def setUp(self):
if not hasattr(self, "name"):
# return immediately when the setup method is being called on the based class and NOT the
# classes created using parametrized
# this will happen when training, but will hopefully be fixed down the line
return
super().setUp()
options = copy.copy(adflowDefOpts)
options["outputdirectory"] = os.path.join(baseDir, options["outputdirectory"])
options.update(self.options)
self.ffdFile = os.path.join(baseDir, "../../input_files/mdo_tutorial_ffd.fmt")
mesh_options = copy.copy(IDWarpDefOpts)
mesh_options.update({"gridFile": options["gridfile"]})
self.ap = copy.deepcopy(self.aero_prob)
# Setup aeroproblem
self.ap.evalFuncs = self.evalFuncs
# add the default dvs to the problem
for dv in defaultAeroDVs:
self.ap.addDV(dv)
self.CFDSolver = ADFLOW(options=options, debug=True)
self.CFDSolver.setMesh(USMesh(options=mesh_options))
self.CFDSolver.setDVGeo(setDVGeo(self.ffdFile, cmplx=False))
# propagates the values from the restart file throughout the code
self.CFDSolver.getResidual(self.ap)
def setup_cb(comm):
# Create the solver
CFDSolver = ADFLOW(options=options, comm=comm, debug=False)
# Setup geometry/mesh
DVGeo = DVGeometry(ffdFile)
nTwist = 6
DVGeo.addRefAxis(
'wing',
Curve(x=numpy.linspace(5.0 / 4.0, 1.5 / 4.0 + 7.5, nTwist),
y=numpy.zeros(nTwist),
z=numpy.linspace(0, 14, nTwist),
k=2))
def twist(val, geo):
for i in range(nTwist):
geo.rot_z['wing'].coef[i] = val[i]
DVGeo.addGeoDVGlobal('twist', [0] * nTwist,
twist,
lower=-10,
upper=10,
scale=1.0)
DVGeo.addGeoDVLocal('shape', lower=-0.5, upper=0.5, axis='y', scale=10.0)
mesh = USMesh(options=meshOptions, comm=comm)
CFDSolver.setMesh(mesh)
CFDSolver.setDVGeo(DVGeo)
return CFDSolver, mesh, DVGeo, None
def test4():
# Test the MDO tutorial h mesh
file_name = '../input_files/mdo_tutorial_face_bcs.cgns'
meshOptions = copy.deepcopy(defOpts)
meshOptions.update({
'gridFile': file_name,
'fileType': 'cgns',
'symmetryPlanes': [[[0, 0, 0], [0, 0, 1]]],
})
# Create warping object
mesh = USMesh(options=meshOptions)
# Extract Surface Coordinates
coords0 = mesh.getSurfaceCoordinates()
vCoords = mesh.getCommonGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of vCoords Inital:')
reg_write(val, 1e-8, 1e-8)
new_coords = coords0.copy()
# Do a shearing sweep deflection:
for i in range(len(coords0)):
span = coords0[i, 2]
new_coords[i, 0] += .05 * span
# Reset the newly computed surface coordiantes
mesh.setSurfaceCoordinates(new_coords)
mesh.warpMesh()
# Get the sum of the warped coordinates
#vCoords = mesh.getSolverGrid()
vCoords = mesh.getWarpGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of vCoords Warped:')
reg_write(val, 1e-8, 1e-8)
# Create a dXv vector to do test the mesh warping with:
dXv_warp = numpy.linspace(0, 1.0, mesh.warp.griddata.warpmeshdof)
if MPI.COMM_WORLD.rank == 0:
print('Computing Warp Deriv')
mesh.warpDeriv(dXv_warp, solverVec=False)
dXs = mesh.getdXs()
val = MPI.COMM_WORLD.reduce(numpy.sum(dXs.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of dxs:')
reg_write(val, 1e-8, 1e-8)
if MPI.COMM_WORLD.rank == 0:
print('Verifying Warp Deriv')
mesh.verifyWarpDeriv(dXv_warp, solverVec=False, dofStart=0, dofEnd=5)
def test3():
# Test the mdo tutorial o mesh
file_name = "../input_files/o_mesh.cgns"
meshOptions = copy.deepcopy(defOpts)
meshOptions.update({"gridFile": file_name, "fileType": "cgns"})
# Create warping object
mesh = USMesh(options=meshOptions)
# Extract Surface Coordinates
coords0 = mesh.getSurfaceCoordinates()
vCoords = mesh.getCommonGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print("Sum of vCoords Inital:")
reg_write(val, 1e-8, 1e-8)
new_coords = coords0.copy()
# Do a shearing sweep deflection:
for i in range(len(coords0)):
span = coords0[i, 2]
new_coords[i, 0] += 0.05 * span
# Reset the newly computed surface coordiantes
mesh.setSurfaceCoordinates(new_coords)
mesh.warpMesh()
# Get the sum of the warped coordinates
# vCoords = mesh.getSolverGrid()
vCoords = mesh.getWarpGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print("Sum of vCoords Warped:")
reg_write(val, 1e-8, 1e-8)
# Create a dXv vector to do test the mesh warping with:
dXv_warp = numpy.linspace(0, 1.0, mesh.warp.griddata.warpmeshdof)
if MPI.COMM_WORLD.rank == 0:
print("Computing Warp Deriv")
mesh.warpDeriv(dXv_warp, solverVec=False)
dXs = mesh.getdXs()
val = MPI.COMM_WORLD.reduce(numpy.sum(dXs.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print("Sum of dxs:")
reg_write(val, 1e-8, 1e-8)
if MPI.COMM_WORLD.rank == 0:
print("Verifying Warp Deriv")
mesh.verifyWarpDeriv(dXv_warp, solverVec=False, dofStart=0, dofEnd=5)
def test1():
# Test the Ahmed body openfoam mesh
sys.stdout.flush()
#change directory to the correct test case
os.chdir('./input/ahmedBodyMesh/')
file_name = os.getcwd()
meshOptions = copy.deepcopy(defOpts)
meshOptions.update({
'gridFile': file_name,
'fileType': 'openfoam',
'symmetryPlanes': [[[0, 0, 0], [0, 1, 0]]],
})
# Create warping object
mesh = USMesh(options=meshOptions, debug=True)
# Extract Surface Coordinates
coords0 = mesh.getSurfaceCoordinates()
vCoords = mesh.getCommonGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of vCoords Inital:')
reg_write(val, 1e-8, 1e-8)
new_coords = coords0.copy()
# Do a stretch:
for i in range(len(coords0)):
length = coords0[i, 2]
new_coords[i, 0] += .05 * length
# Reset the newly computed surface coordiantes
mesh.setSurfaceCoordinates(new_coords)
mesh.warpMesh()
vCoords = mesh.getWarpGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of vCoords Warped:')
reg_write(val, 1e-8, 1e-8)
# Create a dXv vector to do test the mesh warping with:
dXv_warp = numpy.linspace(0, 1.0, mesh.warp.griddata.warpmeshdof)
if not 'complex' in sys.argv:
if MPI.COMM_WORLD.rank == 0:
print('Computing Warp Deriv')
mesh.warpDeriv(dXv_warp, solverVec=False)
dXs = mesh.getdXs()
val = MPI.COMM_WORLD.reduce(numpy.sum(dXs.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of dxs:')
reg_write(val, 1e-8, 1e-8)
else:
# add a complex perturbation on all surface nodes simultaneously:
for i in range(len(coords0)):
new_coords[i, :] += h * 1j
# Reset the newly computed surface coordiantes
mesh.setSurfaceCoordinates(new_coords)
mesh.warpMesh()
vCoords = mesh.getWarpGrid()
deriv = numpy.imag(vCoords) / h
deriv = numpy.dot(dXv_warp, deriv)
val = MPI.COMM_WORLD.reduce(numpy.sum(deriv), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of dxs:')
reg_write(val, 1e-8, 1e-8)
del mesh
#os.system('rm -fr *.cgns *.dat')
#change back to the original directory
os.chdir('../../')
def setUp(self):
# Introduce a transfer class for displacement transfer from struct to aero.
class Transfer:
# simplified transfer class
# converting csd displacement to cfd surface nodes
def __init__(self, alpha, xRot, aeroSolver):
# takes in displacement history
self.alpha = alpha
self.ntimeintervalsspectral = len(alpha)
self.aeroSolver = aeroSolver # a shallow copy of CFD solver
self.xRot = xRot
def getUndeformedSurfaceNodes(self):
self.MDGroup = self.aeroSolver.allWallsGroup
self.cfdPts0 = self.aeroSolver.getSurfaceCoordinates(self.MDGroup, includeZipper=False)
def setDisplacements(self):
xRot = self.xRot
ntimeintervalsspectral = self.ntimeintervalsspectral
alpha = self.alpha # notice a shallow copy introduced here; dont change the underlying obj!
cfdPoints_init = self.cfdPts0 # notice a shallow copy introduced here; dont change the underlying obj!
N_pts = cfdPoints_init.shape[0]
self.cfdPts = []
for sps in range(ntimeintervalsspectral):
cfdPoints_deformed = numpy.zeros((N_pts, 3))
ptch_loc = alpha[sps]
cc = numpy.cos(ptch_loc)
ss = numpy.sin(ptch_loc)
for j in range(N_pts):
cfdPoints_deformed[j, 0] = cc * (cfdPoints_init[j, 0] - xRot) + ss * cfdPoints_init[j, 1] + xRot
cfdPoints_deformed[j, 1] = -ss * (cfdPoints_init[j, 0] - xRot) + cc * cfdPoints_init[j, 1]
cfdPoints_deformed[j, 2] = cfdPoints_init[j, 2]
self.cfdPts.append(cfdPoints_deformed)
def setVolumeMesh(self):
ntimeintervalsspectral = self.ntimeintervalsspectral
for sps in range(ntimeintervalsspectral):
self.aeroSolver.mesh.setSurfaceCoordinates(self.cfdPts[sps])
self.aeroSolver.mesh.warpMesh()
m = self.aeroSolver.mesh.getSolverGrid()
self.aeroSolver.adflow.warping.setgridforoneinstance(m, sps=sps + 1)
self.aeroSolver._updateGeomInfo = True
self.aeroSolver.updateGeometryInfo()
# Set up the test for the parent RegTest class.
super().setUp()
gridFile = os.path.join(baseDir, "../../input_files/naca64A010_euler-L2.cgns")
ntimeintervalsspectral = 3
options = copy.copy(adflowDefOpts)
options.update(
{
"gridfile": gridFile,
"outputDirectory": os.path.join(baseDir, "../output_files"),
"writeVolumeSolution": False,
"writeSurfaceSolution": False,
"blocksplitting": True,
"useblockettes": False,
"equationtype": "Euler",
"equationmode": "time spectral",
"mgcycle": "sg",
"l2convergence": 1e-15,
"ncycles": 200000,
"monitorvariables": ["resrho", "cl"],
"usenksolver": True,
"nkswitchtol": 1e-4,
"NKSubSpaceSize": 400,
"applypcsubspacesize": 400,
"useanksolver": True,
"ankswitchtol": 1e-2,
"anksubspacesize": 50,
"alphafollowing": False,
"timeintervals": ntimeintervalsspectral,
"useexternaldynamicmesh": True,
"usetsinterpolatedgridvelocity": True,
}
)
# Grid option
meshOptions = {
"gridFile": gridFile,
}
# Setup aeroproblem
self.ap = copy.copy(ap_naca64A010_time_spectral)
# Motion history
alpha_0 = 1.01
deltaAlpha = -alpha_0 * numpy.pi / 180.0
alpha = numpy.linspace(0.0, 2.0 * numpy.pi, ntimeintervalsspectral + 1)[:-1]
alpha = -numpy.sin(alpha)
alpha *= deltaAlpha
# Create the solver
self.CFDSolver = ADFLOW(options=options, debug=False)
# self.CFDSolver.addSlices("z", [0.5])
# Deform the mesh
mesh = USMesh(options=meshOptions)
self.CFDSolver.setMesh(mesh)
# deformation
xRot = 0.25 # Hard copied from the reference file.
TSTransfer = Transfer(alpha, xRot, self.CFDSolver)
TSTransfer.getUndeformedSurfaceNodes()
TSTransfer.setDisplacements()
TSTransfer.setVolumeMesh()
"gridFile": "../../input_files/mdo_tutorial_face_bcs.cgns",
"fileType": "CGNS",
"symmetryPlanes": [[[0, 0, 0], [0, 0, 1]]],
"aExp": 3.0,
"bExp": 5.0,
"LdefFact": 1.0,
"alpha": 0.25,
"errTol": 0.0005,
"evalMode": "fast",
"symmTol": 1e-6,
"useRotations": True,
"bucketSize": 8,
}
# Create the mesh object
mesh = USMesh(options=options, comm=MPI.COMM_WORLD)
coords0 = mesh.getSurfaceCoordinates()
new_coords = coords0.copy()
for i in range(len(coords0)):
span = coords0[i, 2]
new_coords[i, 0] += 0.05 * span
new_coords[i, 1] += 0.05 * span
new_coords[i, 2] += 0.15 * span
# Reset the newly computed surface coordiantes
mesh.setSurfaceCoordinates(new_coords)
# Actually run the mesh warping
mesh.warpMesh()
def test1():
# Test the Ahmed body openfoam mesh
sys.stdout.flush()
#change directory to the correct test case
os.chdir('./input/ahmedBodyMesh/')
file_name = os.getcwd()
meshOptions = copy.deepcopy(defOpts)
meshOptions.update({
'gridFile': file_name,
'fileType': 'openfoam',
'symmetryPlanes': [[[0, 0, 0], [0, 1, 0]]],
})
# Create warping object
mesh = USMesh(options=meshOptions)
# Extract Surface Coordinates
coords0 = mesh.getSurfaceCoordinates()
vCoords = mesh.getCommonGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of vCoords Inital:')
reg_write(val, 1e-8, 1e-8)
new_coords = coords0.copy()
# Do a stretch:
for i in range(len(coords0)):
length = coords0[i, 2]
new_coords[i, 0] += .05 * length
# Reset the newly computed surface coordiantes
mesh.setSurfaceCoordinates(new_coords)
mesh.warpMesh()
vCoords = mesh.getWarpGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of vCoords Warped:')
reg_write(val, 1e-8, 1e-8)
# Create a dXv vector to do test the mesh warping with:
dXv_warp = numpy.linspace(0, 1.0, mesh.warp.griddata.warpmeshdof)
if MPI.COMM_WORLD.rank == 0:
print('Computing Warp Deriv')
mesh.warpDeriv(dXv_warp, solverVec=False)
dXs = mesh.getdXs()
val = MPI.COMM_WORLD.reduce(numpy.sum(dXs.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of dxs:')
reg_write(val, 1e-8, 1e-8)
if MPI.COMM_WORLD.rank == 0:
print('Verifying Warp Deriv')
mesh.verifyWarpDeriv(dXv_warp,
solverVec=False,
dofStart=0,
dofEnd=10,
h=1e-9)
#change back to the original directory
os.chdir('../../')
def twist(val, geo):
for i in xrange(nTwist):
geo.rot_z['wing'].coef[i] = val[i]
def span(val, geo):
# Span
C = geo.extractCoef('wing')
s = geo.extractS('wing')
for i in xrange(len(C)-1):
C[-1, 2] = C[-1, 2] + val[0]
geo.restoreCoef(C, 'wing')
DVGeo.addGeoDVGlobal('twist', [0]*nTwist, twist, lower=-10, upper=10, scale=1.0)
DVGeo.addGeoDVGlobal('span', [0], span, lower=-10, upper=10, scale=1.0)
DVGeo.addGeoDVLocal('shape', lower=-0.5, upper=0.5, axis='y', scale=10.0)
mesh = USMesh(options={'gridFile':'../inputFiles/mdo_tutorial_rans.cgns'})
CFDSolver.setMesh(mesh)
CFDSolver.setDVGeo(DVGeo)
#Aeroproblem must be set before we can call DVGeo.setDesignVars
CFDSolver.setAeroProblem(ap)
if not 'complex' in sys.argv:
# Solve system
CFDSolver(ap, writeSolution=False)
funcs = {}
CFDSolver.evalFunctions(ap, funcs)
# Solve sensitivities
funcsSens = {}
CFDSolver.evalFunctionsSens(ap, funcsSens)
# Write values and derivatives out:
if MPI.COMM_WORLD.rank == 0:
def MLMC(self):
# Use an MLMC algorithm to determine an optimal sample distribution between existing mesh levels
# We do this once before optimization, then compute statistics with the same set of samples at every iteration
# start with initial samples
# Get a set of UQ sample points (LHS), enough for each level at the start
#sys.stdout = open(os.devnull, "w")
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach'] #0.95
Re = self.ooptions['Re'] #50000
Re_L = 1.0
tempR = 540
arearef = 2.0
chordref = 1.0
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
self.current_samples = self.NS0 * self.Lmax
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
# Scatter samples on each level, multi-point parallelism
for i in range(self.Lmax):
self.cases.append(divide_cases(self.NS0, size))
for j in range(len(self.cases[i])):
for k in range(len(self.cases[i][j])):
self.cases[i][j][k] += i * self.NS0
#self.nsp.append(len(self.cases[i][rank]))#int(ns/size) # samples per processor
self.samplep.append(self.sample[self.cases[i][rank]])
#import pdb; pdb.set_trace()
#self.samplep = self.sample[self.cases[rank]]#self.sample[(rank*self.nsp):(rank*self.nsp+(self.nsp))] #shouldn't really need to "scatter" per se
#import pdb; pdb.set_trace()
# for i in range(self.Lmax):
# assert len(self.samplep[i]) == self.nsp[i]
# Actually create solvers (and aeroproblems?) (and mesh?) now
nslp = []
nslt = []
for k in range(self.Lmax):
alist = []
slist = []
mlist = []
alist2 = []
slist2 = []
mlist2 = []
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
for i in range(nslp[k]):
namestr = self.gridSol + "_" + str(self.cases[k][rank][i])
# create meshes
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[k]
mlist.append(USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[k]
alist.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
slist.append(ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
# if not self.ooptions['run_once']:
# saconstsm = self.samplep[i].tolist()
# else:
saconstsm = self.samplep[k][i].tolist()
self.saconsts = saconstsm + self.saconstsb
slist[i].setOption('SAConsts', self.saconsts)
slist[i].setDVGeo(self.DVGeo)
slist[i].setMesh(mlist[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist[i].allWallsGroup)
slist[i].DVGeo.addPointSet(coords, 'coords')
if k > 0: #create additional solvers at higher levels for the estimators
# create meshes
namestr = self.gridSol + "_" + str(
self.cases[k][rank][i]) + "_m"
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[k - 1]
mlist2.append(
USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[k - 1]
alist2.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(
0.1) # this solves a few problems for some reason
# create solvers
slist2.append(ADFLOW(options=aloptions,
comm=MPI.COMM_SELF))
slist2[i].setOption('SAConsts', self.saconsts)
slist2[i].setDVGeo(self.DVGeo)
slist2[i].setMesh(mlist2[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist2[i].allWallsGroup)
slist2[i].DVGeo.addPointSet(coords, 'coords')
self.aps.append(alist)
self.solvers.append(slist)
self.meshes.append(mlist)
if k > 0:
self.aps[k] += alist2
self.solvers[k] += slist2
self.meshes[k] += mlist2
#import pdb; pdb.set_trace()
# start looping over mesh levels
L = 0
M = 4.0 #0.5 #refinement factor?
converged = 0
eps = self.uoptions['vartol']
sum1 = []
mus = []
sump = []
musp = []
sumpm = []
muspm = []
summ = []
musm = []
E = []
V = []
N1 = []
while ~converged & L < self.Lmax:
# compute start up samples to estimate variance
dvdict = {'pnts': a_init['pnts']}
funcs = {}
nslp = []
nslt = []
for k in range(self.Lmax):
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
sump.append(0.)
musp.append(numpy.zeros(nslp[L]))
sumpm.append(0.)
muspm.append(numpy.zeros(nslp[L]))
for i in range(nslp[L]):
# just do this again in case
saconstsm = self.samplep[L][i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[L][i].setOption('SAConsts', self.saconsts)
self.solvers[L][i].DVGeo.setDesignVars(dvdict)
self.aps[L][i].setDesignVars(dvdict)
self.solvers[L][i](self.aps[L][i])
self.solvers[L][i].evalFunctions(self.aps[L][i], funcs)
astr = self.gridSol + "_" + str(self.cases[L][rank][i]) + "_cd"
musp[L][i] = funcs[astr]
sump[L] += funcs[astr]
#import pdb; pdb.set_trace()
if L > 0:
self.solvers[L][i + nslp[L]].setOption(
'SAConsts', self.saconsts)
self.solvers[L][i + nslp[L]].DVGeo.setDesignVars(dvdict)
self.aps[L][i + nslp[L]].setDesignVars(dvdict)
self.solvers[L][i + nslp[L]](self.aps[L][i + nslp[L]])
self.solvers[L][i + nslp[L]].evalFunctions(
self.aps[L][i + nslp[L]], funcs)
astr = self.gridSol + "_" + str(
self.cases[L][rank][i]) + "_m_cd"
muspm[L][i] = -funcs[astr]
sumpm[L] += -funcs[astr]
# compute mean and variance estimate from start up samples
sum1.append(comm.allreduce(sump[L]))
mus.append(comm.allgather(musp[L]))
summ.append(comm.allreduce(sumpm[L]))
musm.append(comm.allgather(muspm[L]))
#import pdb; pdb.set_trace()
# mean at each level
E = numpy.zeros(L + 1)
for l in range(L + 1):
E[l] = (sum1[l] + summ[l]) / nslt[l]
# variance at each level
V = numpy.zeros(L + 1)
for l in range(L + 1):
sum2 = 0.
for i in range(len(mus[l])): #range(size):
for j in range(len(mus[l][i])): #range(self.nsp):
if l > 0:
sum2 += ((mus[l][i][j] + musm[l][i][j]) - E[l])**2
else:
sum2 += (mus[l][i][j] - E[l])**2
V[l] = sum2 / nslt[l]
#import pdb; pdb.set_trace()
# now determine the optimal number of samples at each level
N1.append(0.)
worksum = 0
for l in range(L + 1):
worksum += numpy.sqrt(V[l] * (M**l))
for l in range(L + 1):
nlf = 2 * numpy.sqrt(V[l] / (M**l)) * worksum / (eps * eps)
nlfm = max(nslt[l], math.ceil(nlf))
N1[l] = nlfm
# now compute and generate additional samples at each level
# first partition samples NEVERMIND (just do it once at each level, no need to repeat)
# create the extra number of solvers at each (the current) level
# need to loop everything from here on
for l in range(L + 1):
alist = self.aps[l][0:nslp[l]]
slist = self.solvers[l][0:nslp[l]]
mlist = self.meshes[l][0:nslp[l]]
if l > 0:
alist2 = self.aps[l][nslp[l]:]
slist2 = self.solvers[l][nslp[l]:]
mlist2 = self.meshes[l][nslp[l]:]
self.naddedtot[l] = N1[l] - nslt[l]
self.current_samples += self.naddedtot[l]
#import pdb; pdb.set_trace()
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
if self.naddedtot[l] > 0:
temp = divide_cases(self.naddedtot[l], size)
for i in range(len(temp)):
for j in range(len(temp[i])):
temp[i][j] += self.current_samples - self.naddedtot[
l] #self.Lmax*self.NS0 + sum(self.naddedtot[0:L])
else:
temp = []
if len(temp):
for ns in range(size):
self.cases[l][ns] += temp[ns] #append
nslpnew = len(self.cases[l][rank])
nsltnew = sum([len(self.cases[l][x]) for x in range(size)])
#self.nsp[L] = len(self.cases[L][rank]) #int(ns/size) # samples per processor
self.samplep[l] = self.sample[self.cases[l][rank]]
for i in range(nslp[l],
nslpnew): #need it to be just the extra cases
#import pdb; pdb.set_trace()
namestr = self.gridSol + "_" + str(self.cases[l][rank][i])
# create meshes
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[l]
mlist.append(
USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[l]
alist.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(
0.1) # this solves a few problems for some reason
# create solvers
slist.append(ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
saconstsm = self.samplep[l][i].tolist()
self.saconsts = saconstsm + self.saconstsb
slist[i].setOption('SAConsts', self.saconsts)
slist[i].setDVGeo(self.DVGeo)
slist[i].setMesh(mlist[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist[i].allWallsGroup)
slist[i].DVGeo.addPointSet(coords, 'coords')
time.sleep(0.1)
if l > 0: #create additional solvers at higher levels for the estimators
# create meshes
#import pdb; pdb.set_trace()
namestr = self.gridSol + "_" + str(
self.cases[l][rank][i]) + "_m"
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[l - 1]
mlist2.append(
USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[l - 1]
alist2.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(
0.1) # this solves a few problems for some reason
# create solvers
slist2.append(
ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
slist2[i].setOption('SAConsts', self.saconsts)
slist2[i].setDVGeo(self.DVGeo)
slist2[i].setMesh(mlist2[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist2[i].allWallsGroup)
slist2[i].DVGeo.addPointSet(coords, 'coords')
nslp[l] = nslpnew
nslt[l] = nsltnew
self.aps[l] = alist
self.solvers[l] = slist
self.meshes[l] = mlist
if l > 0:
self.aps[l] += alist2
self.solvers[l] += slist2
self.meshes[l] += mlist2
# compute remaining samples
sump[l] = 0
sumpm[l] = 0
musp[l] = numpy.zeros(nslp[l])
muspm[l] = numpy.zeros(nslp[l])
for i in range(nslp[l]):
# just do this again in case
saconstsm = self.samplep[l][i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[l][i].setOption('SAConsts', self.saconsts)
self.solvers[l][i].DVGeo.setDesignVars(dvdict)
self.aps[l][i].setDesignVars(dvdict)
self.solvers[l][i](self.aps[l][i])
self.solvers[l][i].evalFunctions(self.aps[l][i], funcs)
astr = self.gridSol + "_" + str(
self.cases[l][rank][i]) + "_cd"
musp[l][i] = funcs[astr]
sump[l] += funcs[astr]
#import pdb; pdb.set_trace()
if l > 0:
self.solvers[l][i + nslp[l]].setOption(
'SAConsts', self.saconsts)
self.solvers[l][i +
nslp[l]].DVGeo.setDesignVars(dvdict)
self.aps[l][i + nslp[l]].setDesignVars(dvdict)
self.solvers[l][i + nslp[l]](self.aps[l][i + nslp[l]])
self.solvers[l][i + nslp[l]].evalFunctions(
self.aps[l][i + nslp[l]], funcs)
astr = self.gridSol + "_" + str(
self.cases[l][rank][i]) + "_m_cd"
muspm[l][i] = -funcs[astr]
sumpm[l] += -funcs[astr]
# compute mean and variance estimate from all samples
sum1[l] = comm.allreduce(sump[l])
mus[l] = comm.allgather(musp[l])
summ[l] = comm.allreduce(sumpm[l])
musm[l] = comm.allgather(muspm[l])
# mean at each level
E[l] = (sum1[l] + summ[l]) / nslt[l]
# variance at each level
sum2 = 0.
for i in range(len(mus[l])): #range(size):
for j in range(len(mus[l][i])): #range(self.nsp):
if l > 0:
sum2 += ((mus[l][i][j] + musm[l][i][j]) - E[l])**2
else:
sum2 += (mus[l][i][j] - E[l])**2
V[l] = sum2 / nslt[l]
# if L == 1:
# import pdb; pdb.set_trace()
L += 1
#import pdb; pdb.set_trace()
#sys.stdout = sys.__stdout__
if rank == 0:
print("MLMC Completed, Samples per level: ", N1)
self.N1 = N1
scale=1)
#rst Add local dvs
# Comment out one or the other
DVGeo.addGeoDVLocal('local', lower=-0.5, upper=0.5, axis='y', scale=1)
DVGeo.addGeoDVSectionLocal('slocal',
secIndex='k',
axis=1,
lower=-0.5,
upper=0.5,
scale=1)
#rst Embed points
gridFile = 'wing_vol.cgns'
meshOptions = {'gridFile': gridFile}
mesh = USMesh(options=meshOptions)
coords = mesh.getSurfaceCoordinates()
DVGeo.addPointSet(coords, 'coords')
#rst Change dvs
dvDict = DVGeo.getValues()
dvDict['twist'] = numpy.linspace(0, 50, nRefAxPts)[1:]
dvDict['dihedral'] = numpy.linspace(0, 3, nRefAxPts)[1:]
dvDict['taper'] = numpy.array([1.2, 0.5])
dvDict['slocal'][::5] = 0.5
DVGeo.setDesignVars(dvDict)
#rst Update
DVGeo.update('coords')
DVGeo.writePlot3d('ffd_deformed.xyz')
def MFMC(self):
# Use an MFMC algorithm to determine optimal sample distribution and coefficients among mesh levels
# We do this once before optimization, then compute statistics with the same set of samples and coeffs at every iteration
# start with initial samples
# Get a set of UQ sample points (LHS), enough for each level at the start
#sys.stdout = open(os.devnull, "w")
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach'] #0.95
Re = self.ooptions['Re'] #50000
Re_L = 1.0
tempR = 540
arearef = 2.0
chordref = 1.0
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
self.current_samples = self.NS0 * self.Lmax
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
N1 = []
a1 = numpy.zeros(self.Lmax)
r1 = numpy.zeros(self.Lmax)
# Scatter samples on each level, multi-point parallelism
for i in range(self.Lmax):
self.cases.append(divide_cases(self.NS0, size))
for j in range(len(self.cases[i])):
for k in range(len(self.cases[i][j])):
self.cases[i][j][k] += i * self.NS0
#self.nsp.append(len(self.cases[i][rank]))#int(ns/size) # samples per processor
self.samplep.append(self.sample[self.cases[i][rank]])
#import pdb; pdb.set_trace()
#self.samplep = self.sample[self.cases[rank]]#self.sample[(rank*self.nsp):(rank*self.nsp+(self.nsp))] #shouldn't really need to "scatter" per se
#import pdb; pdb.set_trace()
# for i in range(self.Lmax):
# assert len(self.samplep[i]) == self.nsp[i]
# Create solvers for the preliminary data
nslp = []
nslt = []
for k in range(self.Lmax):
alist = []
slist = []
mlist = []
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
for i in range(nslp[k]):
namestr = self.gridSol + "_" + str(self.cases[k][rank][i])
# create meshes
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[self.mord[k]]
#import pdb; pdb.set_trace()
mlist.append(USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[self.mord[k]]
alist.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
slist.append(ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
# if not self.ooptions['run_once']:
# saconstsm = self.samplep[i].tolist()
# else:
saconstsm = self.samplep[0][i].tolist()
self.saconsts = saconstsm + self.saconstsb
slist[i].setOption('SAConsts', self.saconsts)
slist[i].setDVGeo(self.DVGeo)
slist[i].setMesh(mlist[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist[i].allWallsGroup)
slist[i].DVGeo.addPointSet(coords, 'coords')
self.aps.append(alist)
self.solvers.append(slist)
self.meshes.append(mlist)
# Solve the preliminary samples
# start looping over mesh levels
sumt = []
sumtp = []
nslp = []
nslt = []
sum1 = []
mus = []
sump = []
musp = []
sumpm = []
muspm = []
summ = []
musm = []
Et = numpy.zeros(self.Lmax)
E = numpy.zeros(self.Lmax)
V = numpy.zeros(self.Lmax)
S = numpy.zeros(self.Lmax)
N1 = []
for k in range(self.Lmax):
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
dvdict = {'pnts': a_init['pnts']}
funcs = {}
sumtp.append(0.0)
sump.append(0.)
musp.append(numpy.zeros(nslp[k]))
sumpm.append(0.)
muspm.append(numpy.zeros(nslp[k]))
for i in range(nslp[k]):
# just do this again in case
saconstsm = self.samplep[0][i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[k][i].setOption('SAConsts', self.saconsts)
self.solvers[k][i].DVGeo.setDesignVars(dvdict)
self.aps[k][i].setDesignVars(dvdict)
pc0 = time.process_time()
self.solvers[k][i](self.aps[k][i])
self.solvers[k][i].evalFunctions(self.aps[k][i], funcs)
pc1 = time.process_time()
astr = self.gridSol + "_" + str(self.cases[k][rank][i]) + "_cd"
musp[k][i] = funcs[astr]
sump[k] += funcs[astr]
sumtp[k] += (pc1 - pc0)
# compute mean and variance estimate from start up samples
for k in range(self.Lmax):
sumt.append(comm.allreduce(sumtp[k]))
sum1.append(comm.allreduce(sump[k]))
mus.append(comm.allgather(musp[k]))
summ.append(comm.allreduce(sumpm[k]))
musm.append(comm.allgather(muspm[k]))
mus[k] = numpy.concatenate(mus[k][:])
musm[k] = numpy.concatenate(musm[k][:])
#import pdb; pdb.set_trace()
# mean at each level
Et[k] = sumt[k] / nslt[k]
E[k] = (sum1[k]) / nslt[k] #+summ[k]
sum2 = 0.
for i in range(len(mus[k])): #loop over processors
sum2 += (mus[k][i] - E[k])**2
V[k] = sum2 / nslt[k]
S[k] = math.sqrt(V[k])
# compute correlation matrix and rearrange models if necessary
ordered = False
while not ordered:
rho = numpy.corrcoef(mus)
ordered = True # check if contradicted
#tarr = rho[0,1:]
for k in range(self.Lmax - 2):
test = rho[0, 1 + k]**2 - rho[0, 2 + k]**2
if test < 0:
ordered = False
tarr = -rho[0, :]**2
if not ordered:
sind = numpy.argsort(tarr)
#import pdb; pdb.set_trace()
self.mord[:] = [self.mord[i] for i in sind]
E[:] = [E[i] for i in sind]
Et[:] = [Et[i] for i in sind]
V[:] = [V[i] for i in sind]
S[:] = [S[i] for i in sind]
mus[:] = [mus[i] for i in sind]
# now compute N1 and a1 using sigma, rho, w, and p
for k in range(self.Lmax):
a1[k] = S[0] * rho[0, k] / S[k]
if k == 0:
r1[k] = 1
elif k == self.Lmax - 1:
work = Et[0] * (rho[0, k]**2)
work /= Et[k] * (1 - rho[0, 1]**2)
r1[k] = math.sqrt(work)
else:
work = Et[0] * (rho[0, k - 1]**2 - rho[0, k]**2)
work /= Et[k] * (1 - rho[0, 1]**2)
r1[k] = math.sqrt(work)
for k in range(self.Lmax):
N1.append(0)
nsf = self.P / numpy.dot(Et, r1)
N1[0] = math.ceil(nsf)
for k in range(self.Lmax):
nsf = N1[0] * r1[k]
N1[k] = math.ceil(nsf)
# limit the number of samples on the last one to pass the sanity check, for debug
sanity = numpy.dot(N1, Et)
if sanity > 1.2 * self.P:
N1n = (self.P - numpy.dot(N1[0:self.Lmax - 2],
Et[0:self.Lmax - 2])) / Et[self.Lmax - 1]
N1[self.Lmax - 1] = math.ceil(N1n)
self.Pr = numpy.dot(N1, Et)
self.N1 = N1
self.a1 = a1
#import pdb; pdb.set_trace()
if rank == 0:
print("MFMC Completed, Samples per level: ", N1)
# Solution Parameters
'nSolutionSteps': 5, # only for nonLinear or steppedLinear
'ksp_its': 25,
'warp_tol': 1e-10, # overall tolerance for nonLinear/steppedLinear
'reduction_factor_for_reform': 0.5,
'useSolutionMonitor': False,
'useKSPMonitor': False,
# Physical parameters
'nu': 0.0,
'e_exp': 1.0,
'skew_exp': 0.0,
'useRotationCorrection': False,
}
mesh = USMesh(options=optMesh)
options.update({
'gridfile': '../inputFiles/naca0012_rans-L2.cgns',
'writevolumesolution': False,
'vis4': .025,
'vis2': 0.5,
'restrictionrelaxation': .5,
'smoother': 'dadi',
'equationtype': 'RANS',
'equationmode': 'unsteady',
'timeIntegrationscheme': 'bdf',
'ntimestepsfine': nfineSteps,
'deltat': dt,
'nsubiterturb': 10,
'nsubiter': 5,
from adflow import ADFLOW
from pygeo import DVGeometry, DVConstraints
from plate_comp_opts import aeroOptions, warpOptions, optOptions
'''Just generate a mesh moved with a set of design variables'''
aoptions = aeroOptions
woptions = warpOptions
ooptions = optOptions
# Generate FFD and DVs
DVGeo = pf.createFFD()
# starting flat mesh
meshname = aoptions['gridFile']
mesh = USMesh(options=warpOptions)
coords = mesh.getSurfaceCoordinates()
DVGeo.addPointSet(coords, "coords")
vars = optOptions['ro_shape']
dvDict = {'pnts': vars}
DVGeo.setDesignVars(dvDict)
new_coords = DVGeo.update("coords")
# move the mesh using idwarp
mesh.setSurfaceCoordinates(new_coords)
mesh.warpMesh()
# Write the new grid file.
mesh.writeGrid(f'opt_result.cgns')
def test3():
# Test the mdo tutorial o mesh
file_name = '../input_files/o_mesh.cgns'
meshOptions = copy.deepcopy(defOpts)
meshOptions.update({'gridFile': file_name, 'fileType': 'cgns'})
# Create warping object
mesh = USMesh(options=meshOptions)
# Extract Surface Coordinates
coords0 = mesh.getSurfaceCoordinates()
vCoords = mesh.getCommonGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of vCoords Inital:')
reg_write(val, 1e-8, 1e-8)
new_coords = coords0.copy()
# Do a shearing sweep deflection:
for i in range(len(coords0)):
span = coords0[i, 2]
new_coords[i, 0] += .05 * span
# Reset the newly computed surface coordiantes
mesh.setSurfaceCoordinates(new_coords)
mesh.warpMesh()
# Get the sum of the warped coordinates
#vCoords = mesh.getSolverGrid()
vCoords = mesh.getWarpGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of vCoords Warped:')
reg_write(val, 1e-8, 1e-8)
# Create a dXv vector to do test the mesh warping with:
dXv_warp = numpy.linspace(0, 1.0, mesh.warp.griddata.warpmeshdof)
if not 'complex' in sys.argv:
if MPI.COMM_WORLD.rank == 0:
print('Computing Warp Deriv')
mesh.warpDeriv(dXv_warp, solverVec=False)
dXs = mesh.getdXs()
val = MPI.COMM_WORLD.reduce(numpy.sum(dXs.flatten()), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of dxs:')
reg_write(val, 1e-8, 1e-8)
else:
# add a complex perturbation on all surface nodes simultaneously:
for i in range(len(coords0)):
new_coords[i, :] += h * 1j
# Reset the newly computed surface coordiantes
mesh.setSurfaceCoordinates(new_coords)
mesh.warpMesh()
vCoords = mesh.getWarpGrid()
deriv = numpy.imag(vCoords) / h
deriv = numpy.dot(dXv_warp, deriv)
val = MPI.COMM_WORLD.reduce(numpy.sum(deriv), op=MPI.SUM)
if MPI.COMM_WORLD.rank == 0:
print('Sum of dxs:')
reg_write(val, 1e-8, 1e-8)
def initialize(self):
# Need to modify this dictionary when we change the SA constants
#import pdb; pdb.set_trace()
#sys.stdout = open(os.devnull, "w")
self.aoptions = aeroOptions
self.woptions = warpOptions
self.ooptions = optOptions
self.uoptions = uqOptions
self.Pr = 0.
self.P = self.uoptions['P']
self.NS0 = self.uoptions['NS0']
# Generate FFD and DVs
if rank == 0:
rank0dvg = pf.createFFD()
else:
rank0dvg = None
self.DVGeo = comm.bcast(rank0dvg, root=0)
# starting flat mesh
meshname = self.aoptions['gridFile']
gridFile = meshname
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach'] #0.95
Re = self.ooptions['Re'] #50000
Re_L = 1.0
temp = 540
arearef = 2.0
chordref = 1.0
# Spalart Allmaras model constants, to be changed in UQ (4 for now)
saconstsm = [0.41, 0.1355, 0.622, 0.66666666667]
self.saconstsb = [7.1, 0.3, 2.0, 1.0, 2.0, 1.2, 0.5, 2.0]
self.saconsts = saconstsm + self.saconstsb
self.aoptions['SAConsts'] = self.saconsts
#self.gridSol = f'{meshname}_{saconstsm}_sol'
solname = self.ooptions['prob_name']
self.gridSol = f'{solname}_sol'
# Get a set of UQ sample points (LHS)
#if self.ooptions['run_once']:
# self.sample = self.uoptions['dist']
#else
# Scatter samples, multi-point parallelism
if self.uoptions['MCTimeBudget']:
self.aps = []
self.solvers = []
self.meshes = []
self.current_samples = self.NS0
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
self.cases = divide_cases(self.NS0, size)
# Scatter samples on each level, multi-point parallelism
self.samplep = self.sample[self.cases[rank]]
self.nsp = len(self.cases[rank])
# Create solvers for the preliminary data
for i in range(self.nsp):
namestr = self.gridSol + "_" + str(self.cases[rank][i])
# create meshes
self.meshes.append(
USMesh(options=self.woptions, comm=MPI.COMM_SELF))
# create aeroproblems
self.aps.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=temp,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
self.solvers.append(
ADFLOW(options=self.aoptions, comm=MPI.COMM_SELF))
saconstsm = self.samplep[i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[i].setOption('SAConsts', self.saconsts)
self.solvers[i].setDVGeo(self.DVGeo)
self.solvers[i].setMesh(self.meshes[i])
print("what up %i", str(rank))
coords = self.solvers[i].getSurfaceCoordinates(
groupName=self.solvers[i].allWallsGroup)
self.solvers[i].DVGeo.addPointSet(coords, 'coords')
# start looping over mesh levels
sumt = 0.
sumtp = 0.
Et = 0.
funcs = {}
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
dvdict = {'pnts': a_init['pnts']}
for i in range(self.nsp):
saconstsm = self.samplep[i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[i].setOption('SAConsts', self.saconsts)
self.solvers[i].DVGeo.setDesignVars(dvdict)
self.aps[i].setDesignVars(dvdict)
pc0 = time.process_time()
self.solvers[i](self.aps[i])
self.solvers[i].evalFunctions(self.aps[i], funcs)
pc1 = time.process_time()
astr = self.gridSol + "_" + str(self.cases[rank][i]) + "_cd"
sumtp += (pc1 - pc0)
sumt = comm.allreduce(sumtp)
Et = sumt / self.NS0
self.NS = math.ceil(self.P / Et)
self.Pr = self.NS * Et
else:
self.NS = self.uoptions['NS']
#import pdb; pdb.set_trace()
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.NS)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
self.cases = divide_cases(self.NS, size)
self.nsp = len(self.cases[rank]) #int(ns/size) # samples per processor
#import pdb; pdb.set_trace()
self.samplep = self.sample[self.cases[
rank]] #self.sample[(rank*self.nsp):(rank*self.nsp+(self.nsp))] #shouldn't really need to "scatter" per se
#import pdb; pdb.set_trace()
#assert len(self.samplep) == self.nsp
# Actually create solvers (and aeroproblems?) (and mesh?) now
self.aps = []
self.solvers = []
self.meshes = []
#self.mesh = USMesh(options=self.woptions, comm=MPI.COMM_SELF)
for i in range(self.nsp):
namestr = self.gridSol + "_" + str(self.cases[rank][i])
# create meshes
self.meshes.append(
USMesh(options=self.woptions, comm=MPI.COMM_SELF))
# create aeroproblems
self.aps.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=temp,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
self.solvers.append(
ADFLOW(options=self.aoptions, comm=MPI.COMM_SELF))
# if not self.ooptions['run_once']:
# saconstsm = self.samplep[i].tolist()
# else:
saconstsm = self.samplep[i].tolist()
self.saconsts = saconstsm + self.saconstsb
self.solvers[i].setOption('SAConsts', self.saconsts)
self.solvers[i].setDVGeo(self.DVGeo)
self.solvers[i].setMesh(self.meshes[i])
print("what up %i", str(rank))
coords = self.solvers[i].getSurfaceCoordinates(
groupName=self.solvers[i].allWallsGroup)
self.solvers[i].DVGeo.addPointSet(coords, 'coords')
# Set constraints, should only need one of those solvers, the meshes are all the same
self.DVCon = DVConstraints()
self.DVCon2 = DVConstraints()
self.DVCon.setDVGeo(self.solvers[0].DVGeo.getFlattenedChildren()[1])
self.DVCon2.setDVGeo(self.solvers[0].DVGeo)
self.DVCon.setSurface(self.solvers[0].getTriangulatedMeshSurface(
groupName='allSurfaces'))
# set extra group for surface area condition
self.DVCon2.setSurface(self.solvers[0].getTriangulatedMeshSurface(),
name='wall')
# DV should be same into page (not doing anything right now)
#import pdb; pdb.set_trace()
lIndex = self.solvers[0].DVGeo.getFlattenedChildren()[1].getLocalIndex(
0)
indSetA = []
indSetB = []
nXc = optOptions['NX']
self.NC = math.trunc(
((1.0 - self.ooptions['DVFraction']) * self.ooptions['NX']))
ind = [
int(nXc / 2) - int(self.NC / 2),
int(nXc / 2) + int(self.NC / 2)
]
for i in range(ind[0], ind[1]):
indSetA.append(lIndex[i, 0, 1])
indSetB.append(lIndex[i, 1, 1])
# for i in range(lIndex.shape[0]):
# indSetA.append(lIndex[i, 0, 1])
# indSetB.append(lIndex[i, 1, 1])
self.DVCon.addLinearConstraintsShape(indSetA,
indSetB,
factorA=1.0,
factorB=-1.0,
lower=0,
upper=0,
name='eqs')
# Thickness constraints (one for each active DV)
#import pdb; pdb.set_trace()
# Maximum thickness of the domain, translates to minimum thickness of bump
ub = 1.0 - self.ooptions['DCMinThick']
tcf = self.ooptions['DCThickFrac']
ra = self.ooptions['bumpBounds']
lim = self.ooptions['DCMinArea']
span = numpy.linspace(0, 1, nXc)
xc = span * (ra[1] - ra[0]) + ra[0]
#ind = range(int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)))
ind = [
int(nXc / 2) - int(tcf * self.NC / 2),
int(nXc / 2) + int(tcf * self.NC / 2)
]
ptList = numpy.zeros([2, 3])
ptList[:, 0] = xc[ind]
ptList[:, 1] = 0.5
ptList[:, 2] = 0.5
if self.ooptions['use_area_con']:
self.DVCon2.addSurfaceAreaConstraint(lower=lim,
upper=10.,
name='sas',
surfaceName='wall')
else:
self.DVCon2.addThicknessConstraints1D(ptList,
self.NC, [0, 0, 1],
lower=0.5,
upper=ub,
name='tcs')
print("excuse me")
dummy = rank
dsum = comm.allgather(dummy)
sys.stdout = sys.__stdout__
def dist_samples(self):
# If we already have the number of samples, just create as many solvers as needed at each level
# Just do this after running MLMC() anyway
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach'] #0.95
Re = self.ooptions['Re'] #50000
Re_L = 1.0
tempR = 540
arearef = 2.0
chordref = 1.0
a_init = self.DVGeo.getValues()
a_init['pnts'][:] = self.ooptions['DVInit']
self.current_samples = sum(self.N1)
if rank == 0:
rank0sam = plate_sa_lhs.genLHS(s=self.current_samples)
else:
rank0sam = None
self.sample = comm.bcast(rank0sam, root=0)
#import pdb; pdb.set_trace()
# Scatter samples on each level, multi-point parallelism
self.cases = []
self.samplep = []
for i in range(self.Lmax):
self.cases.append(divide_cases(self.N1[i], size))
for j in range(len(self.cases[i])):
for k in range(len(self.cases[i][j])):
self.cases[i][j][k] += sum(self.N1[0:i])
#self.nsp.append(len(self.cases[i][rank]))#int(ns/size) # samples per processor
self.samplep.append(self.sample[self.cases[i][rank]])
# Actually create solvers (and aeroproblems?) (and mesh?) now
self.aps = []
self.solvers = []
self.meshes = []
nslp = []
nslt = []
for k in range(self.Lmax):
alist = []
slist = []
mlist = []
nslp.append(len(self.cases[k][rank]))
nslt.append(sum([len(self.cases[k][x]) for x in range(size)]))
for i in range(nslp[k]):
namestr = self.gridSol + "_" + str(self.cases[k][rank][i])
# create meshes
leveloptions = self.woptions
leveloptions['gridFile'] = self.meshnames[self.mord[k]]
mlist.append(USMesh(options=leveloptions, comm=MPI.COMM_SELF))
# create aeroproblems
aloptions = self.aoptions
aloptions['gridFile'] = self.meshnames[self.mord[k]]
alist.append(
AeroProblem(name=namestr,
alpha=alpha,
mach=mach,
reynolds=Re,
reynoldsLength=Re_L,
T=tempR,
areaRef=arearef,
chordRef=chordref,
evalFuncs=['cd']))
time.sleep(0.1) # this solves a few problems for some reason
# create solvers
slist.append(ADFLOW(options=aloptions, comm=MPI.COMM_SELF))
saconstsm = self.samplep[self.Lmax - 1][i].tolist()
self.saconsts = saconstsm + self.saconstsb
slist[i].setOption('SAConsts', self.saconsts)
slist[i].setDVGeo(self.DVGeo)
slist[i].setMesh(mlist[i])
coords = slist[i].getSurfaceCoordinates(
groupName=slist[i].allWallsGroup)
slist[i].DVGeo.addPointSet(coords, 'coords')
self.aps.append(alist)
self.solvers.append(slist)
self.meshes.append(mlist)
# ======================================================================
# rst dvconLeTe (beg)
# Le/Te constraints
DVCon.addLeTeConstraints(0, "iLow")
DVCon.addLeTeConstraints(0, "iHigh")
if comm.rank == 0:
# Only make one processor do this
DVCon.writeTecplot(os.path.join(args.output, "constraints.dat"))
# rst dvconLeTe (end)
# ======================================================================
# Mesh Warping Set-up
# ======================================================================
# rst warp (beg)
meshOptions = {"gridFile": args.gridFile}
mesh = USMesh(options=meshOptions, comm=comm)
CFDSolver.setMesh(mesh)
# rst warp (end)
# ======================================================================
# Functions:
# ======================================================================
# rst funcs (beg)
def cruiseFuncs(x):
if comm.rank == 0:
print(x)
# Set design vars
DVGeo.setDesignVars(x)
ap.setDesignVars(x)
# Run CFD
def eval_warp(handler, test_name, meshOptions, iscomplex):
# --- Create warping object ---
if iscomplex:
# Checking if the complex verision of the code has been built:
try:
from idwarp import idwarp_cs # noqa: F401
h = 1e-40
mesh = USMesh_C(options=meshOptions, debug=True)
except ImportError:
raise unittest.SkipTest(
"Skipping because you do not have complex idwarp compiled")
else:
try:
from idwarp import idwarp # noqa: F401
mesh = USMesh(options=meshOptions)
except ImportError:
raise unittest.SkipTest(
"Skipping because you do not have real idwarp compiled")
# --- Extract Surface Coordinates ---
coords0 = mesh.getSurfaceCoordinates()
vCoords = mesh.getCommonGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
handler.root_add_val(f"{test_name} - Sum of vCoords Inital:",
val,
tol=1e-8)
new_coords = coords0.copy()
# --- Setting the coordinates displacement for surface mesh ---
if test_name == "Test_inflate_cube":
# This specific test displaces the surface in every direction
for i in range(len(coords0)):
new_coords[i, 0] *= 1.1
new_coords[i, 1] *= 1.2
new_coords[i, 2] *= 1.3
else:
# Do a shearing sweep deflection:
for i in range(len(coords0)):
span = coords0[i, 2]
new_coords[i, 0] += 0.05 * span
# --- Reset the newly computed surface coordiantes
mesh.setSurfaceCoordinates(new_coords)
mesh.warpMesh()
# --- Get the sum of the warped coordinates ---
vCoords = mesh.getWarpGrid()
val = MPI.COMM_WORLD.reduce(numpy.sum(vCoords.flatten()), op=MPI.SUM)
handler.root_add_val(f"{test_name} - Sum of vCoords Warped:",
val,
tol=1e-8)
# --- Create a dXv vector to do test the mesh warping with ---
dXv_warp = numpy.linspace(0, 1.0, mesh.warp.griddata.warpmeshdof)
if not iscomplex:
# --- Computing Warp Derivatives ---
mesh.warpDeriv(dXv_warp, solverVec=False)
dXs = mesh.getdXs()
val = MPI.COMM_WORLD.reduce(numpy.sum(dXs.flatten()), op=MPI.SUM)
# --- Verifying Warp Deriv ---
mesh.verifyWarpDeriv(dXv_warp, solverVec=False, dofStart=0, dofEnd=5)
else:
# add a complex perturbation on all surface nodes simultaneously:
for i in range(len(coords0)):
new_coords[i, :] += h * 1j
# Reset the newly computed surface coordiantes
mesh.setSurfaceCoordinates(new_coords)
mesh.warpMesh()
vCoords = mesh.getWarpGrid()
deriv = numpy.imag(vCoords) / h
deriv = numpy.dot(dXv_warp, deriv)
val = MPI.COMM_WORLD.reduce(numpy.sum(deriv), op=MPI.SUM)
handler.root_add_val(f"{test_name} - Sum of dxs:", val, tol=1e-8)
def initialize(self):
# Need to modify this dictionary when we change the SA constants
sys.stdout = open(os.devnull, "w")
self.aoptions = aeroOptions
self.woptions = warpOptions
self.ooptions = optOptions
# Generate FFD and DVs
self.DVGeo = pf.createFFD()
# starting flat mesh
meshname = self.aoptions['gridFile']
gridFile = meshname
# flow characteristics
alpha = 0.0
mach = self.ooptions['mach']#0.95
Re = self.ooptions['Re']#50000
Re_L = 1.0
temp = 540
arearef = 2.0
chordref = 1.0
# Spalart Allmaras model constants, to be changed in UQ
saconstsm = [0.41, 0.1355, 0.622, 0.66666666667, 7.1, 0.3, 2.0]
self.saconsts = saconstsm + [1.0, 2.0, 1.2, 0.5, 2.0]
self.aoptions['SAConsts'] = self.saconsts
#self.gridSol = f'{meshname}_{saconstsm}_sol'
solname = self.ooptions['prob_name']
self.gridSol = f'{solname}_sol'
# Aerodynamic problem description
self.ap = AeroProblem(name=self.gridSol, alpha=alpha, mach=mach, reynolds=Re, reynoldsLength=Re_L, T=temp, areaRef=arearef, chordRef=chordref,
evalFuncs=['cd'])
# Create solver
self.CFDSolver = ADFLOW(options=self.aoptions, comm=MPI.COMM_WORLD)
self.CFDSolver.setDVGeo(self.DVGeo)
# Set up mesh warping
self.mesh = USMesh(options=self.woptions, comm=MPI.COMM_WORLD)
self.CFDSolver.setMesh(self.mesh)
# Try setting the DVGeo coordinates here
coords = self.CFDSolver.getSurfaceCoordinates(groupName=self.CFDSolver.allWallsGroup)
self.CFDSolver.DVGeo.addPointSet(coords, 'coords')
self.CFDSolver.DVGeo.getFlattenedChildren()[1].writePlot3d("ffdp_opt_def.xyz")
# Set constraints
self.DVCon = DVConstraints()
self.DVCon2 = DVConstraints()
self.DVCon.setDVGeo(self.CFDSolver.DVGeo.getFlattenedChildren()[1])
self.DVCon2.setDVGeo(self.CFDSolver.DVGeo)
self.DVCon.setSurface(self.CFDSolver.getTriangulatedMeshSurface(groupName='allSurfaces'))
# set extra group for surface area condition
self.DVCon2.setSurface(self.CFDSolver.getTriangulatedMeshSurface(), name='wall')
# DV should be same into page (not doing anything right now)
#import pdb; pdb.set_trace()
lIndex = self.CFDSolver.DVGeo.getFlattenedChildren()[1].getLocalIndex(0)
indSetA = []
indSetB = []
nXc = optOptions['NX']
self.NC = math.trunc(((1.0 - self.ooptions['DVFraction'])*self.ooptions['NX']))
ind = [int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)]
for i in range(ind[0], ind[1]):
indSetA.append(lIndex[i, 0, 1])
indSetB.append(lIndex[i, 1, 1])
# for i in range(lIndex.shape[0]):
# indSetA.append(lIndex[i, 0, 1])
# indSetB.append(lIndex[i, 1, 1])
self.DVCon.addLinearConstraintsShape(indSetA, indSetB, factorA=1.0, factorB=-1.0, lower=0, upper=0, name='eqs')
# Thickness constraints (one for each active DV)
#import pdb; pdb.set_trace()
# Maximum thickness of the domain, translates to minimum thickness of bump
ub = 1.0 - self.ooptions['DCMinThick']
tcf = self.ooptions['DCThickFrac']
ra = self.ooptions['bumpBounds']
lim = self.ooptions['DCMinArea']
span = numpy.linspace(0, 1, nXc)
xc = span * (ra[1] - ra[0]) + ra[0]
#ind = range(int(nXc/2) - int(self.NC/2), int(nXc/2) + int(self.NC/2)))
ind = [int(nXc/2) - int(tcf*self.NC/2), int(nXc/2) + int(tcf*self.NC/2)]
ptList = numpy.zeros([2, 3])
ptList[:,0] = xc[ind]
ptList[:,1] = 0.5
ptList[:,2] = 0.5
if self.ooptions['use_area_con']:
self.DVCon2.addSurfaceAreaConstraint(lower=lim, upper=10., name='sas', surfaceName='wall')
else:
self.DVCon2.addThicknessConstraints1D(ptList, self.NC, [0,0,1], lower=0.5, upper=ub, name='tcs')
sys.stdout = sys.__stdout__
def regression_test(self, handler):
'''
This is where the actual testing happens.
'''
import copy
from mpi4py import MPI
from baseclasses import AeroProblem
from ... import ADFLOW
from pyspline import Curve
from pygeo import DVGeometry
from idwarp import USMesh
from commonUtils import adjoint_test, adflowDefOpts, IDWarpDefOpts
comm = MPI.COMM_WORLD
gridFile = 'input_files/mdo_tutorial_euler_scalar_jst.cgns'
ffdFile = 'input_files/mdo_tutorial_ffd.fmt'
options = copy.copy(adflowDefOpts)
options.update({
'gridfile':
gridFile,
'restartfile':
gridFile,
'mgcycle':
'2w',
'ncyclescoarse':
250,
'ncycles':
500,
'monitorvariables': ['cpu', 'resrho', 'cl', 'cd', 'cmz', 'totalr'],
'usenksolver':
True,
'l2convergence':
1e-14,
'l2convergencecoarse':
1e-2,
'nkswitchtol':
1e-2,
'adjointl2convergence':
1e-14,
'solutionprecision':
'double',
'gridprecision':
'double',
})
# Setup aeroproblem, cfdsolver, mesh and geometry.
ap = AeroProblem(name='mdo_tutorial',
alpha=1.8,
mach=0.80,
P=20000.0,
T=220.0,
areaRef=45.5,
chordRef=3.25,
beta=0.0,
R=287.87,
xRef=0.0,
yRef=0.0,
zRef=0.0,
evalFuncs=['cl', 'cd'])
# Create the solver
CFDSolver = ADFLOW(options=options, comm=comm, debug=False)
# Create mesh warper
meshOptions = copy.copy(IDWarpDefOpts)
meshOptions.update({'gridFile': gridFile})
mesh = USMesh(options=meshOptions, comm=comm)
CFDSolver.setMesh(mesh)
# Setup geometry/mesh
DVGeo = DVGeometry(ffdFile)
nTwist = 6
DVGeo.addRefAxis(
'wing',
Curve(x=numpy.linspace(5.0 / 4.0, 1.5 / 4.0 + 7.5, nTwist),
y=numpy.zeros(nTwist),
z=numpy.linspace(0, 14, nTwist),
k=2))
def twist(val, geo):
for i in range(nTwist):
geo.rot_z['wing'].coef[i] = val[i]
DVGeo.addGeoDVGlobal('twist', [0] * nTwist,
twist,
lower=-10,
upper=10,
scale=1.0)
DVGeo.addGeoDVLocal('shape',
lower=-0.5,
upper=0.5,
axis='y',
scale=10.0)
CFDSolver.setDVGeo(DVGeo)
# Run adjoint test
adjoint_test(handler, CFDSolver, ap)