6_sa_def.test_vals = [3.46695e-13] # residual
oneram6_sa_def.su2_exec = "SU2_DEF"
oneram6_sa_def.timeout = 1600
oneram6_sa_def.tol = 1e-13
pass_list.append(oneram6_sa_def.run_def())
test_list.append(oneram6_sa_def)
######################################
### RUN PYTHON TESTS ###
######################################
# test continuous_adjoint.py
contadj_euler_py = TestCase("contadj_euler_py")
contadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
contadj_euler_py.cfg_file = "inv_NACA0012.cfg"
contadj_euler_py.test_iter = 10
contadj_euler_py.su2_exec = "continuous_adjoint.py"
contadj_euler_py.timeout = 1600
contadj_euler_py.reference_file = "of_grad_cd.dat.ref"
contadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(contadj_euler_py.run_filediff())
test_list.append(contadj_euler_py)
# test finite_difference.py
findiff_euler_py = TestCase("findiff_euler_py")
findiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
findiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
findiff_euler_py.test_iter = 10
findiff_euler_py.su2_exec = "finite_differences.py"
findiff_euler_py.timeout = 1600
findiff_euler_py.reference_file = "of_grad_findiff.dat.ref"
findiff_euler_py.test_file = "FINDIFF/of_grad_findiff.dat"
pass_list.append(findiff_euler_py.run_filediff())
test_list.append(findiff_euler_py)
# test shape_optimization.py
shape_opt_euler_py = TestCase("shape_opt_euler_py")
shape_opt_euler_py.cfg_dir = "optimization_euler/steady_naca0012"
shape_opt_euler_py.cfg_file = "inv_NACA0012_adv.cfg"
shape_opt_euler_py.test_iter = 1
shape_opt_euler_py.test_vals = [1, 1, 2.134974e-05, 3.829535e-03] # last 4 columns
shape_opt_euler_py.su2_exec = "shape_optimization.py -f"
shape_opt_euler_py.timeout = 1600
shape_opt_euler_py.tol = 0.00001
pass_list.append(shape_opt_euler_py.run_opt())
test_list.append(shape_opt_euler_py)
# Tests summary
print "=================================================================="
print "Summary of the serial tests"
for i, test in enumerate(test_list):
if pass_list[i]:
print " passed - %s" % test.tag
else:
print "* FAILED - %s" % test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/parallel_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# Build SU2_CFD in parallel using autoconf
os.system('./configure --prefix=$SU2_HOME --with-MPI=mpicxx CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
if not os.path.exists("./SU2_PRT"):
print 'Could not build SU2_PRT'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.007706, 2.358555, 0.008379, 0.028547]
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.157022, -5.537399, 0.334831, 0.022209]
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.647184, 3.989725, -0.251604, 0.044317]
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.707461, -4.138449, 0.269324, 0.018891]
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.232930, 0.260877, -0.166066, 0.013093]
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.759579, -1.292062, 0.047262, 0.139916]
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.454436, -5.440827, 0.892572, 0.024842] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.178534, 4.029258, 0.894386, 0.024992] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.057092, -7.373256, -0.187140, 0.011347] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327515, -6.563376, 0.230436, 0.155816] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.826376, -7.364213, -0.000093, 0.803146] #last 4 columns
turb_naca0012.su2_exec = "parallel_computation.py -f"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709973, -11.007322, -0.000001, 0.211093] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-12.122156, -17.630206, 0.300920, 0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.354703, -6.527803, -0.133910, 0.147720] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-0.585239, -6.048475, -2.056900, 25.115000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-4.234330, -9.705735, 0.516750, 0.398940] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.810435, -6.920519, 1.756200, 1.020100] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-4.351102, -8.919996, -72.511000, -2.541400] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-2.903360, -8.331847, 354.020000, 0.128700] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [-7.275605, -7.111247, 1.892600, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-2.471344, -2.947390, -3.086500, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
# RAM-C II Sphere-Cone -- 61km Altitude
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119, 2.854417, -4.439628, 0.000188]
ramc.su2_exec = "parallel_computation.py -f"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.569056, -0.103736, 0.465430, 0.399409]
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.601720, -1.146034, 8.586054, 0.271493]
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.542156, 0.048663, 1.398952, 2.196894]
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [
-3.606839, -9.035212, -3.3386e-07, 1.8777e-01
] #last 4 columns
discadj_naca0012.su2_exec = "SU2_CFD_AD"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
#######################################################
### Disc. adj. compressible RANS ###
#######################################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [
-1.751947, 0.485758, 0.181440, -0.385110
] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [
-1.658568, -0.487694, 8.7557e-02, -5.3701e-01
] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
# Tests summary
print '=================================================================='
print 'Summary of the serial tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s' % test.tag
else:
print '* FAILED - %s' % test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.110240, 2.263506, 0.008686, 0.029098] #last 4 columns
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.191618, -5.592802, 0.334809, 0.022197] #last 4 columns
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.769374, 3.848733, -0.252191, 0.044410] #last 4 columns
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.393130, -12.928941, 0.282557, 0.012706] #last 4 columns
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
# Fixed CL NACA0012
fixedCL_naca0012 = TestCase('fixedcl_naca0012')
fixedCL_naca0012.cfg_dir = "fixed_cl/naca0012"
fixedCL_naca0012.cfg_file = "inv_NACA0012.cfg"
fixedCL_naca0012.test_iter = 500
fixedCL_naca0012.test_vals = [-6.707530,-1.319851,0.300017,0.019390] #last 4 columns
fixedCL_naca0012.su2_exec = "SU2_CFD"
fixedCL_naca0012.timeout = 1600
fixedCL_naca0012.tol = 0.00001
test_list.append(fixedCL_naca0012)
# Polar sweep of the inviscid NACA0012
polar_naca0012 = TestCase('polar_naca0012')
polar_naca0012.cfg_dir = "polar/naca0012"
polar_naca0012.cfg_file = "inv_NACA0012.cfg"
polar_naca0012.polar = True
polar_naca0012.test_iter = 10
polar_naca0012.test_vals = [-1.319488, 4.112397, 0.011954, 0.009584] #last 4 columns
polar_naca0012.su2_exec = "compute_polar.py -n 1 -i 11"
polar_naca0012.timeout = 1600
polar_naca0012.tol = 0.00001
test_list.append(polar_naca0012)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231916, 0.261866, -0.166832, 0.012717] #last 4 columns
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765426, -1.297422, 0.019496, 0.310082] #last 4 columns
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase('cylinder_lowmach')
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.850123, -1.388088, -0.056090, 108.140177] #last 4 columns
cylinder_lowmach.su2_exec = "SU2_CFD"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.442524, -5.441383, 0.884279, 0.024730] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.185243, 4.018464, 0.886786, 0.024927] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.069447, -7.354601, -0.187187, 0.010831] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438, 0.155815]#last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D results for finest grid: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000763, -9.145363, 1.070528, 0.019417] #last 4 columns
turb_naca0012_sa.su2_exec = "SU2_CFD"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D results for finest grid: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039675, -7.219913, 1.059622, 0.019138] #last 4 columns
turb_naca0012_sst.su2_exec = "SU2_CFD"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
# PROPELLER
propeller = TestCase('propeller')
propeller.cfg_dir = "rans/propeller"
propeller.cfg_file = "propeller.cfg"
propeller.test_iter = 10
propeller.test_vals = [-3.380312, -8.129519, 0.000043, 0.056159] #last 4 columns
propeller.su2_exec = "SU2_CFD"
propeller.timeout = 3200
propeller.tol = 0.00001
test_list.append(propeller)
#############################
### Incompressible Euler ###
#############################
# NACA0012 Hydrofoil
inc_euler_naca0012 = TestCase('inc_euler_naca0012')
inc_euler_naca0012.cfg_dir = "incomp_euler/naca0012"
inc_euler_naca0012.cfg_file = "incomp_NACA0012.cfg"
inc_euler_naca0012.test_iter = 20
inc_euler_naca0012.test_vals = [-3.590333,-3.151515,0.960192,0.013260] #last 4 columns
inc_euler_naca0012.su2_exec = "SU2_CFD"
inc_euler_naca0012.timeout = 1600
inc_euler_naca0012.tol = 0.00001
test_list.append(inc_euler_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710052, -11.007500, -0.000001, 0.210445] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#########################
### Transition ###
#########################
# Schubauer-Klebanoff Natural Transition
schubauer_klebanoff_transition = TestCase('Schubauer_Klebanoff')
schubauer_klebanoff_transition.cfg_dir = "transition/Schubauer_Klebanoff"
schubauer_klebanoff_transition.cfg_file = "transitional_BC_model_ConfigFile.cfg"
schubauer_klebanoff_transition.test_iter = 250
schubauer_klebanoff_transition.test_vals = [-9.474452, -15.630834, 0.000520, 0.001062] #last 4 columns
schubauer_klebanoff_transition.su2_exec = "SU2_CFD"
schubauer_klebanoff_transition.timeout = 1600
schubauer_klebanoff_transition.tol = 0.00001
test_list.append(schubauer_klebanoff_transition)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.787554, -15.192510, 0.300920, 0.019552] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.133352, -12.707213, 6.8590e-01, 0.007594] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
# Inviscid WEDGE: tests generalized adjoint
contadj_wedge = TestCase('contadj_wedge')
contadj_wedge.cfg_dir = "cont_adj_euler/wedge"
contadj_wedge.cfg_file = "inv_wedge_ROE.cfg"
contadj_wedge.test_iter = 10
contadj_wedge.test_vals = [2.780403, -3.223266, -1448300.000000, -0.000000] #last 4 columns
contadj_wedge.su2_exec = "SU2_CFD"
contadj_wedge.timeout = 1600
contadj_wedge.tol = 0.00001
test_list.append(contadj_wedge)
# Inviscid fixed CL NACA0012
contadj_fixedCL_naca0012 = TestCase('contadj_fixedcl_naca0012')
contadj_fixedCL_naca0012.cfg_dir = "fixed_cl/naca0012"
contadj_fixedCL_naca0012.cfg_file = "inv_NACA0012_ContAdj.cfg"
contadj_fixedCL_naca0012.test_iter = 500
contadj_fixedCL_naca0012.test_vals = [-2.896959, -8.484896, 0.250600, 0.000004] #last 4 columns
contadj_fixedCL_naca0012.su2_exec = "SU2_CFD"
contadj_fixedCL_naca0012.timeout = 1600
contadj_fixedCL_naca0012.tol = 0.00001
test_list.append(contadj_fixedCL_naca0012)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.677184, -9.141850, 2.056700, -0.000000] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.001210] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.012494] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, 19.169000, -0.000000] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.377843, -10.882446, -0.212470, 0.005448] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.980272, -12.146779, 1.9399, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718622, -7.027366, 2.932100, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Harmonic Balance ###
######################################
# Description of the regression test
harmonic_balance = TestCase('harmonic_balance')
harmonic_balance.cfg_dir = "harmonic_balance"
harmonic_balance.cfg_file = "HB.cfg"
harmonic_balance.test_iter = 25
harmonic_balance.test_vals = [-1.569573, 3.941896, 0.008780, 0.079775] #last 4 columns
harmonic_balance.su2_exec = "SU2_CFD"
harmonic_balance.timeout = 1600
harmonic_balance.tol = 0.00001
test_list.append(harmonic_balance)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.627934, -0.164470, 0.051972, 2.547034] #last 4 columns
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.709662, -2.274900, 1.418422, 1.734206] #last 4 columns
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.166406,0.076804,1.398548,2.197047] #last 4 columns
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
square_cylinder.unsteady = True
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.006222, -0.001342] #last 4 columns
sine_gust.su2_exec = "SU2_CFD"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077106, 0.036449, -1.684916e-03, -1.131735e-04] #last 4 columns
aeroelastic.su2_exec = "SU2_CFD"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# ls89_sa
ls89_sa = TestCase('ls89_sa')
ls89_sa.cfg_dir = "nicf/LS89"
ls89_sa.cfg_file = "turb_SA_PR.cfg"
ls89_sa.test_iter = 100
ls89_sa.test_vals = [-5.062991, -13.374292, 0.128005, 0.323965] #last 4 columns
ls89_sa.su2_exec = "SU2_CFD"
ls89_sa.timeout = 1600
ls89_sa.tol = 0.00001
test_list.append(ls89_sa)
# # ls89_sst
# ls89_sst = TestCase('ls89_sst')
# ls89_sst.cfg_dir = "nicf/LS89"
# ls89_sst.cfg_file = "turb_SST_PR.cfg"
# ls89_sst.test_iter = 100
# ls89_sst.test_vals = [-8.548266, -1.449437, 0.067986, 0.151168] #last 4 columns
# ls89_sst.su2_exec = "SU2_CFD"
# ls89_sst.timeout = 1600
# ls89_sst.tol = 0.00001
# test_list.append(ls89_sst)
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.055874, 1.117978, -0.000009, 0.000000] #last 4 columns
edge_VW.su2_exec = "SU2_CFD"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.484387, 0.656352, -0.000037, 0.000000] #last 4 columns
edge_PPR.su2_exec = "SU2_CFD"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### turboSU2 ###
######################################
# Mini centrifugal turbine blade
centrifugal_blade = TestCase('centrifugal_blade')
centrifugal_blade.cfg_dir = "turbomachinery/centrifugal_blade"
centrifugal_blade.cfg_file = "centrifugal_blade.cfg"
centrifugal_blade.test_iter = 100
centrifugal_blade.test_vals = [-9.106943, -0.460429, 1.069070e+01, 3.396010e-01] #last 4 columns
centrifugal_blade.su2_exec = "SU2_CFD"
centrifugal_blade.timeout = 1600
centrifugal_blade.tol = 0.000001
test_list.append(centrifugal_blade)
# Mini centrifugal turbine stage
centrifugal_stage = TestCase('centrifugal_stage')
centrifugal_stage.cfg_dir = "turbomachinery/centrifugal_stage"
centrifugal_stage.cfg_file = "centrifugal_stage.cfg"
centrifugal_stage.test_iter = 100
centrifugal_stage.test_vals = [-10.166628, 1.621134, 22.064950, 0.527107] #last 4 columns
centrifugal_stage.su2_exec = "SU2_CFD"
centrifugal_stage.timeout = 1600
centrifugal_stage.tol = 0.000001
test_list.append(centrifugal_stage)
######################################
### Sliding Mesh ###
######################################
# Uniform flow
# uniform_flow = TestCase('uniform_flow')
# uniform_flow.cfg_dir = "sliding_interface/uniform_flow"
# uniform_flow.cfg_file = "uniform_NN.cfg"
# uniform_flow.test_iter = 50
# uniform_flow.test_vals = [-0.368836, 5.156090, 0.000000, 0.000000] #last 4 columns
# uniform_flow.su2_exec = "SU2_CFD"
# uniform_flow.timeout = 1600
# uniform_flow.tol = 0.000001
# uniform_flow.unsteady = True
# test_list.append(uniform_flow)
# Channel_2D
channel_2D = TestCase('channel_2D')
channel_2D.cfg_dir = "sliding_interface/channel_2D"
channel_2D.cfg_file = "channel_2D_NN.cfg"
channel_2D.test_iter = 4
channel_2D.test_vals = [-1.498300, 4.541411, 0.000000, 0.000000] #last 4 columns
channel_2D.su2_exec = "SU2_CFD"
channel_2D.timeout = 100
channel_2D.tol = 0.00001
channel_2D.unsteady = True
test_list.append(channel_2D)
# Channel_3D
channel_3D = TestCase('channel_3D')
channel_3D.cfg_dir = "sliding_interface/channel_3D"
channel_3D.cfg_file = "channel_3D_NN.cfg"
channel_3D.test_iter = 1
channel_3D.test_vals = [-1.899948, 4.032874, 0.000000, 0.000000] #last 4 columns
channel_3D.su2_exec = "SU2_CFD"
channel_3D.timeout = 1600
channel_3D.tol = 0.00001
channel_3D.unsteady = True
test_list.append(channel_3D)
# Pipe
# pipe = TestCase('pipe')
# pipe.cfg_dir = "sliding_interface/pipe"
# pipe.cfg_file = "pipe_NN.cfg"
# pipe.test_iter = 2
# pipe.test_vals = [-3.503708, 3.194241, 0.000000, 0.000000] #last 4 columns
# pipe.su2_exec = "SU2_CFD"
# pipe.timeout = 1600
# pipe.tol = 0.00001
# pipe.unsteady = True
# test_list.append(pipe)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase('statbeam3d')
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-8.498274, -8.230638, -8.123824, 6.4095e+04] #last 4 columns
statbeam3d.su2_exec = "SU2_CFD"
statbeam3d.timeout = 1600
statbeam3d.tol = 0.00001
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase('dynbeam2d')
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-9.420640, -5.365872, -12.430382, 6.5210e+04] #last 4 columns
dynbeam2d.su2_exec = "SU2_CFD"
dynbeam2d.timeout = 1600
dynbeam2d.tol = 0.00001
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase('fsi2d')
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI_2D.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [2.000000, 0.500000, -7.777916, -1.139835] #last 4 columns
fsi2d.su2_exec = "SU2_CFD"
fsi2d.timeout = 1600
fsi2d.tol = 0.00001
test_list.append(fsi2d)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
######################################
### RUN SU2_GEO TESTS ###
######################################
# NACA0012
naca0012_geo = TestCase('naca0012_geo')
naca0012_geo.cfg_dir = "optimization_euler/steady_naca0012"
naca0012_geo.cfg_file = "inv_NACA0012_adv.cfg"
naca0012_geo.test_vals = [0.120011, 0.0816925, 0.0, 1.0] #max thickness, area, twist, chord
naca0012_geo.su2_exec = "SU2_GEO"
naca0012_geo.timeout = 1600
naca0012_geo.tol = 0.00001
pass_list.append(naca0012_geo.run_geo())
test_list.append(naca0012_geo)
######################################
### RUN SU2_DEF TESTS ###
######################################
# Inviscid NACA0012 (triangles)
naca0012_def = TestCase('naca0012_def')
naca0012_def.cfg_dir = "deformation/naca0012"
naca0012_def.cfg_file = "def_NACA0012.cfg"
naca0012_def.test_iter = 400
naca0012_def.test_vals = [4.30698e-15] #residual
naca0012_def.su2_exec = "SU2_DEF"
naca0012_def.timeout = 1600
naca0012_def.tol = 1e-15
pass_list.append(naca0012_def.run_def())
test_list.append(naca0012_def)
# RAE2822 (mixed tris + quads)
rae2822_def = TestCase('rae2822_def')
rae2822_def.cfg_dir = "deformation/rae2822"
rae2822_def.cfg_file = "def_RAE2822.cfg"
rae2822_def.test_iter = 150
rae2822_def.test_vals = [5.59336e-16] #residual
rae2822_def.su2_exec = "SU2_DEF"
rae2822_def.timeout = 1600
rae2822_def.tol = 1e-16
pass_list.append(rae2822_def.run_def())
test_list.append(rae2822_def)
# Turb NACA4412 (quads, wall distance)
naca4412_def = TestCase('naca4412_def')
naca4412_def.cfg_dir = "deformation/naca4412"
naca4412_def.cfg_file = "def_NACA4412.cfg"
naca4412_def.test_iter = 300
naca4412_def.test_vals = [3.26428e-15] #residual
naca4412_def.su2_exec = "SU2_DEF"
naca4412_def.timeout = 1600
naca4412_def.tol = 1e-15
pass_list.append(naca4412_def.run_def())
test_list.append(naca4412_def)
# Brick of tets (inverse volume)
brick_tets_def = TestCase('brick_tets_def')
brick_tets_def.cfg_dir = "deformation/brick_tets"
brick_tets_def.cfg_file = "def_brick_tets.cfg"
brick_tets_def.test_iter = 50
brick_tets_def.test_vals = [7.34025e-15] #residual
brick_tets_def.su2_exec = "SU2_DEF"
brick_tets_def.timeout = 1600
brick_tets_def.tol = 1e-15
pass_list.append(brick_tets_def.run_def())
test_list.append(brick_tets_def)
# Brick of isotropic hexas (inverse volume)
brick_hex_def = TestCase('brick_hex_def')
brick_hex_def.cfg_dir = "deformation/brick_hex"
brick_hex_def.cfg_file = "def_brick_hex.cfg"
brick_hex_def.test_iter = 50
brick_hex_def.test_vals = [1.55154e-15] #residual
brick_hex_def.su2_exec = "SU2_DEF"
brick_hex_def.timeout = 1600
brick_hex_def.tol = 1e-15
pass_list.append(brick_hex_def.run_def())
test_list.append(brick_hex_def)
# Brick with a pyramid layer (inverse volume)
brick_pyra_def = TestCase('brick_pyra_def')
brick_pyra_def.cfg_dir = "deformation/brick_pyra"
brick_pyra_def.cfg_file = "def_brick_pyra.cfg"
brick_pyra_def.test_iter = 400
brick_pyra_def.test_vals = [3.79432e-15] #residual
brick_pyra_def.su2_exec = "SU2_DEF"
brick_pyra_def.timeout = 1600
brick_pyra_def.tol = 1e-15
pass_list.append(brick_pyra_def.run_def())
test_list.append(brick_pyra_def)
# Brick of isotropic prisms (inverse volume)
brick_prism_def = TestCase('brick_prism_def')
brick_prism_def.cfg_dir = "deformation/brick_prism"
brick_prism_def.cfg_file = "def_brick_prism.cfg"
brick_prism_def.test_iter = 150
brick_prism_def.test_vals = [9.14366e-15] #residual
brick_prism_def.su2_exec = "SU2_DEF"
brick_prism_def.timeout = 1600
brick_prism_def.tol = 1e-15
pass_list.append(brick_prism_def.run_def())
test_list.append(brick_prism_def)
# Brick of prisms with high aspect ratio cells near the wall (wall distance)
brick_prism_rans_def = TestCase('brick_prism_rans_def')
brick_prism_rans_def.cfg_dir = "deformation/brick_prism_rans"
brick_prism_rans_def.cfg_file = "def_brick_prism_rans.cfg"
brick_prism_rans_def.test_iter = 100
brick_prism_rans_def.test_vals = [1.64462e-15] #residual
brick_prism_rans_def.su2_exec = "SU2_DEF"
brick_prism_rans_def.timeout = 1600
brick_prism_rans_def.tol = 1e-15
pass_list.append(brick_prism_rans_def.run_def())
test_list.append(brick_prism_rans_def)
# Brick of hexas with high aspect ratio cells near the wall (inverse volume)
brick_hex_rans_def = TestCase('brick_hex_rans_def')
brick_hex_rans_def.cfg_dir = "deformation/brick_hex_rans"
brick_hex_rans_def.cfg_file = "def_brick_hex_rans.cfg"
brick_hex_rans_def.test_iter = 50
brick_hex_rans_def.test_vals = [9.26657e-16] #residual
brick_hex_rans_def.su2_exec = "SU2_DEF"
brick_hex_rans_def.timeout = 1600
brick_hex_rans_def.tol = 1e-16
pass_list.append(brick_hex_rans_def.run_def())
test_list.append(brick_hex_rans_def)
# Cylindrical FFD test
cylinder_ffd_def = TestCase('cylinder_ffd_def')
cylinder_ffd_def.cfg_dir = "deformation/cylindrical_ffd"
cylinder_ffd_def.cfg_file = "def_cylindrical.cfg"
cylinder_ffd_def.test_iter = 50
cylinder_ffd_def.test_vals = [1.30556e-10] #residual
cylinder_ffd_def.su2_exec = "SU2_DEF"
cylinder_ffd_def.timeout = 1600
cylinder_ffd_def.tol = 1e-16
pass_list.append(cylinder_ffd_def.run_def())
test_list.append(cylinder_ffd_def)
# Spherical FFD test
sphere_ffd_def = TestCase('sphere_ffd_def')
sphere_ffd_def.cfg_dir = "deformation/spherical_ffd"
sphere_ffd_def.cfg_file = "def_spherical.cfg"
sphere_ffd_def.test_iter = 50
sphere_ffd_def.test_vals = [1.09326e-10] #residual
sphere_ffd_def.su2_exec = "SU2_DEF"
sphere_ffd_def.timeout = 1600
sphere_ffd_def.tol = 1e-16
pass_list.append(sphere_ffd_def.run_def())
test_list.append(sphere_ffd_def)
# Spherical FFD test using BSplines
sphere_ffd_def_bspline = TestCase('sphere_ffd_def_bspline')
sphere_ffd_def_bspline.cfg_dir = "deformation/spherical_ffd"
sphere_ffd_def_bspline.cfg_file = "def_spherical_bspline.cfg"
sphere_ffd_def_bspline.test_iter = 50
sphere_ffd_def_bspline.test_vals = [6.69927e-11] #residual
sphere_ffd_def_bspline.su2_exec = "SU2_DEF"
sphere_ffd_def_bspline.timeout = 1600
sphere_ffd_def_bspline.tol = 1e-16
pass_list.append(sphere_ffd_def_bspline.run_def())
test_list.append(sphere_ffd_def_bspline)
######################################
### RUN PYTHON TESTS ###
######################################
# test continuous_adjoint.py
contadj_euler_py = TestCase('contadj_euler_py')
contadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
contadj_euler_py.cfg_file = "inv_NACA0012.cfg"
contadj_euler_py.test_iter = 10
contadj_euler_py.su2_exec = "continuous_adjoint.py"
contadj_euler_py.timeout = 1600
contadj_euler_py.reference_file = "of_grad_cd.dat.ref"
contadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(contadj_euler_py.run_filediff())
test_list.append(contadj_euler_py)
# test finite_difference.py
findiff_euler_py = TestCase('findiff_euler_py')
findiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
findiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
findiff_euler_py.test_iter = 10
findiff_euler_py.su2_exec = "finite_differences.py"
findiff_euler_py.timeout = 1600
findiff_euler_py.reference_file = "of_grad_findiff.dat.ref"
findiff_euler_py.test_file = "FINDIFF/of_grad_findiff.dat"
pass_list.append(findiff_euler_py.run_filediff())
test_list.append(findiff_euler_py)
# test shape_optimization.py
shape_opt_euler_py = TestCase('shape_opt_euler_py')
shape_opt_euler_py.cfg_dir = "optimization_euler/steady_naca0012"
shape_opt_euler_py.cfg_file = "inv_NACA0012_adv.cfg"
shape_opt_euler_py.test_iter = 1
shape_opt_euler_py.test_vals = [1, 1, 2.134974E-05, 3.829535E-03] #last 4 columns
shape_opt_euler_py.su2_exec = "shape_optimization.py -f"
shape_opt_euler_py.timeout = 1600
shape_opt_euler_py.tol = 0.00001
pass_list.append(shape_opt_euler_py.run_opt())
test_list.append(shape_opt_euler_py)
# test continuous_adjoint.py, with multiple objectives
#contadj_multi_py = TestCase('contadj_multi_py')
#contadj_multi_py.cfg_dir = "cont_adj_euler/wedge"
#contadj_multi_py.cfg_file = "inv_wedge_ROE_multiobj.cfg"
#contadj_multi_py.test_iter = 10
#contadj_multi_py.su2_exec = "continuous_adjoint.py"
#contadj_multi_py.timeout = 1600
#contadj_multi_py.reference_file = "of_grad_combo.dat.ref"
#contadj_multi_py.test_file = "of_grad_combo.dat"
#pass_list.append(contadj_multi_py.run_filediff())
#test_list.append(contadj_multi_py)
##########################
### Python wrapper ###
##########################
# NACA0012
pywrapper_naca0012 = TestCase('pywrapper_naca0012')
pywrapper_naca0012.cfg_dir = "euler/naca0012"
pywrapper_naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
pywrapper_naca0012.test_iter = 100
pywrapper_naca0012.test_vals = [-6.191618, -5.592802, 0.334809, 0.022197] #last 4 columns
pywrapper_naca0012.su2_exec = "SU2_CFD.py -f"
pywrapper_naca0012.timeout = 1600
pywrapper_naca0012.tol = 0.00001
test_list.append(pywrapper_naca0012)
pass_list.append(pywrapper_naca0012.run_test())
# NACA0012 (SST, FUN3D results for finest grid: CL=1.0840, CD=0.01253)
pywrapper_turb_naca0012_sst = TestCase('pywrapper_turb_naca0012_sst')
pywrapper_turb_naca0012_sst.cfg_dir = "rans/naca0012"
pywrapper_turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
pywrapper_turb_naca0012_sst.test_iter = 10
pywrapper_turb_naca0012_sst.test_vals = [-15.039675, -7.219913, 1.059622, 0.019138] #last 4 columns
pywrapper_turb_naca0012_sst.su2_exec = "SU2_CFD.py -f"
pywrapper_turb_naca0012_sst.timeout = 3200
pywrapper_turb_naca0012_sst.tol = 0.00001
test_list.append(pywrapper_turb_naca0012_sst)
pass_list.append(pywrapper_turb_naca0012_sst.run_test())
# Square cylinder
pywrapper_square_cylinder = TestCase('pywrapper_square_cylinder')
pywrapper_square_cylinder.cfg_dir = "unsteady/square_cylinder"
pywrapper_square_cylinder.cfg_file = "turb_square.cfg"
pywrapper_square_cylinder.test_iter = 3
pywrapper_square_cylinder.test_vals = [-1.166406,0.076804,1.398548,2.197047] #last 4 columns
pywrapper_square_cylinder.su2_exec = "SU2_CFD.py -f"
pywrapper_square_cylinder.timeout = 1600
pywrapper_square_cylinder.tol = 0.00001
pywrapper_square_cylinder.unsteady = True
test_list.append(pywrapper_square_cylinder)
pass_list.append(pywrapper_square_cylinder.run_test())
# Aeroelastic
pywrapper_aeroelastic = TestCase('pywrapper_aeroelastic')
pywrapper_aeroelastic.cfg_dir = "aeroelastic"
pywrapper_aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
pywrapper_aeroelastic.test_iter = 2
pywrapper_aeroelastic.test_vals = [0.077106, 0.036449, -1.684916e-03, -1.131735e-04] #last 4 columns
pywrapper_aeroelastic.su2_exec = "SU2_CFD.py -f"
pywrapper_aeroelastic.timeout = 1600
pywrapper_aeroelastic.tol = 0.000001
pywrapper_aeroelastic.unsteady = True
test_list.append(pywrapper_aeroelastic)
pass_list.append(pywrapper_aeroelastic.run_test())
# FSI, 2d
pywrapper_fsi2d = TestCase('pywrapper_fsi2d')
pywrapper_fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
pywrapper_fsi2d.cfg_file = "configFSI_2D.cfg"
pywrapper_fsi2d.test_iter = 4
pywrapper_fsi2d.test_vals = [2.000000, 0.500000, -7.777916, -1.139835] #last 4 columns
pywrapper_fsi2d.su2_exec = "SU2_CFD.py --nZone 2 --fsi True -f"
pywrapper_fsi2d.timeout = 1600
pywrapper_fsi2d.tol = 0.00001
test_list.append(pywrapper_fsi2d)
pass_list.append(pywrapper_fsi2d.run_test())
# Tests summary
print '=================================================================='
print 'Summary of the serial tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s'%test.tag
else:
print '* FAILED - %s'%test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ[
'SU2_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2'
os.environ[
'SU2_RUN'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir(os.environ['SU2_HOME'])
os.system('git pull')
# Build SU2_CFD in serial using autoconf
os.system('./configure --prefix=$SU2_HOME CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.489214, 2.821231, 0.008730, 0.053947]
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.203359, -5.582393, 0.334818, 0.022197]
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-2.703316, 3.192215, -0.252410, 0.044446]
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.830417, -4.273125, 0.290066, 0.015809]
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.227537, 0.267007, -0.167233, 0.012854]
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.764866, -1.296840, -0.024986, 0.974669]
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.542705, -5.430675, 0.884353,
0.024153] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.214015, 4.020029, 0.884881,
0.024141] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.068405, -7.340795, -0.187223,
0.010395] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327517, -6.563378, 0.230436,
0.155816] #last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.826334, -7.364207, -0.000025,
0.803037] #last 4 columns
turb_naca0012.su2_exec = "SU2_CFD"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709986, -11.007545, 0.000008,
0.210347] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-12.206764, -16.000000, 0.005483,
0.536870] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.353629, -6.525887, -0.000023,
0.147720] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [
-0.599698, -6.065249, -0.032305, 25.115000
] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [
-4.234330, -9.705736, 0.005161, 0.398940
] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [
-1.810435, -6.920519, 0.014614, 1.020100
] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [
-4.351102, -8.919996, -1.275200, -2.541400
] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [
-2.870304, -8.350308, 4.5270e+00, 3.5527e-01
] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [
-7.551025, -7.377690, 0.010910, 0.000000
] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [
-2.423636, -2.916834, -0.048414, 0.000000
] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119, 2.854417, -4.439628, 0.000188]
ramc.su2_exec = "SU2_CFD"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.940515, -0.480469, 0.018068, -3.926360]
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.744370, -1.298814, 8.697757, 0.133608]
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.542160, 0.048661, 1.398952, 2.196894]
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ['SU2_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2'
os.environ['SU2_RUN'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir( os.environ['SU2_HOME'] )
os.system('git pull')
# Build SU2_CFD in serial using autoconf
os.system('./configure --prefix=$SU2_HOME CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.489827,2.821844,0.008730,0.053947]
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.195996,-5.597033,0.334818,0.022197]
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-2.717009,3.183742,-0.252144,0.044399]
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.819422,-4.284121,0.290066,0.015809]
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.225114,0.270273,0.020536,0.012860]
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.781338,-1.335300,-0.025054,0.974312]
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822
rae2822 = TestCase('rae2822')
rae2822.cfg_dir = "rans/rae2822"
rae2822.cfg_file = "turb_SA_RAE2822.cfg"
rae2822.test_iter = 100
rae2822.test_vals = [-3.559272,-5.452676,0.884380,0.024162] #last 4 columns
rae2822.su2_exec = "SU2_CFD"
rae2822.timeout = 1600
rae2822.tol = 0.00001
test_list.append(rae2822)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.074224,-7.332708,0.000505,0.010354] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.343659,-6.584583,0.230390,0.155769]#last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.824671,-7.364141,-0.000026,0.803047] #last 4 columns
turb_naca0012.su2_exec = "SU2_CFD"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709981,-11.007623,0.000008,0.210345] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 100
contadj_naca0012.test_vals = [-4.882472,-10.149505,0.006059,0.519590] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid RAM-C (To be validated with finite differences)
contadj_ram_c = TestCase('contadj_ram_c')
contadj_ram_c.cfg_dir = "cont_adj_euler/ram_c"
contadj_ram_c.cfg_file = "inv_RAMC.cfg"
contadj_ram_c.test_iter = 100
contadj_ram_c.test_vals = [0.776609,-7.308868,-0.001885,0.080464] #last 4 columns
contadj_ram_c.su2_exec = "SU2_CFD"
contadj_ram_c.timeout = 1600
contadj_ram_c.tol = 0.00001
test_list.append(contadj_ram_c)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [2.467226,-2.105465,0.555930,93.625000] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012
contadj_ns_naca0012 = TestCase('contadj_ns_naca0012')
contadj_ns_naca0012.cfg_dir = "cont_adj_navierstokes/naca0012"
contadj_ns_naca0012.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012.test_iter = 100
contadj_ns_naca0012.test_vals = [-0.012901,-5.322715,0.896630,-0.045627] #last 4 columns
contadj_ns_naca0012.su2_exec = "SU2_CFD"
contadj_ns_naca0012.timeout = 1600
contadj_ns_naca0012.tol = 0.00001
test_list.append(contadj_ns_naca0012)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012 (To be validated with finite differences)
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-5.356749,-8.622049,18.310000,-0.000000] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [-7.644867,-7.179288,0.011112,0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-9.002576,-10.097248,0.048091,0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119,2.854417,-4.439634,0.000188]
ramc.su2_exec = "SU2_CFD"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### Spectral Method ###
######################################
spectral = TestCase('spectral')
spectral.cfg_dir = "spectral_method"
spectral.cfg_file = "spectral.cfg"
spectral.test_iter = 25
spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
spectral.su2_exec = "SU2_CFD"
spectral.timeout = 1600
spectral.tol = 0.00001
test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.957018,-0.518901,0.017833,-3.937129]
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.754859,-1.333184,8.912235,0.163860]
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.585044,-1.425752,1.490389,2.340439]
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU^2 and ensures that the output matches specified values.
This will be used to do nightly checks to make sure nothing is broken. '''
workdir = os.getcwd()
# environment variables for SU2
os.environ[
'SU2_HOME'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2'
os.environ[
'SU2_RUN'] = '/home/ale11/.cruise/projects/serial_regression/work/SU2/bin'
os.environ['PATH'] = os.environ['PATH'] + ':' + os.environ['SU2_RUN']
# sync SU2 repo
os.chdir(os.environ['SU2_HOME'])
os.system('git fetch')
os.system('git checkout develop')
os.system('git pull origin develop')
# Build SU2_CFD in serial using autoconf
os.system('./configure --prefix=$SU2_HOME CXXFLAGS="-O3"')
os.system('make clean')
os.system('make install')
os.chdir(os.environ['SU2_RUN'])
if not os.path.exists("./SU2_CFD"):
print 'Could not build SU2_CFD'
sys.exit(1)
os.chdir(workdir)
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.110240, 2.263506, 0.008686, 0.029098]
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.198537, -5.577721, 0.334810, 0.022197]
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.711318, 3.913749, -0.252131, 0.044402]
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6_JST.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-4.715342, -4.148920, 0.271678, 0.018869]
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.228462, 0.265581, -0.166503, 0.013013]
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765426, -1.297422, 0.019501, 0.310134]
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.442525, -5.441383, 0.884279,
0.024730] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.186943, 4.023140, 0.886788,
0.024927] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.067553, -7.354291, -0.187192,
0.010831] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327516, -6.563376, 0.230437,
0.155816] #last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012
turb_naca0012 = TestCase('turb_naca0012')
turb_naca0012.cfg_dir = "rans/naca0012"
turb_naca0012.cfg_file = "turb_NACA0012.cfg"
turb_naca0012.test_iter = 20
turb_naca0012.test_vals = [-2.826358, -7.364211, -0.000020,
0.803040] #last 4 columns
turb_naca0012.su2_exec = "SU2_CFD"
turb_naca0012.timeout = 3200
turb_naca0012.tol = 0.00001
test_list.append(turb_naca0012)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710052, -11.007500, -0.000001,
0.210445] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-12.215877, -17.724135, 0.300920,
0.536870] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 5
contadj_oneram6.test_vals = [-6.354670, -6.530109, -0.133220,
0.147720] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [
-0.601729, -6.067386, -2.056900, 25.115000
] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [
-4.234330, -9.705736, 0.516750, 0.398940
] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [
-1.810435, -6.920519, 1.756200, 1.020100
] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [
-4.351102, -8.919996, -72.511000, -2.541400
] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [
-2.959224, -8.349094, 354.120000, 0.106450
] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 140
contadj_incomp_NACA0012.test_vals = [
-7.326112, -7.153756, 1.892600, 0.000000
] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [
-2.476381, -2.941665, -3.081400, 0.000000
] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.638119, 2.854417, -4.439628, 0.000188]
ramc.su2_exec = "SU2_CFD"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.627883, -0.164418, 0.051983, 2.546202]
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-6.851254, -1.408408, 9.093772, 0.060754]
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.542156, 0.048662, 1.398952, 2.196893]
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
######################################
### Real_Gas ###
######################################
# ls89_sa
ls89_sa = TestCase('ls89_sa')
ls89_sa.cfg_dir = "nicf/LS89"
ls89_sa.cfg_file = "turb_SA_PR.cfg"
ls89_sa.test_iter = 100
ls89_sa.test_vals = [-7.042593, -12.006909, 0.067512, 0.149691]
ls89_sa.su2_exec = "SU2_CFD"
ls89_sa.timeout = 1600
ls89_sa.tol = 0.00001
test_list.append(ls89_sa)
# ls89_sst
ls89_sst = TestCase('ls89_sst')
ls89_sst.cfg_dir = "nicf/LS89"
ls89_sst.cfg_file = "turb_SST_PR.cfg"
ls89_sst.test_iter = 100
ls89_sst.test_vals = [-8.901539, -1.625729, 0.067796, 0.151151]
ls89_sst.su2_exec = "SU2_CFD"
ls89_sst.timeout = 1600
ls89_sst.tol = 0.00001
test_list.append(ls89_sst)
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.728637, -3.272400, -0.000046, 0.000000]
edge_VW.su2_exec = "SU2_CFD"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-6.278519, -3.849022, -0.000056, 0.000000]
edge_PPR.su2_exec = "SU2_CFD"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.110240, 2.263506, 0.008686,
0.029098] #last 4 columns
channel.su2_exec = "SU2_CFD"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.191618, -5.592802, 0.334809,
0.022197] #last 4 columns
naca0012.su2_exec = "SU2_CFD"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.769374, 3.848733, -0.252191,
0.044410] #last 4 columns
wedge.su2_exec = "SU2_CFD"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.393130, -12.928941, 0.282557,
0.012706] #last 4 columns
oneram6.su2_exec = "SU2_CFD"
oneram6.timeout = 9600
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231916, 0.261866, -0.166832,
0.012717] #last 4 columns
flatplate.su2_exec = "SU2_CFD"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.765426, -1.297422, 0.019496,
0.310082] #last 4 columns
cylinder.su2_exec = "SU2_CFD"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase('cylinder_lowmach')
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.850123, -1.388088, -0.056090,
108.140177] #last 4 columns
cylinder_lowmach.su2_exec = "SU2_CFD"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.442524, -5.441383, 0.884279,
0.024730] #last 4 columns
rae2822_sa.su2_exec = "SU2_CFD"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.185243, 4.018464, 0.886786,
0.024927] #last 4 columns
rae2822_sst.su2_exec = "SU2_CFD"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.069447, -7.354601, -0.187187,
0.010831] #last 4 columns
turb_flatplate.su2_exec = "SU2_CFD"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438,
0.155815] #last 4 columns
turb_oneram6.su2_exec = "SU2_CFD"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D results for finest grid: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000763, -9.145363, 1.070528,
0.019417] #last 4 columns
turb_naca0012_sa.su2_exec = "SU2_CFD"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D results for finest grid: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039675, -7.219913, 1.059622,
0.019138] #last 4 columns
turb_naca0012_sst.su2_exec = "SU2_CFD"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710052, -11.007500, -0.000001,
0.210445] #last 4 columns
inc_turb_naca0012.su2_exec = "SU2_CFD"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.787554, -15.192510, 0.300920,
0.536870] #last 4 columns
contadj_naca0012.su2_exec = "SU2_CFD"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [
-12.133352, -12.707213, 6.8590e-01, 1.4092e-01
] #last 4 columns
contadj_oneram6.su2_exec = "SU2_CFD"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
# Inviscid WEDGE: tests generalized adjoint
contadj_wedge = TestCase('contadj_wedge')
contadj_wedge.cfg_dir = "cont_adj_euler/wedge"
contadj_wedge.cfg_file = "inv_wedge_ROE.cfg"
contadj_wedge.test_iter = 10
contadj_wedge.test_vals = [
2.780403, -3.223266, -1448300.000000, -0.000004
] #last 4 columns
contadj_wedge.su2_exec = "SU2_CFD"
contadj_wedge.timeout = 1600
contadj_wedge.tol = 0.00001
test_list.append(contadj_wedge)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.677184, -9.141850, 2.056700,
4.497000] #last 4 columns
contadj_ns_cylinder.su2_exec = "SU2_CFD"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [
-2.744551, -8.216469, 0.518810, 0.229160
] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "SU2_CFD"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [
-1.041539, -6.578524, 1.772300, 0.620880
] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "SU2_CFD"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [
-0.814757, -5.726517, 19.169000, -2.994100
] #last 4 columns
contadj_rans_naca0012.su2_exec = "SU2_CFD"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae2822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [
-5.377843, -10.882446, -0.212470, 0.269390
] #last 4 columns
contadj_rans_rae2822.su2_exec = "SU2_CFD"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [
-11.980272, -12.146779, 1.9399, 0.000000
] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "SU2_CFD"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [
-5.718622, -7.027366, 2.932100, 0.000000
] #last 4 columns
contadj_incomp_cylinder.su2_exec = "SU2_CFD"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
# ######################################
# ### Spectral Method ###
# ######################################
# spectral = TestCase('spectral')
# spectral.cfg_dir = "spectral_method"
# spectral.cfg_file = "spectral.cfg"
# spectral.test_iter = 25
# spectral.test_vals = [-1.621870,3.852164,0.007465,0.084358]
# spectral.su2_exec = "SU2_CFD"
# spectral.timeout = 1600
# spectral.tol = 0.00001
# test_list.append(spectral)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.627934, -0.164470, 0.051972,
2.547034] #last 4 columns
cavity.su2_exec = "SU2_CFD"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.709662, -2.274900, 1.418422,
1.734206] #last 4 columns
spinning_cylinder.su2_exec = "SU2_CFD"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.166406, 0.076804, 1.398548,
2.197047] #last 4 columns
square_cylinder.su2_exec = "SU2_CFD"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
square_cylinder.unsteady = True
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.006222,
-0.001342] #last 4 columns
sine_gust.su2_exec = "SU2_CFD"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077106, 0.036449, -1.684916e-03,
-1.131735e-04] #last 4 columns
aeroelastic.su2_exec = "SU2_CFD"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# ls89_sa
ls89_sa = TestCase('ls89_sa')
ls89_sa.cfg_dir = "nicf/LS89"
ls89_sa.cfg_file = "turb_SA_PR.cfg"
ls89_sa.test_iter = 100
ls89_sa.test_vals = [-5.062991, -13.374292, 0.128005,
0.323965] #last 4 columns
ls89_sa.su2_exec = "SU2_CFD"
ls89_sa.timeout = 1600
ls89_sa.tol = 0.00001
test_list.append(ls89_sa)
# # ls89_sst
# ls89_sst = TestCase('ls89_sst')
# ls89_sst.cfg_dir = "nicf/LS89"
# ls89_sst.cfg_file = "turb_SST_PR.cfg"
# ls89_sst.test_iter = 100
# ls89_sst.test_vals = [-8.548266, -1.449437, 0.067986, 0.151168] #last 4 columns
# ls89_sst.su2_exec = "SU2_CFD"
# ls89_sst.timeout = 1600
# ls89_sst.tol = 0.00001
# test_list.append(ls89_sst)
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.055874, 1.117978, -0.000009,
0.000000] #last 4 columns
edge_VW.su2_exec = "SU2_CFD"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.484387, 0.656352, -0.000037,
0.000000] #last 4 columns
edge_PPR.su2_exec = "SU2_CFD"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### turboSU2 ###
######################################
# Mini centrifugal turbine blade
centrifugal_blade = TestCase('centrifugal_blade')
centrifugal_blade.cfg_dir = "turbomachinery/centrifugal_blade"
centrifugal_blade.cfg_file = "centrifugal_blade.cfg"
centrifugal_blade.test_iter = 100
centrifugal_blade.test_vals = [
-9.106943, -0.460429, 1.069070e+01, 3.396010e-01
] #last 4 columns
centrifugal_blade.su2_exec = "SU2_CFD"
centrifugal_blade.timeout = 1600
centrifugal_blade.tol = 0.000001
test_list.append(centrifugal_blade)
# Mini centrifugal turbine stage
centrifugal_stage = TestCase('centrifugal_stage')
centrifugal_stage.cfg_dir = "turbomachinery/centrifugal_stage"
centrifugal_stage.cfg_file = "centrifugal_stage.cfg"
centrifugal_stage.test_iter = 100
centrifugal_stage.test_vals = [
-10.166364, 1.621172, 2.206476e+01, 5.271075e-01
] #last 4 columns
centrifugal_stage.su2_exec = "SU2_CFD"
centrifugal_stage.timeout = 1600
centrifugal_stage.tol = 0.000001
test_list.append(centrifugal_stage)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase('statbeam3d')
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-8.498274, -8.230638, -8.123824,
6.4095e+04] #last 4 columns
statbeam3d.su2_exec = "SU2_CFD"
statbeam3d.timeout = 1600
statbeam3d.tol = 0.00001
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase('dynbeam2d')
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-9.420640, -5.365872, -12.430382,
6.5210e+04] #last 4 columns
dynbeam2d.su2_exec = "SU2_CFD"
dynbeam2d.timeout = 1600
dynbeam2d.tol = 0.00001
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase('fsi2d')
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI_2D.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [2.000000, 0.500000, -7.777916,
-1.139835] #last 4 columns
fsi2d.su2_exec = "SU2_CFD"
fsi2d.timeout = 1600
fsi2d.tol = 0.00001
test_list.append(fsi2d)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
######################################
### RUN SU2_GEO TESTS ###
######################################
# NACA0012
naca0012_geo = TestCase('naca0012_geo')
naca0012_geo.cfg_dir = "optimization_euler/steady_naca0012"
naca0012_geo.cfg_file = "inv_NACA0012_adv.cfg"
naca0012_geo.test_vals = [0.120011, 0.0816925, 0.0,
1.0] #max thickness, area, twist, chord
naca0012_geo.su2_exec = "SU2_GEO"
naca0012_geo.timeout = 1600
naca0012_geo.tol = 0.00001
pass_list.append(naca0012_geo.run_geo())
test_list.append(naca0012_geo)
######################################
### RUN SU2_DEF TESTS ###
######################################
# Inviscid NACA0012 (triangles)
naca0012_def = TestCase('naca0012_def')
naca0012_def.cfg_dir = "deformation/naca0012"
naca0012_def.cfg_file = "def_NACA0012.cfg"
naca0012_def.test_iter = 400
naca0012_def.test_vals = [4.30698e-15] #residual
naca0012_def.su2_exec = "SU2_DEF"
naca0012_def.timeout = 1600
naca0012_def.tol = 1e-15
pass_list.append(naca0012_def.run_def())
test_list.append(naca0012_def)
# RAE2822 (mixed tris + quads)
rae2822_def = TestCase('rae2822_def')
rae2822_def.cfg_dir = "deformation/rae2822"
rae2822_def.cfg_file = "def_RAE2822.cfg"
rae2822_def.test_iter = 150
rae2822_def.test_vals = [5.59336e-16] #residual
rae2822_def.su2_exec = "SU2_DEF"
rae2822_def.timeout = 1600
rae2822_def.tol = 1e-16
pass_list.append(rae2822_def.run_def())
test_list.append(rae2822_def)
# Turb NACA4412 (quads, wall distance)
naca4412_def = TestCase('naca4412_def')
naca4412_def.cfg_dir = "deformation/naca4412"
naca4412_def.cfg_file = "def_NACA4412.cfg"
naca4412_def.test_iter = 300
naca4412_def.test_vals = [3.26428e-15] #residual
naca4412_def.su2_exec = "SU2_DEF"
naca4412_def.timeout = 1600
naca4412_def.tol = 1e-15
pass_list.append(naca4412_def.run_def())
test_list.append(naca4412_def)
# Brick of tets (inverse volume)
brick_tets_def = TestCase('brick_tets_def')
brick_tets_def.cfg_dir = "deformation/brick_tets"
brick_tets_def.cfg_file = "def_brick_tets.cfg"
brick_tets_def.test_iter = 50
brick_tets_def.test_vals = [7.34025e-15] #residual
brick_tets_def.su2_exec = "SU2_DEF"
brick_tets_def.timeout = 1600
brick_tets_def.tol = 1e-15
pass_list.append(brick_tets_def.run_def())
test_list.append(brick_tets_def)
# Brick of isotropic hexas (inverse volume)
brick_hex_def = TestCase('brick_hex_def')
brick_hex_def.cfg_dir = "deformation/brick_hex"
brick_hex_def.cfg_file = "def_brick_hex.cfg"
brick_hex_def.test_iter = 50
brick_hex_def.test_vals = [1.55154e-15] #residual
brick_hex_def.su2_exec = "SU2_DEF"
brick_hex_def.timeout = 1600
brick_hex_def.tol = 1e-15
pass_list.append(brick_hex_def.run_def())
test_list.append(brick_hex_def)
# Brick with a pyramid layer (inverse volume)
brick_pyra_def = TestCase('brick_pyra_def')
brick_pyra_def.cfg_dir = "deformation/brick_pyra"
brick_pyra_def.cfg_file = "def_brick_pyra.cfg"
brick_pyra_def.test_iter = 400
brick_pyra_def.test_vals = [3.79432e-15] #residual
brick_pyra_def.su2_exec = "SU2_DEF"
brick_pyra_def.timeout = 1600
brick_pyra_def.tol = 1e-15
pass_list.append(brick_pyra_def.run_def())
test_list.append(brick_pyra_def)
# Brick of isotropic prisms (inverse volume)
brick_prism_def = TestCase('brick_prism_def')
brick_prism_def.cfg_dir = "deformation/brick_prism"
brick_prism_def.cfg_file = "def_brick_prism.cfg"
brick_prism_def.test_iter = 150
brick_prism_def.test_vals = [9.14366e-15] #residual
brick_prism_def.su2_exec = "SU2_DEF"
brick_prism_def.timeout = 1600
brick_prism_def.tol = 1e-15
pass_list.append(brick_prism_def.run_def())
test_list.append(brick_prism_def)
# Brick of prisms with high aspect ratio cells near the wall (wall distance)
brick_prism_rans_def = TestCase('brick_prism_rans_def')
brick_prism_rans_def.cfg_dir = "deformation/brick_prism_rans"
brick_prism_rans_def.cfg_file = "def_brick_prism_rans.cfg"
brick_prism_rans_def.test_iter = 100
brick_prism_rans_def.test_vals = [1.64462e-15] #residual
brick_prism_rans_def.su2_exec = "SU2_DEF"
brick_prism_rans_def.timeout = 1600
brick_prism_rans_def.tol = 1e-15
pass_list.append(brick_prism_rans_def.run_def())
test_list.append(brick_prism_rans_def)
# Brick of hexas with high aspect ratio cells near the wall (inverse volume)
brick_hex_rans_def = TestCase('brick_hex_rans_def')
brick_hex_rans_def.cfg_dir = "deformation/brick_hex_rans"
brick_hex_rans_def.cfg_file = "def_brick_hex_rans.cfg"
brick_hex_rans_def.test_iter = 50
brick_hex_rans_def.test_vals = [9.26657e-16] #residual
brick_hex_rans_def.su2_exec = "SU2_DEF"
brick_hex_rans_def.timeout = 1600
brick_hex_rans_def.tol = 1e-16
pass_list.append(brick_hex_rans_def.run_def())
test_list.append(brick_hex_rans_def)
######################################
### RUN PYTHON TESTS ###
######################################
# test continuous_adjoint.py
contadj_euler_py = TestCase('contadj_euler_py')
contadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
contadj_euler_py.cfg_file = "inv_NACA0012.cfg"
contadj_euler_py.test_iter = 10
contadj_euler_py.su2_exec = "continuous_adjoint.py"
contadj_euler_py.timeout = 1600
contadj_euler_py.reference_file = "of_grad_cd.dat.ref"
contadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(contadj_euler_py.run_filediff())
test_list.append(contadj_euler_py)
# test finite_difference.py
findiff_euler_py = TestCase('findiff_euler_py')
findiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
findiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
findiff_euler_py.test_iter = 10
findiff_euler_py.su2_exec = "finite_differences.py"
findiff_euler_py.timeout = 1600
findiff_euler_py.reference_file = "of_grad_findiff.dat.ref"
findiff_euler_py.test_file = "FINDIFF/of_grad_findiff.dat"
pass_list.append(findiff_euler_py.run_filediff())
test_list.append(findiff_euler_py)
# test shape_optimization.py
shape_opt_euler_py = TestCase('shape_opt_euler_py')
shape_opt_euler_py.cfg_dir = "optimization_euler/steady_naca0012"
shape_opt_euler_py.cfg_file = "inv_NACA0012_adv.cfg"
shape_opt_euler_py.test_iter = 1
shape_opt_euler_py.test_vals = [1, 1, 2.134974E-05,
3.829535E-03] #last 4 columns
shape_opt_euler_py.su2_exec = "shape_optimization.py -f"
shape_opt_euler_py.timeout = 1600
shape_opt_euler_py.tol = 0.00001
pass_list.append(shape_opt_euler_py.run_opt())
test_list.append(shape_opt_euler_py)
# test continuous_adjoint.py, with multiple objectives
contadj_multi_py = TestCase('contadj_multi_py')
contadj_multi_py.cfg_dir = "cont_adj_euler/wedge"
contadj_multi_py.cfg_file = "inv_wedge_ROE_multiobj.cfg"
contadj_multi_py.test_iter = 10
contadj_multi_py.su2_exec = "continuous_adjoint.py"
contadj_multi_py.timeout = 1600
contadj_multi_py.reference_file = "of_grad_combo.dat.ref"
contadj_multi_py.test_file = "of_grad_combo.dat"
pass_list.append(contadj_multi_py.run_filediff())
test_list.append(contadj_multi_py)
##########################
### Python wrapper ###
##########################
# NACA0012
pywrapper_naca0012 = TestCase('pywrapper_naca0012')
pywrapper_naca0012.cfg_dir = "euler/naca0012"
pywrapper_naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
pywrapper_naca0012.test_iter = 100
pywrapper_naca0012.test_vals = [-6.191618, -5.592802, 0.334809,
0.022197] #last 4 columns
pywrapper_naca0012.su2_exec = "pyWrap_SU2_CFD.py -f"
pywrapper_naca0012.timeout = 1600
pywrapper_naca0012.tol = 0.00001
test_list.append(pywrapper_naca0012)
pass_list.append(pywrapper_naca0012.run_test())
# NACA0012 (SST, FUN3D results for finest grid: CL=1.0840, CD=0.01253)
pywrapper_turb_naca0012_sst = TestCase('pywrapper_turb_naca0012_sst')
pywrapper_turb_naca0012_sst.cfg_dir = "rans/naca0012"
pywrapper_turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
pywrapper_turb_naca0012_sst.test_iter = 10
pywrapper_turb_naca0012_sst.test_vals = [
-15.039675, -7.219913, 1.059622, 0.019138
] #last 4 columns
pywrapper_turb_naca0012_sst.su2_exec = "pyWrap_SU2_CFD.py -f"
pywrapper_turb_naca0012_sst.timeout = 3200
pywrapper_turb_naca0012_sst.tol = 0.00001
test_list.append(pywrapper_turb_naca0012_sst)
pass_list.append(pywrapper_turb_naca0012_sst.run_test())
# Square cylinder
pywrapper_square_cylinder = TestCase('pywrapper_square_cylinder')
pywrapper_square_cylinder.cfg_dir = "unsteady/square_cylinder"
pywrapper_square_cylinder.cfg_file = "turb_square.cfg"
pywrapper_square_cylinder.test_iter = 3
pywrapper_square_cylinder.test_vals = [
-1.166406, 0.076804, 1.398548, 2.197047
] #last 4 columns
pywrapper_square_cylinder.su2_exec = "pyWrap_SU2_CFD.py -f"
pywrapper_square_cylinder.timeout = 1600
pywrapper_square_cylinder.tol = 0.00001
pywrapper_square_cylinder.unsteady = True
test_list.append(pywrapper_square_cylinder)
pass_list.append(pywrapper_square_cylinder.run_test())
# Aeroelastic
pywrapper_aeroelastic = TestCase('pywrapper_aeroelastic')
pywrapper_aeroelastic.cfg_dir = "aeroelastic"
pywrapper_aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
pywrapper_aeroelastic.test_iter = 2
pywrapper_aeroelastic.test_vals = [
0.077106, 0.036449, -1.684916e-03, -1.131735e-04
] #last 4 columns
pywrapper_aeroelastic.su2_exec = "pyWrap_SU2_CFD.py -f"
pywrapper_aeroelastic.timeout = 1600
pywrapper_aeroelastic.tol = 0.000001
pywrapper_aeroelastic.unsteady = True
test_list.append(pywrapper_aeroelastic)
pass_list.append(pywrapper_aeroelastic.run_test())
# FSI, 2d
pywrapper_fsi2d = TestCase('pywrapper_fsi2d')
pywrapper_fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
pywrapper_fsi2d.cfg_file = "configFSI_2D.cfg"
pywrapper_fsi2d.test_iter = 4
pywrapper_fsi2d.test_vals = [2.000000, 0.500000, -7.777916,
-1.139835] #last 4 columns
pywrapper_fsi2d.su2_exec = "pyWrap_SU2_CFD.py --nZone 2 --fsi True -f"
pywrapper_fsi2d.timeout = 1600
pywrapper_fsi2d.tol = 0.00001
test_list.append(pywrapper_fsi2d)
pass_list.append(pywrapper_fsi2d.run_test())
######################################
### RUN EXTERNAL FSI COUPLING TEST ###
######################################
# Pitch-plunge NACA 0012 (external FSI coupling)
coupled_FSI = TestCase('coupled_FSI')
coupled_FSI.cfg_dir = "coupled_fsi/2d_aeroelasticity"
coupled_FSI.cfg_file = "FSICoupler_config.cfg"
coupled_FSI.test_iter = 1
coupled_FSI.su2_exec = "fsi_computation.py"
coupled_FSI.timeout = 1600
coupled_FSI.reference_file = "StructHistory.dat.ref_serial"
coupled_FSI.test_file = "StructHistory.dat"
pass_list.append(coupled_FSI.run_filediff())
test_list.append(coupled_FSI)
# Tests summary
print '=================================================================='
print 'Summary of the serial tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s' % test.tag
else:
print '* FAILED - %s' % test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase('channel')
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-2.984481, 2.389875, 0.008865, 0.027854] #last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase('naca0012')
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] #last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase('wedge')
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.702502, 3.923373, -0.252116, 0.044396] #last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase('oneram6')
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.398374, -12.928436, 0.282557, 0.012706] #last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase('flatplate')
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.233923, 0.259801, -0.166790, 0.012722] #last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase('cylinder')
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948, 0.625438] #last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase('rae2822_sa')
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.637762, -5.450251, 0.890401, 0.025056] #last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase('rae2822_sst')
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.217020, 4.023774, 0.892665, 0.025209] #last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase('turb_flatplate')
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.073540, -7.354716, -0.187154, 0.011105] #last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase('turb_oneram6')
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438, 0.155815] #last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase('turb_naca0012_sa')
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000764, -9.145363, 1.070528, 0.019417] #last 4 columns
turb_naca0012_sa.su2_exec = "parallel_computation.py -f"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase('turb_naca0012_sst')
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039665, -7.220109, 1.059622, 0.019138] #last 4 columns
turb_naca0012_sst.su2_exec = "parallel_computation.py -f"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase('inc_turb_naca0012')
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.709508, -11.006161, -0.000017, 0.211696] #last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase('contadj_naca0012')
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.783712, -15.192812, 0.300920, 0.536870] #last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase('contadj_oneram6')
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.132862, -12.704820, 0.685900, 0.140920] #last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase('contadj_ns_cylinder')
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.658396, -9.117436, -2.056700, 4.497000] #last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase('contadj_ns_naca0012_sub')
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.229160] #last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase('contadj_ns_naca0012_trans')
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.620880] #last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase('contadj_rans_naca0012')
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, -19.169000, -2.994100] #last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase('contadj_rans_rae822')
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.381632, -10.887032, -0.212470, 0.269390] #last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase('contadj_incomp_NACA0012')
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.968536, -12.133235, 1.939900, 0.000000] #last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase('contadj_incomp_cylinder')
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718776, -7.020714, -2.932100, 0.000000] #last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Thermochemical Nonequilibrium ###
######################################
# RAM-C II Sphere-Cone -- 61km Altitude
ramc = TestCase('ramc')
ramc.cfg_dir = "tne2/ramc"
ramc.cfg_file = "ramc61km.cfg"
ramc.test_iter = 25
ramc.test_vals = [-4.643029, 2.849441, -4.443852, 0.000313] #last 4 columns
ramc.su2_exec = "parallel_computation.py -f"
ramc.timeout = 1600
ramc.tol = 0.00001
test_list.append(ramc)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase('cavity')
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.594283, -0.130745, -0.510607, 0.061921] #last 4 columns
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase('spinning_cylinder')
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.637313, -2.194229, 1.212769, 1.605369] #last 4 columns
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase('square_cylinder')
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.544602, 0.048576, 1.398951, 2.196894] #last 4 columns
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase('sine_gust')
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.014552, -0.004969] #last 4 columns
sine_gust.su2_exec = "parallel_computation.py -f"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase('aeroelastic')
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077319, 0.036428, -1.685289e-03, -1.129111e-04] #last 4 columns
aeroelastic.su2_exec = "parallel_computation.py -f"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase('edge_VW')
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-1.446201, 4.751213, -0.000046, 0.000000] #last 4 columns
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase('edge_PPR')
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-1.995058, 4.175675, -0.000056, 0.000000] #last 4 columns
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
# Tests summary
print '=================================================================='
print 'Summary of the parallel tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s'%test.tag
else:
print '* FAILED - %s'%test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606839, -9.035212, -0.000000, 0.005688] #last 4 columns
discadj_naca0012.su2_exec = "SU2_CFD_AD"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.724711, -4.052467, -0.000000, 0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "SU2_CFD_AD"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
#######################################################
### Disc. adj. compressible RANS ###
#######################################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-1.751962, 0.485775, 0.182122, -0.000018] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-1.654903, -0.491416, 0.109157, 0.000011] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [-3.391214, -2.560170, 0.000000, 0.000000] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "SU2_CFD_AD"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder_disc.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [-2.802148, -2.228080, 0.000000, 0.000000] #last 4 columns
discadj_incomp_cylinder.su2_exec = "SU2_CFD_AD"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012
discadj_incomp_turb_NACA0012 = TestCase('discadj_incomp_turb_NACA0012')
discadj_incomp_turb_NACA0012.cfg_dir = "incomp_rans/naca0012"
discadj_incomp_turb_NACA0012.cfg_file = "naca0012_disc.cfg"
discadj_incomp_turb_NACA0012.test_iter = 10
discadj_incomp_turb_NACA0012.test_vals = [-3.847506, -1.009607, 0.000000, 0.000000] #last 4 columns
discadj_incomp_turb_NACA0012.su2_exec = "SU2_CFD_AD"
discadj_incomp_turb_NACA0012.timeout = 1600
discadj_incomp_turb_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746904, -1.544886, -0.008345, 0.000014] #last 4 columns
discadj_cylinder.su2_exec = "SU2_CFD_AD"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
###################################
### Structural Adjoint ###
###################################
# Structural model
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 9
discadj_fea.test_vals = [-6.403771, -6.404196, -3.6413e-04, -8.7087e+00] #last 4 columns
discadj_fea.su2_exec = "SU2_CFD_AD"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Coupled FSI Adjoint ###
###################################
# Structural model
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "configAD_fsi.cfg"
discadj_fsi.test_iter = 3000
discadj_fsi.test_vals = [0.958848,-0.157183,0.658415,1.302076] #last 4 columns
discadj_fsi.su2_exec = "SU2_CFD_AD"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
######################################
### RUN PYTHON TESTS ###
######################################
# test discrete_adjoint.py
discadj_euler_py = TestCase('discadj_euler_py')
discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
discadj_euler_py.cfg_file = "inv_NACA0012.cfg"
discadj_euler_py.test_iter = 10
discadj_euler_py.su2_exec = "discrete_adjoint.py"
discadj_euler_py.timeout = 1600
discadj_euler_py.reference_file = "of_grad_cd_disc.dat.ref"
discadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_euler_py.run_filediff())
test_list.append(discadj_euler_py)
# test direct_differentiation.py
directdiff_euler_py = TestCase('directdiff_euler_py')
directdiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
directdiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
directdiff_euler_py.test_iter = 10
directdiff_euler_py.su2_exec = "direct_differentiation.py"
directdiff_euler_py.timeout = 1600
directdiff_euler_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_euler_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_euler_py.run_filediff())
test_list.append(directdiff_euler_py)
# test continuous_adjoint.py, with multiple objectives
discadj_multi_py = TestCase('discadj_multi_py')
discadj_multi_py.cfg_dir = "cont_adj_euler/wedge"
discadj_multi_py.cfg_file = "inv_wedge_ROE_multiobj.cfg"
discadj_multi_py.test_iter = 10
discadj_multi_py.su2_exec = "discrete_adjoint.py"
discadj_multi_py.timeout = 1600
discadj_multi_py.reference_file = "of_grad_combo.dat.refdiscrete"
discadj_multi_py.test_file = "of_grad_combo.dat"
pass_list.append(discadj_multi_py.run_filediff())
test_list.append(discadj_multi_py)
# Tests summary
print('==================================================================')
print('Summary of the serial tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s'%test.tag)
else:
print('* FAILED - %s'%test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606839, -9.035212, -0.000000,
0.005688] #last 4 columns
discadj_naca0012.su2_exec = "SU2_CFD_AD"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.724711, -4.052467, -0.000000,
0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "SU2_CFD_AD"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
#######################################################
### Disc. adj. compressible RANS ###
#######################################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [
-1.751962, 0.485775, 0.182122, -0.000018
] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [
-1.654903, -0.491416, 0.109157, 0.000011
] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [
-2.911277, -2.705448, 0.000000, 0.000000
] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "SU2_CFD_AD"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder_disc.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [
-2.731029, -2.243767, 0.000000, 0.000000
] #last 4 columns
discadj_incomp_cylinder.su2_exec = "SU2_CFD_AD"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012
discadj_incomp_turb_NACA0012 = TestCase('discadj_incomp_turb_NACA0012')
discadj_incomp_turb_NACA0012.cfg_dir = "incomp_rans/naca0012"
discadj_incomp_turb_NACA0012.cfg_file = "naca0012_disc.cfg"
discadj_incomp_turb_NACA0012.test_iter = 100
discadj_incomp_turb_NACA0012.test_vals = [
-3.645349, -1.625510, 0.000000, 0.000000
] #last 4 columns
discadj_incomp_turb_NACA0012.su2_exec = "SU2_CFD_AD"
discadj_incomp_turb_NACA0012.timeout = 1600
discadj_incomp_turb_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746904, -1.544886, -0.008345,
0.000014] #last 4 columns
discadj_cylinder.su2_exec = "SU2_CFD_AD"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
###################################
### Structural Adjoint ###
###################################
# Structural model
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 9
discadj_fea.test_vals = [-6.403771, -6.404196, -3.6413e-04,
-8.7087e+00] #last 4 columns
discadj_fea.su2_exec = "SU2_CFD_AD"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Coupled FSI Adjoint ###
###################################
# Structural model
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "configAD_fsi.cfg"
discadj_fsi.test_iter = 3000
discadj_fsi.test_vals = [0.958848, -0.157183, 0.658415,
1.302076] #last 4 columns
discadj_fsi.su2_exec = "SU2_CFD_AD"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
######################################
### RUN PYTHON TESTS ###
######################################
# test discrete_adjoint.py
discadj_euler_py = TestCase('discadj_euler_py')
discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
discadj_euler_py.cfg_file = "inv_NACA0012.cfg"
discadj_euler_py.test_iter = 10
discadj_euler_py.su2_exec = "discrete_adjoint.py"
discadj_euler_py.timeout = 1600
discadj_euler_py.reference_file = "of_grad_cd_disc.dat.ref"
discadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_euler_py.run_filediff())
test_list.append(discadj_euler_py)
# test direct_differentiation.py
directdiff_euler_py = TestCase('directdiff_euler_py')
directdiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
directdiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
directdiff_euler_py.test_iter = 10
directdiff_euler_py.su2_exec = "direct_differentiation.py"
directdiff_euler_py.timeout = 1600
directdiff_euler_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_euler_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_euler_py.run_filediff())
test_list.append(directdiff_euler_py)
# test continuous_adjoint.py, with multiple objectives
discadj_multi_py = TestCase('discadj_multi_py')
discadj_multi_py.cfg_dir = "cont_adj_euler/wedge"
discadj_multi_py.cfg_file = "inv_wedge_ROE_multiobj.cfg"
discadj_multi_py.test_iter = 10
discadj_multi_py.su2_exec = "discrete_adjoint.py"
discadj_multi_py.timeout = 1600
discadj_multi_py.reference_file = "of_grad_combo.dat.refdiscrete"
discadj_multi_py.test_file = "of_grad_combo.dat"
pass_list.append(discadj_multi_py.run_filediff())
test_list.append(discadj_multi_py)
# Tests summary
print('==================================================================')
print('Summary of the serial tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s' % test.tag)
else:
print('* FAILED - %s' % test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
"""This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. """
test_list = []
##########################
### Compressible Euler ###
##########################
# Channel
channel = TestCase("channel")
channel.cfg_dir = "euler/channel"
channel.cfg_file = "inv_channel_RK.cfg"
channel.test_iter = 100
channel.test_vals = [-3.071007, 2.301191, 0.008562, 0.028922] # last 4 columns
channel.su2_exec = "parallel_computation.py -f"
channel.timeout = 1600
channel.tol = 0.00001
test_list.append(channel)
# NACA0012
naca0012 = TestCase("naca0012")
naca0012.cfg_dir = "euler/naca0012"
naca0012.cfg_file = "inv_NACA0012_Roe.cfg"
naca0012.test_iter = 100
naca0012.test_vals = [-6.237188, -5.641250, 0.334843, 0.022206] # last 4 columns
naca0012.su2_exec = "parallel_computation.py -f"
naca0012.timeout = 1600
naca0012.tol = 0.00001
test_list.append(naca0012)
# Supersonic wedge
wedge = TestCase("wedge")
wedge.cfg_dir = "euler/wedge"
wedge.cfg_file = "inv_wedge_HLLC.cfg"
wedge.test_iter = 100
wedge.test_vals = [-1.690232, 3.924432, -0.252221, 0.044419] # last 4 columns
wedge.su2_exec = "parallel_computation.py -f"
wedge.timeout = 1600
wedge.tol = 0.00001
test_list.append(wedge)
# ONERA M6 Wing
oneram6 = TestCase("oneram6")
oneram6.cfg_dir = "euler/oneram6"
oneram6.cfg_file = "inv_ONERAM6.cfg"
oneram6.test_iter = 10
oneram6.test_vals = [-13.400678, -12.932056, 0.282557, 0.012706] # last 4 columns
oneram6.su2_exec = "parallel_computation.py -f"
oneram6.timeout = 3200
oneram6.tol = 0.00001
test_list.append(oneram6)
##########################
### Compressible N-S ###
##########################
# Laminar flat plate
flatplate = TestCase("flatplate")
flatplate.cfg_dir = "navierstokes/flatplate"
flatplate.cfg_file = "lam_flatplate.cfg"
flatplate.test_iter = 100
flatplate.test_vals = [-5.231727, 0.261637, -0.166869, 0.012707] # last 4 columns
flatplate.su2_exec = "parallel_computation.py -f"
flatplate.timeout = 1600
flatplate.tol = 0.00001
test_list.append(flatplate)
# Laminar cylinder (steady)
cylinder = TestCase("cylinder")
cylinder.cfg_dir = "navierstokes/cylinder"
cylinder.cfg_file = "lam_cylinder.cfg"
cylinder.test_iter = 25
cylinder.test_vals = [-6.757291, -1.289309, -0.125948, 0.625438] # last 4 columns
cylinder.su2_exec = "parallel_computation.py -f"
cylinder.timeout = 1600
cylinder.tol = 0.00001
test_list.append(cylinder)
# Laminar cylinder (low Mach correction)
cylinder_lowmach = TestCase("cylinder_lowmach")
cylinder_lowmach.cfg_dir = "navierstokes/cylinder"
cylinder_lowmach.cfg_file = "cylinder_lowmach.cfg"
cylinder_lowmach.test_iter = 25
cylinder_lowmach.test_vals = [-6.861860, -1.399846, -1.557250, 110.230719] # last 4 columns
cylinder_lowmach.su2_exec = "parallel_computation.py -f"
cylinder_lowmach.timeout = 1600
cylinder_lowmach.tol = 0.00001
test_list.append(cylinder_lowmach)
##########################
### Compressible RANS ###
##########################
# RAE2822 SA
rae2822_sa = TestCase("rae2822_sa")
rae2822_sa.cfg_dir = "rans/rae2822"
rae2822_sa.cfg_file = "turb_SA_RAE2822.cfg"
rae2822_sa.test_iter = 100
rae2822_sa.test_vals = [-3.647743, -5.442583, 0.903159, 0.025800] # last 4 columns
rae2822_sa.su2_exec = "parallel_computation.py -f"
rae2822_sa.timeout = 1600
rae2822_sa.tol = 0.00001
test_list.append(rae2822_sa)
# RAE2822 SST
rae2822_sst = TestCase("rae2822_sst")
rae2822_sst.cfg_dir = "rans/rae2822"
rae2822_sst.cfg_file = "turb_SST_RAE2822.cfg"
rae2822_sst.test_iter = 100
rae2822_sst.test_vals = [-1.198777, 4.013989, 0.904265, 0.025941] # last 4 columns
rae2822_sst.su2_exec = "parallel_computation.py -f"
rae2822_sst.timeout = 1600
rae2822_sst.tol = 0.00001
test_list.append(rae2822_sst)
# Flat plate
turb_flatplate = TestCase("turb_flatplate")
turb_flatplate.cfg_dir = "rans/flatplate"
turb_flatplate.cfg_file = "turb_SA_flatplate.cfg"
turb_flatplate.test_iter = 100
turb_flatplate.test_vals = [-5.071289, -7.366446, -0.187145, 0.010957] # last 4 columns
turb_flatplate.su2_exec = "parallel_computation.py -f"
turb_flatplate.timeout = 1600
turb_flatplate.tol = 0.00001
test_list.append(turb_flatplate)
# ONERA M6 Wing
turb_oneram6 = TestCase("turb_oneram6")
turb_oneram6.cfg_dir = "rans/oneram6"
turb_oneram6.cfg_file = "turb_ONERAM6.cfg"
turb_oneram6.test_iter = 10
turb_oneram6.test_vals = [-2.327509, -6.563372, 0.230438, 0.155815] # last 4 columns
turb_oneram6.su2_exec = "parallel_computation.py -f"
turb_oneram6.timeout = 3200
turb_oneram6.tol = 0.00001
test_list.append(turb_oneram6)
# NACA0012 (SA, FUN3D finest grid results: CL=1.0983, CD=0.01242)
turb_naca0012_sa = TestCase("turb_naca0012_sa")
turb_naca0012_sa.cfg_dir = "rans/naca0012"
turb_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
turb_naca0012_sa.test_iter = 10
turb_naca0012_sa.test_vals = [-12.000764, -9.145363, 1.070528, 0.019417] # last 4 columns
turb_naca0012_sa.su2_exec = "parallel_computation.py -f"
turb_naca0012_sa.timeout = 3200
turb_naca0012_sa.tol = 0.00001
test_list.append(turb_naca0012_sa)
# NACA0012 (SST, FUN3D finest grid results: CL=1.0840, CD=0.01253)
turb_naca0012_sst = TestCase("turb_naca0012_sst")
turb_naca0012_sst.cfg_dir = "rans/naca0012"
turb_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
turb_naca0012_sst.test_iter = 10
turb_naca0012_sst.test_vals = [-15.039645, -7.220177, 1.059622, 0.019138] # last 4 columns
turb_naca0012_sst.su2_exec = "parallel_computation.py -f"
turb_naca0012_sst.timeout = 3200
turb_naca0012_sst.tol = 0.00001
test_list.append(turb_naca0012_sst)
############################
### Incompressible RANS ###
############################
# NACA0012
inc_turb_naca0012 = TestCase("inc_turb_naca0012")
inc_turb_naca0012.cfg_dir = "incomp_rans/naca0012"
inc_turb_naca0012.cfg_file = "naca0012.cfg"
inc_turb_naca0012.test_iter = 20
inc_turb_naca0012.test_vals = [-4.710048, -11.007498, 0.000002, 0.210441] # last 4 columns
inc_turb_naca0012.su2_exec = "parallel_computation.py -f"
inc_turb_naca0012.timeout = 1600
inc_turb_naca0012.tol = 0.00001
test_list.append(inc_turb_naca0012)
#####################################
### Cont. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
contadj_naca0012 = TestCase("contadj_naca0012")
contadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
contadj_naca0012.cfg_file = "inv_NACA0012.cfg"
contadj_naca0012.test_iter = 5
contadj_naca0012.test_vals = [-9.783712, -15.192812, 0.300920, 0.536870] # last 4 columns
contadj_naca0012.su2_exec = "parallel_computation.py -f"
contadj_naca0012.timeout = 1600
contadj_naca0012.tol = 0.00001
test_list.append(contadj_naca0012)
# Inviscid ONERA M6
contadj_oneram6 = TestCase("contadj_oneram6")
contadj_oneram6.cfg_dir = "cont_adj_euler/oneram6"
contadj_oneram6.cfg_file = "inv_ONERAM6.cfg"
contadj_oneram6.test_iter = 10
contadj_oneram6.test_vals = [-12.131587, -12.703243, 0.685900, 0.140920] # last 4 columns
contadj_oneram6.su2_exec = "parallel_computation.py -f"
contadj_oneram6.timeout = 1600
contadj_oneram6.tol = 0.00001
test_list.append(contadj_oneram6)
# Inviscid WEDGE: generalized adjoint and custom DV
contadj_wedge = TestCase("contadj_wedge")
contadj_wedge.cfg_dir = "cont_adj_euler/wedge"
contadj_wedge.cfg_file = "inv_wedge_ROE.cfg"
contadj_wedge.test_iter = 10
contadj_wedge.test_vals = [-7.364977, -13.301134, 0.000266, 0.000000] # last 4 columns
contadj_wedge.su2_exec = "parallel_computation.py -f"
contadj_wedge.timeout = 1600
contadj_wedge.tol = 0.00001
test_list.append(contadj_wedge)
###################################
### Cont. adj. compressible N-S ###
###################################
# Adjoint laminar cylinder
contadj_ns_cylinder = TestCase("contadj_ns_cylinder")
contadj_ns_cylinder.cfg_dir = "cont_adj_navierstokes/cylinder"
contadj_ns_cylinder.cfg_file = "lam_cylinder.cfg"
contadj_ns_cylinder.test_iter = 100
contadj_ns_cylinder.test_vals = [-3.659040, -9.117773, 2.056700, 4.497000] # last 4 columns
contadj_ns_cylinder.su2_exec = "parallel_computation.py -f"
contadj_ns_cylinder.timeout = 1600
contadj_ns_cylinder.tol = 0.00001
test_list.append(contadj_ns_cylinder)
# Adjoint laminar naca0012 subsonic
contadj_ns_naca0012_sub = TestCase("contadj_ns_naca0012_sub")
contadj_ns_naca0012_sub.cfg_dir = "cont_adj_navierstokes/naca0012_sub"
contadj_ns_naca0012_sub.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_sub.test_iter = 100
contadj_ns_naca0012_sub.test_vals = [-2.744551, -8.216469, 0.518810, 0.229160] # last 4 columns
contadj_ns_naca0012_sub.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_sub.timeout = 1600
contadj_ns_naca0012_sub.tol = 0.00001
test_list.append(contadj_ns_naca0012_sub)
# Adjoint laminar naca0012 transonic
contadj_ns_naca0012_trans = TestCase("contadj_ns_naca0012_trans")
contadj_ns_naca0012_trans.cfg_dir = "cont_adj_navierstokes/naca0012_trans"
contadj_ns_naca0012_trans.cfg_file = "lam_NACA0012.cfg"
contadj_ns_naca0012_trans.test_iter = 100
contadj_ns_naca0012_trans.test_vals = [-1.041539, -6.578524, 1.772300, 0.620880] # last 4 columns
contadj_ns_naca0012_trans.su2_exec = "parallel_computation.py -f"
contadj_ns_naca0012_trans.timeout = 1600
contadj_ns_naca0012_trans.tol = 0.00001
test_list.append(contadj_ns_naca0012_trans)
#######################################################
### Cont. adj. compressible RANS (frozen viscosity) ###
#######################################################
# Adjoint turbulent NACA0012
contadj_rans_naca0012 = TestCase("contadj_rans_naca0012")
contadj_rans_naca0012.cfg_dir = "cont_adj_rans/naca0012"
contadj_rans_naca0012.cfg_file = "turb_nasa.cfg"
contadj_rans_naca0012.test_iter = 100
contadj_rans_naca0012.test_vals = [-0.814757, -5.726517, 19.169000, -2.994100] # last 4 columns
contadj_rans_naca0012.su2_exec = "parallel_computation.py -f"
contadj_rans_naca0012.timeout = 1600
contadj_rans_naca0012.tol = 0.00001
test_list.append(contadj_rans_naca0012)
# Adjoint turbulent RAE2822
contadj_rans_rae2822 = TestCase("contadj_rans_rae822")
contadj_rans_rae2822.cfg_dir = "cont_adj_rans/rae2822"
contadj_rans_rae2822.cfg_file = "turb_SA_RAE2822.cfg"
contadj_rans_rae2822.test_iter = 100
contadj_rans_rae2822.test_vals = [-5.380929, -10.886092, -0.212470, 0.269390] # last 4 columns
contadj_rans_rae2822.su2_exec = "parallel_computation.py -f"
contadj_rans_rae2822.timeout = 1600
contadj_rans_rae2822.tol = 0.00001
test_list.append(contadj_rans_rae2822)
#######################################
### Cont. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
contadj_incomp_NACA0012 = TestCase("contadj_incomp_NACA0012")
contadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
contadj_incomp_NACA0012.cfg_file = "incomp_NACA0012.cfg"
contadj_incomp_NACA0012.test_iter = 5
contadj_incomp_NACA0012.test_vals = [-11.968536, -12.133235, 1.939900, 0.000000] # last 4 columns
contadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
contadj_incomp_NACA0012.timeout = 1600
contadj_incomp_NACA0012.tol = 0.00001
test_list.append(contadj_incomp_NACA0012)
#####################################
### Cont. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
contadj_incomp_cylinder = TestCase("contadj_incomp_cylinder")
contadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
contadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder.cfg"
contadj_incomp_cylinder.test_iter = 25
contadj_incomp_cylinder.test_vals = [-5.718840, -7.012324, 2.932100, 0.000000] # last 4 columns
contadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
contadj_incomp_cylinder.timeout = 1600
contadj_incomp_cylinder.tol = 0.00001
test_list.append(contadj_incomp_cylinder)
######################################
### Moving Wall ###
######################################
# Lid-driven cavity
cavity = TestCase("cavity")
cavity.cfg_dir = "moving_wall/cavity"
cavity.cfg_file = "lam_cavity.cfg"
cavity.test_iter = 25
cavity.test_vals = [-5.597018, -0.133158, 0.169034, 0.821371] # last 4 columns
cavity.su2_exec = "parallel_computation.py -f"
cavity.timeout = 1600
cavity.tol = 0.00001
test_list.append(cavity)
# Spinning cylinder
spinning_cylinder = TestCase("spinning_cylinder")
spinning_cylinder.cfg_dir = "moving_wall/spinning_cylinder"
spinning_cylinder.cfg_file = "spinning_cylinder.cfg"
spinning_cylinder.test_iter = 25
spinning_cylinder.test_vals = [-7.648320, -2.202753, 1.236836, 1.609040] # last 4 columns
spinning_cylinder.su2_exec = "parallel_computation.py -f"
spinning_cylinder.timeout = 1600
spinning_cylinder.tol = 0.00001
test_list.append(spinning_cylinder)
######################################
### Unsteady ###
######################################
# Square cylinder
square_cylinder = TestCase("square_cylinder")
square_cylinder.cfg_dir = "unsteady/square_cylinder"
square_cylinder.cfg_file = "turb_square.cfg"
square_cylinder.test_iter = 3
square_cylinder.test_vals = [-1.166422, 0.076751, 1.398549, 2.197047] # last 4 columns
square_cylinder.su2_exec = "parallel_computation.py -f"
square_cylinder.timeout = 1600
square_cylinder.tol = 0.00001
square_cylinder.unsteady = True
test_list.append(square_cylinder)
# Gust
sine_gust = TestCase("sine_gust")
sine_gust.cfg_dir = "gust"
sine_gust.cfg_file = "inv_gust_NACA0012.cfg"
sine_gust.test_iter = 5
sine_gust.test_vals = [-1.977531, 3.481790, -0.014552, -0.004969] # last 4 columns
sine_gust.su2_exec = "parallel_computation.py -f"
sine_gust.timeout = 1600
sine_gust.tol = 0.00001
sine_gust.unsteady = True
test_list.append(sine_gust)
# Aeroelastic
aeroelastic = TestCase("aeroelastic")
aeroelastic.cfg_dir = "aeroelastic"
aeroelastic.cfg_file = "aeroelastic_NACA64A010.cfg"
aeroelastic.test_iter = 2
aeroelastic.test_vals = [0.077169, 0.036452, -0.001685, -0.000113] # last 4 columns
aeroelastic.su2_exec = "parallel_computation.py -f"
aeroelastic.timeout = 1600
aeroelastic.tol = 0.000001
aeroelastic.unsteady = True
test_list.append(aeroelastic)
######################################
### NICFD ###
######################################
# Rarefaction shock wave edge_VW
edge_VW = TestCase("edge_VW")
edge_VW.cfg_dir = "nicf/edge"
edge_VW.cfg_file = "edge_VW.cfg"
edge_VW.test_iter = 100
edge_VW.test_vals = [-5.058481, 1.115321, -0.000009, 0.000000] # last 4 columns
edge_VW.su2_exec = "parallel_computation.py -f"
edge_VW.timeout = 1600
edge_VW.tol = 0.00001
test_list.append(edge_VW)
# Rarefaction shock wave edge_PPR
edge_PPR = TestCase("edge_PPR")
edge_PPR.cfg_dir = "nicf/edge"
edge_PPR.cfg_file = "edge_PPR.cfg"
edge_PPR.test_iter = 100
edge_PPR.test_vals = [-5.486409, 0.654417, -0.000037, 0.000000] # last 4 columns
edge_PPR.su2_exec = "parallel_computation.py -f"
edge_PPR.timeout = 1600
edge_PPR.tol = 0.00001
test_list.append(edge_PPR)
##########################
### FEA - FSI ###
##########################
# Static beam, 3d
statbeam3d = TestCase("statbeam3d")
statbeam3d.cfg_dir = "fea_fsi/StatBeam_3d"
statbeam3d.cfg_file = "configBeam_3d.cfg"
statbeam3d.test_iter = 0
statbeam3d.test_vals = [-8.520066, -8.069308, -8.062384, 64095.000000] # last 4 columns
statbeam3d.su2_exec = "parallel_computation_fsi.py -f"
statbeam3d.timeout = 1600
statbeam3d.tol = 0.00001
test_list.append(statbeam3d)
# Dynamic beam, 2d
dynbeam2d = TestCase("dynbeam2d")
dynbeam2d.cfg_dir = "fea_fsi/DynBeam_2d"
dynbeam2d.cfg_file = "configBeam_2d.cfg"
dynbeam2d.test_iter = 6
dynbeam2d.test_vals = [-9.420641, -5.365871, -12.430382, 6.5210e04] # last 4 columns
dynbeam2d.su2_exec = "parallel_computation_fsi.py -f"
dynbeam2d.timeout = 1600
dynbeam2d.tol = 0.00001
test_list.append(dynbeam2d)
# FSI, 2d
fsi2d = TestCase("fsi2d")
fsi2d.cfg_dir = "fea_fsi/WallChannel_2d"
fsi2d.cfg_file = "configFSI_2D.cfg"
fsi2d.test_iter = 4
fsi2d.test_vals = [2.000000, 0.500000, -7.777910, -1.139830] # last 4 columns
fsi2d.su2_exec = "parallel_computation_fsi.py -f"
fsi2d.timeout = 1600
fsi2d.tol = 0.00001
test_list.append(fsi2d)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
######################################
### RUN SU2_DEF TESTS ###
######################################
# Inviscid NACA0012 (triangles)
naca0012_def = TestCase("naca0012_def")
naca0012_def.cfg_dir = "deformation/naca0012"
naca0012_def.cfg_file = "def_NACA0012.cfg"
naca0012_def.test_iter = 250
naca0012_def.test_vals = [5.44754e-15] # residual
naca0012_def.su2_exec = "mpirun -n 2 SU2_DEF"
naca0012_def.timeout = 1600
naca0012_def.tol = 1e-15
pass_list.append(naca0012_def.run_def())
test_list.append(naca0012_def)
# RAE2822 (mixed tris + quads)
rae2822_def = TestCase("rae2822_def")
rae2822_def.cfg_dir = "deformation/rae2822"
rae2822_def.cfg_file = "def_RAE2822.cfg"
rae2822_def.test_iter = 150
rae2822_def.test_vals = [1.47076e-15] # residual
rae2822_def.su2_exec = "mpirun -n 2 SU2_DEF"
rae2822_def.timeout = 1600
rae2822_def.tol = 1e-16
pass_list.append(rae2822_def.run_def())
test_list.append(rae2822_def)
# Turb NACA4412 (quads, wall distance)
naca4412_def = TestCase("naca4412_def")
naca4412_def.cfg_dir = "deformation/naca4412"
naca4412_def.cfg_file = "def_NACA4412.cfg"
naca4412_def.test_iter = 300
naca4412_def.test_vals = [4.46129e-15] # residual
naca4412_def.su2_exec = "mpirun -n 2 SU2_DEF"
naca4412_def.timeout = 1600
naca4412_def.tol = 1e-15
pass_list.append(naca4412_def.run_def())
test_list.append(naca4412_def)
# Brick of tets (inverse volume)
brick_tets_def = TestCase("brick_tets_def")
brick_tets_def.cfg_dir = "deformation/brick_tets"
brick_tets_def.cfg_file = "def_brick_tets.cfg"
brick_tets_def.test_iter = 1000
brick_tets_def.test_vals = [9.35558e-16] # residual
brick_tets_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_tets_def.timeout = 1600
brick_tets_def.tol = 1e-15
pass_list.append(brick_tets_def.run_def())
test_list.append(brick_tets_def)
# Brick of isotropic hexas (inverse volume)
brick_hex_def = TestCase("brick_hex_def")
brick_hex_def.cfg_dir = "deformation/brick_hex"
brick_hex_def.cfg_file = "def_brick_hex.cfg"
brick_hex_def.test_iter = 1000
brick_hex_def.test_vals = [1.46423e-15] # residual
brick_hex_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_hex_def.timeout = 1600
brick_hex_def.tol = 1e-15
pass_list.append(brick_hex_def.run_def())
test_list.append(brick_hex_def)
# Brick with a pyramid layer (inverse volume)
brick_pyra_def = TestCase("brick_pyra_def")
brick_pyra_def.cfg_dir = "deformation/brick_pyra"
brick_pyra_def.cfg_file = "def_brick_pyra.cfg"
brick_pyra_def.test_iter = 100
brick_pyra_def.test_vals = [5.97202e-15] # residual
brick_pyra_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_pyra_def.timeout = 1600
brick_pyra_def.tol = 1e-15
pass_list.append(brick_pyra_def.run_def())
test_list.append(brick_pyra_def)
# Brick of isotropic prisms (inverse volume)
brick_prism_def = TestCase("brick_prism_def")
brick_prism_def.cfg_dir = "deformation/brick_prism"
brick_prism_def.cfg_file = "def_brick_prism.cfg"
brick_prism_def.test_iter = 100
brick_prism_def.test_vals = [2.80867e-14] # residual
brick_prism_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_prism_def.timeout = 1600
brick_prism_def.tol = 1e-15
pass_list.append(brick_prism_def.run_def())
test_list.append(brick_prism_def)
# Brick of prisms with high aspect ratio cells near the wall (wall distance)
brick_prism_rans_def = TestCase("brick_prism_rans_def")
brick_prism_rans_def.cfg_dir = "deformation/brick_prism_rans"
brick_prism_rans_def.cfg_file = "def_brick_prism_rans.cfg"
brick_prism_rans_def.test_iter = 50
brick_prism_rans_def.test_vals = [3.5265e-15] # residual
brick_prism_rans_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_prism_rans_def.timeout = 1600
brick_prism_rans_def.tol = 1e-15
pass_list.append(brick_prism_rans_def.run_def())
test_list.append(brick_prism_rans_def)
# Brick of hexas with high aspect ratio cells near the wall (inverse volume)
brick_hex_rans_def = TestCase("brick_hex_rans_def")
brick_hex_rans_def.cfg_dir = "deformation/brick_hex_rans"
brick_hex_rans_def.cfg_file = "def_brick_hex_rans.cfg"
brick_hex_rans_def.test_iter = 600
brick_hex_rans_def.test_vals = [2.75292e-14] # residual
brick_hex_rans_def.su2_exec = "mpirun -n 2 SU2_DEF"
brick_hex_rans_def.timeout = 1600
brick_hex_rans_def.tol = 1e-16
pass_list.append(brick_hex_rans_def.run_def())
test_list.append(brick_hex_rans_def)
# Tests summary
print "=================================================================="
print "Summary of the parallel tests"
for i, test in enumerate(test_list):
if pass_list[i]:
print " passed - %s" % test.tag
else:
print "* FAILED - %s" % test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.561506, -8.926634, -0.000000, 0.005587]
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.730673, -3.832084, -0.000000, 0.000000]
test_list.append(discadj_cylinder3D)
# Arina nozzle 2D
discadj_arina2k = TestCase('discadj_arina2k')
discadj_arina2k.cfg_dir = "disc_adj_euler/arina2k"
discadj_arina2k.cfg_file = "Arina2KRS.cfg"
discadj_arina2k.test_iter = 20
discadj_arina2k.test_vals = [-3.087876, -3.481506, 0.068878, 0.000000]
test_list.append(discadj_arina2k)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [
-2.230632, 0.696530, 0.177890, -0.000016, 5, -3.007652, 5, -7.666352
]
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [
-2.221793, -0.491367, 0.182000, -0.000018
]
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "disc_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [
20.000000, -4.092007, -2.652751, 0.000000
]
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder (Heated)
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "disc_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "heated_cylinder.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [
20.000000, -2.705921, -2.837904, 0.000000
]
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012 SA
discadj_incomp_turb_NACA0012_sa = TestCase(
'discadj_incomp_turb_NACA0012_sa')
discadj_incomp_turb_NACA0012_sa.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sa.cfg_file = "turb_naca0012_sa.cfg"
discadj_incomp_turb_NACA0012_sa.test_iter = 10
discadj_incomp_turb_NACA0012_sa.test_vals = [
10.000000, -3.845995, -1.031097, 0.000000
]
test_list.append(discadj_incomp_turb_NACA0012_sa)
# Adjoint Incompressible Turbulent NACA 0012 SST
discadj_incomp_turb_NACA0012_sst = TestCase(
'discadj_incomp_turb_NACA0012_sst')
discadj_incomp_turb_NACA0012_sst.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sst.cfg_file = "turb_naca0012_sst.cfg"
discadj_incomp_turb_NACA0012_sst.test_iter = 10
discadj_incomp_turb_NACA0012_sst.test_vals = [
-3.845593, -2.414026, -8.420194, 0.000000
]
test_list.append(discadj_incomp_turb_NACA0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746907, -1.544882, -0.008321, 0.000014]
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##############################################################
### Unsteady Disc. adj. compressible RANS Windowed Average ###
##############################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder_windowed_average_AD')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder_Windowing_AD.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.004402]
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##########################################################################
### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order ###
##########################################################################
# Turbulent Cylinder
discadj_DT_1ST_cylinder = TestCase('unsteady_cylinder_DT_1ST')
discadj_DT_1ST_cylinder.cfg_dir = "disc_adj_rans/cylinder_DT_1ST"
discadj_DT_1ST_cylinder.cfg_file = "cylinder.cfg"
discadj_DT_1ST_cylinder.test_iter = 9
discadj_DT_1ST_cylinder.test_vals = [
3.698167, -1.607051, -0.002159, 0.000028
]
discadj_DT_1ST_cylinder.unsteady = True
test_list.append(discadj_DT_1ST_cylinder)
######################################################
### Unsteady Disc. adj. compressible pitching NACA ###
######################################################
# compressible pitching NACA0012
discadj_pitchingNACA0012 = TestCase('pitchingNACA0012')
discadj_pitchingNACA0012.cfg_dir = "disc_adj_euler/naca0012_pitching"
discadj_pitchingNACA0012.cfg_file = "inv_NACA0012_pitching.cfg"
discadj_pitchingNACA0012.test_iter = 4
discadj_pitchingNACA0012.test_vals = [
-1.219713, -1.645717, -0.007513, 0.000013
]
discadj_pitchingNACA0012.unsteady = True
test_list.append(discadj_pitchingNACA0012)
#######################################################
### Disc. adj. turbomachinery ###
#######################################################
# Transonic Stator 2D
discadj_trans_stator = TestCase('transonic_stator')
discadj_trans_stator.cfg_dir = "disc_adj_turbomachinery/transonic_stator_2D"
discadj_trans_stator.cfg_file = "transonic_stator.cfg"
discadj_trans_stator.test_iter = 79
discadj_trans_stator.test_vals = [79.000000, -1.938806, -1.995540]
test_list.append(discadj_trans_stator)
###################################
### Structural Adjoint ###
###################################
# Structural model
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 4
discadj_fea.test_vals = [1.774569, 1.928023, -0.000364, -8.690300]
test_list.append(discadj_fea)
######################################
### RUN TESTS ###
######################################
for test in test_list:
test.su2_exec = "SU2_CFD_AD -t 2"
test.timeout = 600
test.tol = 1e-4
#end
pass_list = [test.run_test() for test in test_list]
# Tests summary
print('==================================================================')
print('Summary of the hybrid parallel AD tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s' % test.tag)
else:
print('* FAILED - %s' % test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [
-3.606963, -9.034619, -3.3385e-07, 1.8777e-01
] #last 4 columns
discadj_naca0012.su2_exec = "parallel_computation.py -f"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [
-1.751829, 0.485848, 0.182890, -0.383520
] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [
-1.653638, -0.502899, 1.3126e-01, -4.7494e-01
] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
# Tests summary
print '=================================================================='
print 'Summary of the parallel tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s' % test.tag
else:
print '* FAILED - %s' % test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.559002, -8.926022, -0.000000,
0.005588] #last 4 columns
discadj_naca0012.su2_exec = "SU2_CFD_AD"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.759637, -3.864023, -0.000000,
0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "SU2_CFD_AD"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
# Arina nozzle 2D
discadj_arina2k = TestCase('discadj_arina2k')
discadj_arina2k.cfg_dir = "disc_adj_euler/arina2k"
discadj_arina2k.cfg_file = "Arina2KRS.cfg"
discadj_arina2k.test_iter = 20
discadj_arina2k.test_vals = [2.108283, 1.574295, 47250.0,
0.0] #last 4 columns
discadj_arina2k.su2_exec = "SU2_CFD_AD"
discadj_arina2k.timeout = 8400
discadj_arina2k.tol = 0.00001
test_list.append(discadj_arina2k)
#######################################################
### Disc. adj. compressible RANS ###
#######################################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [
-2.230556, 0.696586, 0.180740, -0.000018
] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [
-2.221232, -0.492215, 0.557480, 0.000027
] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "SU2_CFD_AD"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "disc_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [20.0, -4.092007, -2.652750,
0.0] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "SU2_CFD_AD"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder (Heated)
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "disc_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "heated_cylinder.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [
20.000000, -2.374306, -2.371564, 0.000000
] #last 4 columns
discadj_incomp_cylinder.su2_exec = "SU2_CFD_AD"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012 SA
discadj_incomp_turb_NACA0012_sa = TestCase(
'discadj_incomp_turb_NACA0012_sa')
discadj_incomp_turb_NACA0012_sa.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sa.cfg_file = "turb_naca0012_sa.cfg"
discadj_incomp_turb_NACA0012_sa.test_iter = 10
discadj_incomp_turb_NACA0012_sa.test_vals = [
10.000000, -3.845979, -1.031095, 0.000000
] #last 4 columns
discadj_incomp_turb_NACA0012_sa.su2_exec = "SU2_CFD_AD"
discadj_incomp_turb_NACA0012_sa.timeout = 1600
discadj_incomp_turb_NACA0012_sa.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sa)
# Adjoint Incompressible Turbulent NACA 0012 SST
discadj_incomp_turb_NACA0012_sst = TestCase(
'discadj_incomp_turb_NACA0012_sst')
discadj_incomp_turb_NACA0012_sst.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sst.cfg_file = "turb_naca0012_sst.cfg"
discadj_incomp_turb_NACA0012_sst.test_iter = 10
discadj_incomp_turb_NACA0012_sst.test_vals = [
-3.845577, -2.414021, -8.420183, 0.000000
] #last 4 columns
discadj_incomp_turb_NACA0012_sst.su2_exec = "SU2_CFD_AD"
discadj_incomp_turb_NACA0012_sst.timeout = 1600
discadj_incomp_turb_NACA0012_sst.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746909, -1.544883, -0.008321,
0.000014] #last 4 columns
discadj_cylinder.su2_exec = "SU2_CFD_AD"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##########################################################################
### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order ###
##########################################################################
# Turbulent Cylinder
discadj_DT_1ST_cylinder = TestCase('unsteady_cylinder_DT_1ST')
discadj_DT_1ST_cylinder.cfg_dir = "disc_adj_rans/cylinder_DT_1ST"
discadj_DT_1ST_cylinder.cfg_file = "cylinder.cfg"
discadj_DT_1ST_cylinder.test_iter = 9
discadj_DT_1ST_cylinder.test_vals = [
3.698168, -1.607050, -0.002159, 0.000028
] #last 4 columns
discadj_DT_1ST_cylinder.su2_exec = "SU2_CFD_AD"
discadj_DT_1ST_cylinder.timeout = 1600
discadj_DT_1ST_cylinder.tol = 0.00001
discadj_DT_1ST_cylinder.unsteady = True
test_list.append(discadj_DT_1ST_cylinder)
######################################################
### Unsteady Disc. adj. compressible pitching NACA ###
######################################################
# compressible pitching NACA0012
discadj_pitchingNACA0012 = TestCase('pitchingNACA0012')
discadj_pitchingNACA0012.cfg_dir = "disc_adj_euler/naca0012_pitching"
discadj_pitchingNACA0012.cfg_file = "inv_NACA0012_pitching.cfg"
discadj_pitchingNACA0012.test_iter = 4
discadj_pitchingNACA0012.test_vals = [
-1.223509, -1.646090, -0.007671, 0.000013
] #last 4 columns
discadj_pitchingNACA0012.su2_exec = "SU2_CFD_AD"
discadj_pitchingNACA0012.timeout = 1600
discadj_pitchingNACA0012.tol = 0.00001
discadj_pitchingNACA0012.unsteady = True
test_list.append(discadj_pitchingNACA0012)
# deforming pitching NACA0012
unst_deforming_naca0012 = TestCase('unst_deforming_naca0012')
unst_deforming_naca0012.cfg_dir = "disc_adj_euler/naca0012_pitching_def"
unst_deforming_naca0012.cfg_file = "inv_NACA0012_pitching_deform_ad.cfg"
unst_deforming_naca0012.test_iter = 4
unst_deforming_naca0012.test_vals = [
-1.867980, -1.741743, 1090.200000, 0.000006
] #last 4 columns
unst_deforming_naca0012.su2_exec = "SU2_CFD_AD"
unst_deforming_naca0012.timeout = 1600
unst_deforming_naca0012.tol = 0.00001
unst_deforming_naca0012.unsteady = True
test_list.append(unst_deforming_naca0012)
###################################
### Structural Adjoint ###
###################################
# Structural model
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 4
discadj_fea.test_vals = [-2.849531, -3.238474, -3.6413e-04,
-8.7087] #last 4 columns
discadj_fea.su2_exec = "SU2_CFD_AD"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Disc. adj. heat ###
###################################
# Discrete adjoint for heated cylinder
discadj_heat = TestCase('discadj_heat')
discadj_heat.cfg_dir = "disc_adj_heat"
discadj_heat.cfg_file = "disc_adj_heat.cfg"
discadj_heat.test_iter = 10
discadj_heat.test_vals = [-2.271573, 0.671242, -3.172000,
-8.231600] #last 4 columns
discadj_heat.su2_exec = "SU2_CFD_AD"
discadj_heat.timeout = 1600
discadj_heat.tol = 0.00001
test_list.append(discadj_heat)
###################################
### Coupled RHT-CFD Adjoint ###
###################################
# Coupled discrete adjoint for radiative heat transfer in heated cylinder
discadj_rht = TestCase('discadj_rht')
discadj_rht.cfg_dir = "radiation/p1adjoint"
discadj_rht.cfg_file = "configp1adjoint.cfg"
discadj_rht.test_iter = 10
discadj_rht.su2_exec = "discrete_adjoint.py -f"
discadj_rht.timeout = 1600
discadj_rht.reference_file = "of_grad_cd.csv.ref"
discadj_rht.test_file = "of_grad_cd.csv"
test_list.append(discadj_rht)
###################################
### Coupled FSI Adjoint ###
###################################
# Structural model
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "config.cfg"
discadj_fsi.test_iter = 6
discadj_fsi.test_vals = [6, -1.572702, -3.084381, 4.3990e-04,
-1.0631] #last 5 columns
discadj_fsi.su2_exec = "SU2_CFD_AD"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
###################################
### Coupled CHT Adjoint ###
###################################
# Coupled discrete adjoint for heatflux in heated cylinder array
discadj_cht = TestCase('discadj_cht')
discadj_cht.cfg_dir = "coupled_cht/disc_adj_incomp_2d"
discadj_cht.cfg_file = "cht_2d_3cylinders.cfg"
discadj_cht.test_iter = 10
discadj_cht.test_vals = [-2.364405, -3.085551, -3.085518,
-3.085513] #last 4 columns
discadj_cht.su2_exec = "SU2_CFD_AD"
discadj_cht.timeout = 1600
discadj_cht.tol = 0.00001
test_list.append(discadj_cht)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
######################################
### RUN PYTHON TESTS ###
######################################
# test discrete_adjoint.py
discadj_euler_py = TestCase('discadj_euler_py')
discadj_euler_py.cfg_dir = "cont_adj_euler/naca0012"
discadj_euler_py.cfg_file = "inv_NACA0012.cfg"
discadj_euler_py.test_iter = 10
discadj_euler_py.su2_exec = "discrete_adjoint.py -f"
discadj_euler_py.timeout = 1600
discadj_euler_py.reference_file = "of_grad_cd_disc.dat.ref"
discadj_euler_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_euler_py.run_filediff())
test_list.append(discadj_euler_py)
# test discrete_adjoint with multiple ffd boxes
discadj_multiple_ffd_py = TestCase('discadj_multiple_ffd_py')
discadj_multiple_ffd_py.cfg_dir = "multiple_ffd/naca0012"
discadj_multiple_ffd_py.cfg_file = "inv_NACA0012_ffd.cfg"
discadj_multiple_ffd_py.test_iter = 9
discadj_multiple_ffd_py.su2_exec = "discrete_adjoint.py -f"
discadj_multiple_ffd_py.timeout = 1600
discadj_multiple_ffd_py.reference_file = "of_grad_cd.dat.ref"
discadj_multiple_ffd_py.test_file = "of_grad_cd.dat"
pass_list.append(discadj_multiple_ffd_py.run_filediff())
test_list.append(discadj_multiple_ffd_py)
# test direct_differentiation.py
directdiff_euler_py = TestCase('directdiff_euler_py')
directdiff_euler_py.cfg_dir = "cont_adj_euler/naca0012"
directdiff_euler_py.cfg_file = "inv_NACA0012_FD.cfg"
directdiff_euler_py.test_iter = 10
directdiff_euler_py.su2_exec = "direct_differentiation.py -f"
directdiff_euler_py.timeout = 1600
directdiff_euler_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_euler_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_euler_py.run_filediff())
test_list.append(directdiff_euler_py)
# test direct_differentiation.py with multiple ffd boxes
directdiff_multiple_ffd_py = TestCase('directdiff_multiple_ffd_py')
directdiff_multiple_ffd_py.cfg_dir = "multiple_ffd/naca0012"
directdiff_multiple_ffd_py.cfg_file = "inv_NACA0012_ffd.cfg"
directdiff_multiple_ffd_py.test_iter = 9
directdiff_multiple_ffd_py.su2_exec = "direct_differentiation.py -f"
directdiff_multiple_ffd_py.timeout = 1600
directdiff_multiple_ffd_py.reference_file = "of_grad_directdiff.dat.ref"
directdiff_multiple_ffd_py.test_file = "DIRECTDIFF/of_grad_directdiff.dat"
pass_list.append(directdiff_multiple_ffd_py.run_filediff())
test_list.append(directdiff_multiple_ffd_py)
# test continuous_adjoint.py, with multiple objectives
# discadj_multi_py = TestCase('discadj_multi_py')
# discadj_multi_py.cfg_dir = "cont_adj_euler/wedge"
# discadj_multi_py.cfg_file = "inv_wedge_ROE_multiobj.cfg"
# discadj_multi_py.test_iter = 10
# discadj_multi_py.su2_exec = "discrete_adjoint.py"
# discadj_multi_py.timeout = 1600
# discadj_multi_py.reference_file = "of_grad_combo.dat.refdiscrete"
# discadj_multi_py.test_file = "of_grad_combo.dat"
# pass_list.append(discadj_multi_py.run_filediff())
# test_list.append(discadj_multi_py)
# FEA AD Flow Load Sensitivity
pywrapper_FEA_AD_FlowLoad = TestCase('pywrapper_FEA_AD_FlowLoad')
pywrapper_FEA_AD_FlowLoad.cfg_dir = "py_wrapper/disc_adj_fea/flow_load_sens"
pywrapper_FEA_AD_FlowLoad.cfg_file = "configAD_fem.cfg"
pywrapper_FEA_AD_FlowLoad.test_iter = 100
pywrapper_FEA_AD_FlowLoad.test_vals = [
-0.13945587401579657, -0.585985886606256, -0.00036377840086080753,
-0.0031005670174756375
] #last 4 columns
pywrapper_FEA_AD_FlowLoad.su2_exec = "python run_adjoint.py -f"
pywrapper_FEA_AD_FlowLoad.timeout = 1600
pywrapper_FEA_AD_FlowLoad.tol = 0.000001
pywrapper_FEA_AD_FlowLoad.new_output = False
test_list.append(pywrapper_FEA_AD_FlowLoad)
pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
# Flow AD Mesh Displacement Sensitivity
pywrapper_FEA_AD_FlowLoad = TestCase('pywrapper_CFD_AD_MeshDisp')
pywrapper_FEA_AD_FlowLoad.cfg_dir = "py_wrapper/disc_adj_flow/mesh_disp_sens"
pywrapper_FEA_AD_FlowLoad.cfg_file = "configAD_flow.cfg"
pywrapper_FEA_AD_FlowLoad.test_iter = 1000
pywrapper_FEA_AD_FlowLoad.test_vals = [
30.000000, -2.518695, 1.390150, 0.000000
] #last 4 columns
pywrapper_FEA_AD_FlowLoad.su2_exec = "python run_adjoint.py -f"
pywrapper_FEA_AD_FlowLoad.timeout = 1600
pywrapper_FEA_AD_FlowLoad.tol = 0.000001
pywrapper_FEA_AD_FlowLoad.new_output = False
test_list.append(pywrapper_FEA_AD_FlowLoad)
pass_list.append(pywrapper_FEA_AD_FlowLoad.run_test())
# Tests summary
print('==================================================================')
print('Summary of the serial tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s' % test.tag)
else:
print('* FAILED - %s' % test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606963, -9.034619, -0.000000,
0.005688] #last 4 columns
discadj_naca0012.su2_exec = "parallel_computation.py -f"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [
-1.751997, 0.485368, 0.182890, -0.000018
] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [
-1.655243, -0.507187, 0.129010, -0.000013
] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 10
discadj_cylinder.test_vals = [3.522085, -1.787791, -0.012031,
0.000017] #last 4 columns
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
# Tests summary
print '=================================================================='
print 'Summary of the parallel tests'
for i, test in enumerate(test_list):
if (pass_list[i]):
print ' passed - %s' % test.tag
else:
print '* FAILED - %s' % test.tag
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606841, -9.035214, -0.000000,
0.005688] #last 4 columns
discadj_naca0012.su2_exec = "parallel_computation.py -f"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.720476, -4.039256, 0.000000,
0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "parallel_computation.py -f"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [
-1.751965, 0.485796, 0.182895, -0.000018
] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [
-1.654193, -0.499281, 0.145545, -0.000018
] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "cont_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [
-2.917789, -2.714752, 0.000000, 0.000000
] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "cont_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "lam_incomp_cylinder_disc.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [
-2.727423, -2.272530, 0.000000, 0.000000
] #last 4 columns
discadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012
discadj_incomp_turb_NACA0012 = TestCase('discadj_incomp_turb_NACA0012')
discadj_incomp_turb_NACA0012.cfg_dir = "incomp_rans/naca0012"
discadj_incomp_turb_NACA0012.cfg_file = "naca0012_disc.cfg"
discadj_incomp_turb_NACA0012.test_iter = 100
discadj_incomp_turb_NACA0012.test_vals = [
-3.645810, -1.625922, 0.000000, 0.000000
] #last 4 columns
discadj_incomp_turb_NACA0012.su2_exec = "parallel_computation.py -f"
discadj_incomp_turb_NACA0012.timeout = 1600
discadj_incomp_turb_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [
3.746900, -1.544893, -8.3447e-03, 1.3808e-05
] #last 4 columns
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
#######################################################
### Disc. adj. turbomachinery ###
#######################################################
# Transonic Stator 2D
discadj_trans_stator = TestCase('transonic_stator')
discadj_trans_stator.cfg_dir = "disc_adj_turbomachinery/transonic_stator_2D"
discadj_trans_stator.cfg_file = "transonic_stator.cfg"
discadj_trans_stator.test_iter = 79
discadj_trans_stator.test_vals = [
-2.001081, -2.115303, -0.450996, -15.778175
] #last 4 columns
discadj_trans_stator.su2_exec = "parallel_computation.py -f"
discadj_trans_stator.timeout = 1600
discadj_trans_stator.tol = 0.00001
test_list.append(discadj_trans_stator)
###################################
### Structural Adjoint ###
###################################
# Turbulent Cylinder
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 9
discadj_fea.test_vals = [-4.872191, -5.131614, -3.6413e-04,
-8.7087e+00] #last 4 columns
discadj_fea.su2_exec = "parallel_computation.py -f"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Coupled FSI Adjoint ###
###################################
# Structural model
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "configAD_fsi.cfg"
discadj_fsi.test_iter = 3000
discadj_fsi.test_vals = [0.958848, -0.157183, 0.658415,
1.302076] #last 4 columns
discadj_fsi.su2_exec = "parallel_computation.py -f"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
######################################
### RUN TESTS ###
######################################
pass_list = [test.run_test() for test in test_list]
# Tests summary
print('==================================================================')
print('Summary of the parallel tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s' % test.tag)
else:
print('* FAILED - %s' % test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
def main():
'''This program runs SU2 and ensures that the output matches specified values.
This will be used to do checks when code is pushed to github
to make sure nothing is broken. '''
test_list = []
#####################################
### Disc. adj. compressible Euler ###
#####################################
# Inviscid NACA0012
discadj_naca0012 = TestCase('discadj_naca0012')
discadj_naca0012.cfg_dir = "cont_adj_euler/naca0012"
discadj_naca0012.cfg_file = "inv_NACA0012_discadj.cfg"
discadj_naca0012.test_iter = 100
discadj_naca0012.test_vals = [-3.606841, -9.035214, -0.000000, 0.005688] #last 4 columns
discadj_naca0012.su2_exec = "parallel_computation.py -f"
discadj_naca0012.timeout = 1600
discadj_naca0012.tol = 0.00001
test_list.append(discadj_naca0012)
# Inviscid Cylinder 3D (multiple markers)
discadj_cylinder3D = TestCase('discadj_cylinder3D')
discadj_cylinder3D.cfg_dir = "disc_adj_euler/cylinder3D"
discadj_cylinder3D.cfg_file = "inv_cylinder3D.cfg"
discadj_cylinder3D.test_iter = 5
discadj_cylinder3D.test_vals = [-3.719306, -4.038129, 0.000000, 0.000000] #last 4 columns
discadj_cylinder3D.su2_exec = "parallel_computation.py -f"
discadj_cylinder3D.timeout = 1600
discadj_cylinder3D.tol = 0.00001
test_list.append(discadj_cylinder3D)
# Arina nozzle 2D
discadj_arina2k = TestCase('discadj_arina2k')
discadj_arina2k.cfg_dir = "disc_adj_euler/arina2k"
discadj_arina2k.cfg_file = "Arina2KRS.cfg"
discadj_arina2k.test_iter = 20
discadj_arina2k.test_vals = [2.229071, 1.716910, 4.7258e+04, 0.0000e+00] #last 4 columns
discadj_arina2k.su2_exec = "parallel_computation.py -f"
discadj_arina2k.timeout = 8400
discadj_arina2k.tol = 0.00001
test_list.append(discadj_arina2k)
####################################
### Disc. adj. compressible RANS ###
####################################
# Adjoint turbulent NACA0012 SA
discadj_rans_naca0012_sa = TestCase('discadj_rans_naca0012_sa')
discadj_rans_naca0012_sa.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sa.cfg_file = "turb_NACA0012_sa.cfg"
discadj_rans_naca0012_sa.test_iter = 10
discadj_rans_naca0012_sa.test_vals = [-1.751966, 0.485717, 0.183154, -0.000018] #last 4 columns
discadj_rans_naca0012_sa.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sa.timeout = 1600
discadj_rans_naca0012_sa.tol = 0.00001
test_list.append(discadj_rans_naca0012_sa)
# Adjoint turbulent NACA0012 SST
discadj_rans_naca0012_sst = TestCase('discadj_rans_naca0012_sst')
discadj_rans_naca0012_sst.cfg_dir = "disc_adj_rans/naca0012"
discadj_rans_naca0012_sst.cfg_file = "turb_NACA0012_sst.cfg"
discadj_rans_naca0012_sst.test_iter = 10
discadj_rans_naca0012_sst.test_vals = [-1.654042, -0.500718, 0.154704, -0.000022] #last 4 columns
discadj_rans_naca0012_sst.su2_exec = "parallel_computation.py -f"
discadj_rans_naca0012_sst.timeout = 1600
discadj_rans_naca0012_sst.tol = 0.00001
test_list.append(discadj_rans_naca0012_sst)
#######################################
### Disc. adj. incompressible Euler ###
#######################################
# Adjoint Incompressible Inviscid NACA0012
discadj_incomp_NACA0012 = TestCase('discadj_incomp_NACA0012')
discadj_incomp_NACA0012.cfg_dir = "disc_adj_incomp_euler/naca0012"
discadj_incomp_NACA0012.cfg_file = "incomp_NACA0012_disc.cfg"
discadj_incomp_NACA0012.test_iter = 20
discadj_incomp_NACA0012.test_vals = [-3.595580, -2.549720, 0.000000, 0.000000] #last 4 columns
discadj_incomp_NACA0012.su2_exec = "parallel_computation.py -f"
discadj_incomp_NACA0012.timeout = 1600
discadj_incomp_NACA0012.tol = 0.00001
test_list.append(discadj_incomp_NACA0012)
#####################################
### Disc. adj. incompressible N-S ###
#####################################
# Adjoint Incompressible Viscous Cylinder (Heated)
discadj_incomp_cylinder = TestCase('discadj_incomp_cylinder')
discadj_incomp_cylinder.cfg_dir = "disc_adj_incomp_navierstokes/cylinder"
discadj_incomp_cylinder.cfg_file = "heated_cylinder.cfg"
discadj_incomp_cylinder.test_iter = 20
discadj_incomp_cylinder.test_vals = [-2.104640, -2.004547, 0.0000e+00, 0.0000e+00] #last 4 columns
discadj_incomp_cylinder.su2_exec = "parallel_computation.py -f"
discadj_incomp_cylinder.timeout = 1600
discadj_incomp_cylinder.tol = 0.00001
test_list.append(discadj_incomp_cylinder)
######################################
### Disc. adj. incompressible RANS ###
######################################
# Adjoint Incompressible Turbulent NACA 0012 SA
discadj_incomp_turb_NACA0012_sa = TestCase('discadj_incomp_turb_NACA0012_sa')
discadj_incomp_turb_NACA0012_sa.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sa.cfg_file = "turb_naca0012_sa.cfg"
discadj_incomp_turb_NACA0012_sa.test_iter = 10
discadj_incomp_turb_NACA0012_sa.test_vals = [-3.846036, -1.031071, 0.000000, 0.000000] #last 4 columns
discadj_incomp_turb_NACA0012_sa.su2_exec = "parallel_computation.py -f"
discadj_incomp_turb_NACA0012_sa.timeout = 1600
discadj_incomp_turb_NACA0012_sa.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sa)
# Adjoint Incompressible Turbulent NACA 0012 SST
discadj_incomp_turb_NACA0012_sst = TestCase('discadj_incomp_turb_NACA0012_sst')
discadj_incomp_turb_NACA0012_sst.cfg_dir = "disc_adj_incomp_rans/naca0012"
discadj_incomp_turb_NACA0012_sst.cfg_file = "turb_naca0012_sst.cfg"
discadj_incomp_turb_NACA0012_sst.test_iter = 10
discadj_incomp_turb_NACA0012_sst.test_vals = [-3.845805, -2.416675, 0.000000, 0.000000] #last 4 columns
discadj_incomp_turb_NACA0012_sst.su2_exec = "parallel_computation.py -f"
discadj_incomp_turb_NACA0012_sst.timeout = 1600
discadj_incomp_turb_NACA0012_sst.tol = 0.00001
test_list.append(discadj_incomp_turb_NACA0012_sst)
#######################################################
### Unsteady Disc. adj. compressible RANS ###
#######################################################
# Turbulent Cylinder
discadj_cylinder = TestCase('unsteady_cylinder')
discadj_cylinder.cfg_dir = "disc_adj_rans/cylinder"
discadj_cylinder.cfg_file = "cylinder.cfg"
discadj_cylinder.test_iter = 9
discadj_cylinder.test_vals = [3.746900, -1.544893, -8.3447e-03, 1.3808e-05] #last 4 columns
discadj_cylinder.su2_exec = "parallel_computation.py -f"
discadj_cylinder.timeout = 1600
discadj_cylinder.tol = 0.00001
discadj_cylinder.unsteady = True
test_list.append(discadj_cylinder)
##########################################################################
### Unsteady Disc. adj. compressible RANS DualTimeStepping 1st order ###
##########################################################################
# Turbulent Cylinder
discadj_DT_1ST_cylinder = TestCase('unsteady_cylinder_DT_1ST')
discadj_DT_1ST_cylinder.cfg_dir = "disc_adj_rans/cylinder_DT_1ST"
discadj_DT_1ST_cylinder.cfg_file = "cylinder.cfg"
discadj_DT_1ST_cylinder.test_iter = 9
discadj_DT_1ST_cylinder.test_vals = [3.698165, -1.607052, -2.2503e-03, 2.7212e-05] #last 4 columns
discadj_DT_1ST_cylinder.su2_exec = "parallel_computation.py -f"
discadj_DT_1ST_cylinder.timeout = 1600
discadj_DT_1ST_cylinder.tol = 0.00001
discadj_DT_1ST_cylinder.unsteady = True
test_list.append(discadj_DT_1ST_cylinder)
#######################################################
### Disc. adj. turbomachinery ###
#######################################################
# Transonic Stator 2D
discadj_trans_stator = TestCase('transonic_stator')
discadj_trans_stator.cfg_dir = "disc_adj_turbomachinery/transonic_stator_2D"
discadj_trans_stator.cfg_file = "transonic_stator.cfg"
discadj_trans_stator.test_iter = 79
discadj_trans_stator.test_vals = [-2.001082, -2.115018, -0.450986, -15.778292] #last 4 columns
discadj_trans_stator.su2_exec = "parallel_computation.py -f"
discadj_trans_stator.timeout = 1600
discadj_trans_stator.tol = 0.00001
test_list.append(discadj_trans_stator)
###################################
### Structural Adjoint ###
###################################
# Structural model
discadj_fea = TestCase('discadj_fea')
discadj_fea.cfg_dir = "disc_adj_fea"
discadj_fea.cfg_file = "configAD_fem.cfg"
discadj_fea.test_iter = 9
discadj_fea.test_vals = [-4.751576, -4.692029, -0.000364, -8.708700] #last 4 columns
discadj_fea.su2_exec = "parallel_computation.py -f"
discadj_fea.timeout = 1600
discadj_fea.tol = 0.00001
test_list.append(discadj_fea)
###################################
### Disc. adj. heat ###
###################################
# Discrete adjoint for heated cylinder
discadj_heat = TestCase('discadj_heat')
discadj_heat.cfg_dir = "disc_adj_heat"
discadj_heat.cfg_file = "disc_adj_heat.cfg"
discadj_heat.test_iter = 10
discadj_heat.test_vals = [3.162960, 0.923834, -223.148728, -3562.233908] #last 4 columns
discadj_heat.su2_exec = "parallel_computation.py -f"
discadj_heat.timeout = 1600
discadj_heat.tol = 0.00001
test_list.append(discadj_heat)
###################################
### Coupled FSI Adjoint ###
###################################
# Structural model
discadj_fsi = TestCase('discadj_fsi')
discadj_fsi.cfg_dir = "disc_adj_fsi"
discadj_fsi.cfg_file = "configAD_fsi.cfg"
discadj_fsi.test_iter = 3000
discadj_fsi.test_vals = [0.958848,-0.157183,0.658415,1.302076] #last 4 columns
discadj_fsi.su2_exec = "parallel_computation.py -f"
discadj_fsi.timeout = 1600
discadj_fsi.tol = 0.00001
test_list.append(discadj_fsi)
######################################
### RUN TESTS ###
######################################
pass_list = [ test.run_test() for test in test_list ]
##################################################
### Structural Adjoint - Topology Optimization ###
##################################################
# test discrete_adjoint.py
discadj_topol_optim = TestCase('discadj_topol_optim')
discadj_topol_optim.cfg_dir = "fea_topology"
discadj_topol_optim.cfg_file = "config.cfg"
discadj_topol_optim.test_iter = 0
discadj_topol_optim.su2_exec = "parallel_computation.py"
discadj_topol_optim.timeout = 1600
discadj_topol_optim.reference_file = "grad_ref_node.dat.ref"
discadj_topol_optim.test_file = "grad_ref_node.dat"
pass_list.append(discadj_topol_optim.run_filediff())
test_list.append(discadj_topol_optim)
###################################
### Coupled FSI Adjoint ###
###################################
discadj_fsi2 = TestCase('discadj_fsi_airfoil')
discadj_fsi2.cfg_dir = "disc_adj_fsi/Airfoil_2d"
discadj_fsi2.cfg_file = "config.cfg"
discadj_fsi2.test_iter = 0
discadj_fsi2.su2_exec = "parallel_computation.py"
discadj_fsi2.timeout = 1600
discadj_fsi2.reference_file = "grad_young.opt.ref"
discadj_fsi2.test_file = "grad_young.opt"
pass_list.append(discadj_fsi2.run_filediff())
test_list.append(discadj_fsi2)
# Tests summary
print('==================================================================')
print('Summary of the parallel tests')
print('python version:', sys.version)
for i, test in enumerate(test_list):
if (pass_list[i]):
print(' passed - %s'%test.tag)
else:
print('* FAILED - %s'%test.tag)
if all(pass_list):
sys.exit(0)
else:
sys.exit(1)
