def compute_sol(self, stop, monitors):
rhs = modeldisc.fvm(self.eulermodel,
self.mesh50,
self.xsch,
bcL=self.bcL,
bcR=self.bcR)
finit = rhs.fdata_fromprim([1., 0., 1.]) # rho, u, p
solver = tnum.rk4(self.mesh50, rhs)
fsol = solver.solve(finit, self.cfl, stop=stop, monitors=monitors)
return fsol
def test_numscheme():
curmesh = mesh50
endtime = 1
cfl = .5
tnum = rk3ssp
for xnum in [ extrapol1(), extrapol2(), extrapol3(), muscl(minmod), muscl(vanalbada) ]:
finit = field.fdata(mymodel, curmesh, [ init_sinperk(curmesh, k=5) ] )
rhs = modeldisc.fvm(mymodel, curmesh, xnum)
solver = tnum(curmesh, rhs)
solver.solve(finit, cfl, [endtime])
assert 1
def test_wavelength(k):
curmesh = mesh50
endtime = 5
cfl = .8
# extrapol1(), extrapol2()=extrapolk(1), centered=extrapolk(-1), extrapol3=extrapolk(1./3.)
xnum = extrapol1()
# explicit, rk2, rk3ssp, rk4, implicit, trapezoidal=cranknicolson
tnum = explicit
finit = field.fdata(mymodel, curmesh, [ init_sinperk(curmesh, k=k) ] )
rhs = modeldisc.fvm(mymodel, curmesh, xnum)
solver = tnum(curmesh, rhs)
fsol = solver.solve(finit, cfl, [endtime])
assert not fsol[-1].isnan()
def test_integrators(tnum):
curmesh = mesh50
endtime = 1
cfl = .8
# extrapol1(), extrapol2()=extrapolk(1), centered=extrapolk(-1), extrapol3=extrapolk(1./3.)
xnum = extrapol1()
# explicit, rk2, rk3ssp, rk4, implicit, trapezoidal=cranknicolson
finit = field.fdata(mymodel, curmesh, [ init_sinperk(curmesh, k=2) ] )
rhs = modeldisc.fvm(mymodel, curmesh, xnum)
solver = tnum(curmesh, rhs)
fsol = solver.solve(finit, cfl, [endtime])
assert not fsol[-1].isnan()
assert fsol[-1].average('q') < 1.e-12
def test_checkend_maxit_noendtime(self):
endtime = 5.
cfl = .5
maxit = 100
stop_directive = {'maxit': maxit}
finit = field.fdata(self.convmodel, self.curmesh,
[self.init_sinperk(self.curmesh, k=4)])
rhs = modeldisc.fvm(self.convmodel, self.curmesh, self.xsch)
solver = tnum.rk4(self.curmesh, rhs)
fsol = solver.solve(finit, cfl, stop=stop_directive)
assert len(fsol) == 1 # end before expected by tsave
assert not fsol[-1].isnan()
assert solver.nit() == 100
def test_mesh_refined(lratio):
lmesh = mesh.refinedmesh(ncell=50, length=1., ratio=2., nratioa=lratio)
endtime = 5
cfl = 1.
# extrapol1(), extrapol2()=extrapolk(1), centered=extrapolk(-1), extrapol3=extrapolk(1./3.)
xnum = extrapol3()
# explicit, rk2, rk3ssp, rk4, implicit, trapezoidal=cranknicolson
tnum = rk3ssp
finit = field.fdata(mymodel, lmesh, [init_sinperk(lmesh, k=2)])
rhs = modeldisc.fvm(mymodel, lmesh, xnum)
solver = tnum(lmesh, rhs)
fsol = solver.solve(finit, cfl, [endtime])
assert not fsol[-1].isnan()
def test_integrators():
curmesh = mesh50
endtime = 1
cfl = .8
# extrapol1(), extrapol2()=extrapolk(1), centered=extrapolk(-1), extrapol3=extrapolk(1./3.)
xnum = extrapol1()
# explicit, rk2, rk3ssp, rk4, implicit, trapezoidal=cranknicolson
for tnum in [ explicit,rk2, rk3ssp, implicit, cranknicolson ]:
finit = field.fdata(mymodel, curmesh, [ init_sinperk(curmesh, k=2) ] )
rhs = modeldisc.fvm(mymodel, curmesh, xnum)
solver = tnum(curmesh, rhs)
solver.solve(finit, cfl, [endtime])
assert 1
def test_checkend_tottime(self):
endtime = 5.
cfl = .5
stop_directive = {'tottime': endtime}
finit = field.fdata(self.convmodel, self.curmesh,
[self.init_sinperk(self.curmesh, k=4)])
rhs = modeldisc.fvm(self.convmodel, self.curmesh, self.xsch)
solver = tnum.rk4(self.curmesh, rhs)
nsol = 11
tsave = np.linspace(0, 2 * endtime, nsol, endpoint=True)
fsol = solver.solve(finit, cfl, tsave, stop=stop_directive)
assert len(fsol) < nsol # end before expected by tsave
assert not fsol[-1].isnan()
assert fsol[-1].time < 2 * endtime
def test_compression_centered():
endtime = 2.
cfl = .5
xnum = muscl(minmod)
tnum = integ.rk3ssp
thismesh = mesh100
thisprim = [init_step(thismesh, 2, -1.)]
thiscons = field.fdata(mymodel, thismesh, thisprim)
bcL = { 'type': 'dirichlet', 'prim': thisprim[0] }
bcR = { 'type': 'dirichlet', 'prim': thisprim[-1] }
rhs = modeldisc.fvm(mymodel, thismesh, xnum, bcL=bcL, bcR=bcR)
solver = tnum(thismesh, rhs)
solver.solve(thiscons, cfl, [endtime])
assert 1
def test_sin_bcper():
endtime = 2.
cfl = 0.5
xnum = muscl(minmod)
tnum = integ.rk3ssp
thismesh = mesh100
thisprim = [ init_sin(thismesh) ]
thiscons = field.fdata(mymodel, thismesh, thisprim)
bcL = { 'type': 'per' }
bcR = { 'type': 'per' }
rhs = modeldisc.fvm(mymodel, thismesh, xnum, bcL=bcL, bcR=bcR)
solver = tnum(thismesh, rhs)
solver.solve(thiscons, cfl, [endtime])
assert 1
def test_conv_it_perf(self, tmeth):
endtime = 5
cfl = .8
xsch = xnum.extrapol3()
finit = field.fdata(self.convmodel, self.curmesh,
[self.init_sinperk(self.curmesh, k=4)])
rhs = modeldisc.fvm(self.convmodel, self.curmesh, xsch)
solver = tmeth(self.curmesh, rhs)
fsol = solver.solve(finit, cfl, [endtime])
assert solver.nit() > 300
assert solver.nit() < 400
maxperf = 40. if tmeth in tnum.List_Explicit_Integrators else 100.
assert solver.perf_micros() < maxperf
assert not fsol[-1].isnan()
def test_acousticpacket_sym(flux):
endtime = 2.
cfl = 0.6
xnum = muscl(minmod)
tnum = integ.rk3ssp
meshsim = mesh100
xc = meshsim.centers()
bcL = {'type': 'sym'}
bcR = {'type': 'sym'}
rhs = modeldisc.fvm(model, meshsim, xnum, numflux=flux, bcL=bcL, bcR=bcR)
finit = rhs.fdata(model.prim2cons([frho(xc), fu(xc), fp(xc)])) # rho, u, p
solver = tnum(meshsim, rhs)
fsol = solver.solve(finit, cfl, [endtime])
assert not fsol[-1].isnan()
def test_sin_bcper(self):
endtime = 2.
cfl = 0.5
xnum = muscl(minmod)
tnum = integ.rk3ssp
thismesh = self.mesh100
thisprim = [ self.init_sin(thismesh) ]
thiscons = field.fdata(self.mymodel, thismesh, thisprim)
bcL = { 'type': 'per' }
bcR = { 'type': 'per' }
rhs = modeldisc.fvm(self.mymodel, thismesh, xnum, bcL=bcL, bcR=bcR)
solver = tnum(thismesh, rhs)
fsol = solver.solve(thiscons, cfl, [endtime])
assert not fsol[-1].isnan()
def test_expansion(self):
endtime = 2.
cfl = 0.5
xnum = muscl(minmod)
tnum = integ.rk3ssp
thismesh = self.mesh100
thisprim = [self.init_step(thismesh, 1., 2.)]
thiscons = field.fdata(self.mymodel, thismesh, thisprim)
bcL = { 'type': 'dirichlet', 'prim': thisprim[0] }
bcR = { 'type': 'dirichlet', 'prim': thisprim[-1] }
rhs = modeldisc.fvm(self.mymodel, thismesh, xnum, bcL=bcL, bcR=bcR)
solver = tnum(thismesh, rhs)
fsol = solver.solve(thiscons, cfl, [endtime])
assert not fsol[-1].isnan()
def test_muscl_limiters(self, limiter):
curmesh = self.mesh50
endtime = 5
cfl = .8
# extrapol1(), extrapol2()=extrapolk(1), centered=extrapolk(-1), extrapol3=extrapolk(1./3.)
xnum = muscl(limiter)
finit = field.fdata(self.mymodel, curmesh,
[self.init_sinperk(curmesh, k=4)])
rhs = modeldisc.fvm(self.mymodel, curmesh, xnum)
solver = rk3ssp(curmesh, rhs)
fsol = solver.solve(finit, cfl, [endtime])
assert not fsol[-1].isnan()
avg, var = fsol[-1].stats('q')
#varref = { }
assert avg == pytest.approx(0., abs=1.e-12)
def test_rayleigh(self):
endtime = 100.
cfl = 1.2
xnum = muscl(minmod)
tnum = integ.rk4
meshsim = self.mesh20
modelrayleigh = euler.model(source=[None, None, lambda x, q: 2.])
bcL = {'type': 'insub', 'ptot': 1.4, 'rttot': 1.}
bcR = {'type': 'outsub', 'p': 1.}
rhs = modeldisc.fvm(modelrayleigh, meshsim, xnum, bcL=bcL, bcR=bcR)
finit = rhs.fdata_fromprim([1., 0., 1.]) # rho, u, p
solver = tnum(meshsim, rhs)
fsol = solver.solve(finit, cfl, [endtime])
assert not fsol[-1].isnan()
avg, var = fsol[-1].stats('rttot')
assert avg == pytest.approx(1.6139, rel=1.e-4)
assert var == pytest.approx(0.1242, rel=1.e-2)
def test_interpol_t(self):
endtime = 1. / self.curmesh.ncell
cfl = 5. # unstable but no risk with 1 it
maxit = 1
stop_directive = {'maxit': maxit}
finit = field.fdata(self.convmodel, self.curmesh,
[self.init_sinperk(self.curmesh, k=4)])
rhs = modeldisc.fvm(self.convmodel, self.curmesh, self.xsch)
solver = tnum.explicit(self.curmesh, rhs)
fsol2 = solver.solve(finit, cfl, [2 * endtime], stop=stop_directive)
fsol1 = solver.solve(finit, cfl, [endtime], stop=stop_directive)
assert not fsol2[-1].isnan()
assert 2 * fsol1[-1].time == pytest.approx(fsol2[-1].time, abs=1.e-12)
fi = finit.interpol_t(fsol2[-1], endtime)
diff = fi.diff(fsol1[-1])
for d in diff.data:
assert np.average(np.abs(d)) == pytest.approx(0., abs=1.e-6)
def test_flow_sub(self, bcin, bcout):
endtime = 100.
cfl = 1.2
xnum = muscl(minmod)
tnum = integ.rk4
meshsim = self.mesh20
bcL = {'type': bcin, 'ptot': 1.4, 'rttot': 1.}
bcR = {'type': bcout, 'p': 1.}
rhs = modeldisc.fvm(self.model, meshsim, xnum, bcL=bcL, bcR=bcR)
finit = rhs.fdata_fromprim([1., 0., 1.]) # rho, u, p
solver = tnum(meshsim, rhs)
fsol = solver.solve(finit, cfl, [endtime])
assert not fsol[-1].isnan()
mach_th = np.sqrt(((bcL['ptot'] / bcR['p'])**(1. / 3.5) - 1.) / .2)
error = np.sqrt(
np.sum((fsol[-1].phydata('mach') - mach_th)**2) /
meshsim.ncell) / mach_th
assert error < 1.e-8
def test_shocktube_sodsup(flux):
model = euler.model()
sod = solR.Sod_supersonic(model) # sol.Sod_supersonic(model) #
bcL = { 'type': 'dirichlet', 'prim': sod.bcL() }
bcR = { 'type': 'dirichlet', 'prim': sod.bcR() }
xnum = muscl(minmod) #
rhs = modeldisc.fvm(model, meshref, xnum, numflux=flux, bcL=bcL, bcR=bcR)
solver = integ.rk3ssp(meshref, rhs)
# computation
#
endtime = 2.
cfl = 1.
finit = sod.fdata(meshref)
fsol = solver.solve(finit, cfl, [endtime])
fref = sod.fdata(meshref, endtime)
#
for name in ['density', 'pressure', 'mach']:
error = np.sqrt(np.sum((fsol[-1].phydata(name)-fref.phydata(name))**2))/np.sum(np.abs(fref.phydata(name)))
assert error < 5.e-3
def test_sym_flux(flux):
endtime = 1.
cfl = 0.6
xnum = muscl(minmod)
tnum = integ.rk3ssp
meshsim = mesh.unimesh(ncell=100, length=1.)
xc = meshsim.centers()
bcL = { 'type': 'sym'}
bcR = { 'type': 'sym'}
model = shw.shallowwater1d()
model10 = shw.shallowwater1d(g=10.)
rhs = modeldisc.fvm(model, meshsim, xnum, numflux=flux, bcL=bcL, bcR=bcR)
finit = rhs.fdata(model.prim2cons(waterdrop(xc, .01))) # rho, u, p
solver = tnum(meshsim, rhs)
fsol = solver.solve(finit, cfl, [endtime])
assert not fsol[-1].isnan()
avg, var = fsol[-1].stats('height')
assert avg == pytest.approx(0.098232, rel=1.e-4)
assert var >= 6.5e-6
def test_interpolation_regression(self):
endtime = 5
cfl = .5
finit = field.fdata(self.convmodel, self.curmesh,
[self.init_sinperk(self.curmesh, k=4)])
rhs = modeldisc.fvm(self.convmodel, self.curmesh, self.xsch)
solver = tnum.rk4(self.curmesh, rhs)
nsol = 5
tsave = np.linspace(0, endtime, nsol, endpoint=True)
fsol = solver.solve(finit, cfl, tsave)
fleg = solver.solve_legacy(finit, cfl, tsave)
assert len(fsol) == nsol
assert len(fleg) == nsol
for fs, fl in zip(fsol, fleg):
assert not fs.isnan()
diff = fs.diff(fl)
assert diff.time == pytest.approx(0., abs=1.e-12)
for d in diff.data:
assert np.average(np.abs(d)) == pytest.approx(0., abs=1.e-6)
def test_frequency(self, montype):
endtime = 5.
cfl = .5
finit = field.fdata(self.convmodel, self.mesh50,
[self.init_sinperk(self.mesh50, k=4)])
rhs = modeldisc.fvm(self.convmodel, self.mesh50, self.xsch)
maxit = 500
stop_directive = {'maxit': maxit}
solver = tnum.rk4(self.mesh50, rhs)
mondict = {}
for f in 1, 2, 10, 50, 100:
monitors = {montype: {'frequency': f}}
fsol = solver.solve(finit,
cfl, [endtime],
stop=stop_directive,
monitors=monitors)
mondict[f] = monitors[montype]['output']
assert not fsol[-1].isnan()
assert mondict[f]._it[-1] == maxit
assert (len(mondict[f]._it) - 1) * f == maxit
def test_restart(self):
tottime = 10.
breaktime = 5.
cfl = .5
finit = field.fdata(self.convmodel, self.curmesh,
[self.init_sinperk(self.curmesh, k=4)])
rhs = modeldisc.fvm(self.convmodel, self.curmesh, self.xsch)
solver = tnum.rk4(self.curmesh, rhs)
nsol = 10 + 1 # every second
tsave = np.linspace(0, tottime, nsol, endpoint=True)
#
stop_directive = {'tottime': breaktime}
fsol0 = solver.solve(finit, cfl, tsave, stop=stop_directive)
assert len(fsol0) == 6 # end before expected by tsave
assert not fsol0[-1].isnan()
assert fsol0[-1].time == breaktime
#
fsol = solver.restart(fsol0[-1], cfl, tsave)
assert len(fsol) == 6 # only last snapshots ; time 5. is saved again
assert not fsol[-1].isnan()
assert fsol[-1].time == tottime
def test_acousticpacket_bcout(self, bcout):
endtime = 2.
cfl = 0.6
xnum = muscl(minmod)
tnum = integ.rk3ssp
meshsim = self.mesh100
xc = meshsim.centers()
bcL = {'type': 'sym'}
bcR = {'type': bcout, 'p': 1.} # 'p' will be ignored if unused
rhs = modeldisc.fvm(self.model,
meshsim,
xnum,
numflux='hllc',
bcL=bcL,
bcR=bcR)
finit = rhs.fdata(
self.model.prim2cons([self.frho(xc),
self.fu(xc),
self.fp(xc)])) # rho, u, p
solver = tnum(meshsim, rhs)
fsol = solver.solve(finit, cfl, [endtime])
assert not fsol[-1].isnan()
def test_nozzle(NPR):
def S(x): # section law, throat is at x=5
return 1. - .5 * np.exp(-.5 * (x - 5.)**2)
model = euler.nozzle(sectionlaw=S)
meshsim = mesh.unimesh(ncell=50, length=10.)
nozz = solN.nozzle(model, S(meshsim.centers()), NPR=NPR)
fref = nozz.fdata(meshsim)
# BC
bcL = {'type': 'insub', 'ptot': NPR, 'rttot': 1.}
bcR = {'type': 'outsub', 'p': 1.}
#
rhs = modeldisc.fvm(model, meshsim, muscl(vanleer), bcL=bcL, bcR=bcR)
solver = integ.rk3ssp(meshsim, rhs)
# computation
endtime = 100.
cfl = .8
finit = rhs.fdata_fromprim([1., 0.1, 1.]) # rho, u, p
fsol = solver.solve(finit, cfl, [endtime])
# error
error = np.sqrt(
np.sum((fsol[-1].phydata('mach') - fref.phydata('mach'))**2)) / np.sum(
np.abs(fref.phydata('mach')))
assert error < 5.e-2
def test_variables(self):
bcL = {'type': 'insub', 'ptot': 1.4, 'rttot': 1.}
bcR = {'type': 'outsub', 'p': 1.}
meshsim = self.mesh100
rhs = modeldisc.fvm(self.model, meshsim, extrapol1(), bcL=bcL, bcR=bcR)
xc = meshsim.centers()
finit = rhs.fdata_fromprim([self.frho(xc),
self.fu(xc),
self.fp(xc)]) # rho, u, p
data = finit.phydata('asound') * finit.phydata('mach') - finit.phydata(
'velocity')
error = np.sum(np.abs(data))
assert error < 1.e-12
data = finit.phydata('velocity') * finit.phydata(
'density') - finit.phydata('massflow')
error = np.sum(np.abs(data))
assert error < 1.e-12
data = finit.phydata('htot') - finit.phydata(
'enthalpy') - finit.phydata('kinetic-energy') - finit.phydata(
'massflow')
error = np.sum(np.abs(data))
# entropy should be constant (variance = 0)
__, error = finit.stats('entropy')
assert error < 1.e-12
def init_rupturebarrage(mesh):
h0_vect = np.zeros(len(mesh.centers())) + 0.5
for i in range(len(mesh.centers())):
if mesh.centers()[i] < 1:
h0_vect[i] = 1
return h0_vect
#h0_vect = init_rupturebarrage(mesh)
u0_vect = .5 + np.zeros((ncell))
w_init = [h0_vect, u0_vect * h0_vect]
# Define RHS
rhs = modeldisc.fvm(model, mesh, xmeth, numflux=numflux, bcL=bcL, bcR=bcR)
field0 = rhs.fdata_fromprim(w_init)
# Define the solver
solver = tmeth(mesh, rhs)
# Solution
w_sol = solver.solve(field0, cfl, tsave)
# VERIFIED : w_sol contains solutions in conservative variables [h,q=h*u]
solver.show_perf()
fig2, (ax1, ax2) = plt.subplots(1, 2, figsize=(15, 7))
ax1.set_xlabel('$x$'), ax1.set_ylabel('$h(t,x)$'), ax1.set_title(
'Hauteur de fluide au temps t = ' + str(endtime) + '\n (CFL ' + str(cfl) +
', flux : ' + numflux + ', ' + xmethstr + ', ' + tmethstr + ')')
ax1.set(xlim=(-0.1, mesh.centers()[-1] + 0.1), ylim=(-0.0, .2))
ax1.grid(linestyle='--', color='0.5')
line1, = ax1.plot(mesh.centers(), w_sol[-1].data[0])
import flowdyn.integration as integ
#meshsim = mesh.unimesh(ncell=200, length=10., x0=-4.)
#meshref = mesh.unimesh(ncell=1000, length=10., x0=-4.)
@pytest.mark.parametrize("case, endtime", [(solR.Sod_subsonic, 2.8),
(solR.Sod_supersonic, 2.)])
def test_shocktube(case, endtime):
meshsim = mesh.unimesh(ncell=200, length=10., x0=-4.)
model = euler.euler1d()
sod = case(model) # sol.Sod_supersonic(model) #
bcL = {'type': 'dirichlet', 'prim': sod.bcL()}
bcR = {'type': 'dirichlet', 'prim': sod.bcR()}
xnum = muscl(minmod) #
rhs = modeldisc.fvm(model, meshsim, xnum, numflux='hllc', bcL=bcL, bcR=bcR)
solver = integ.rk3ssp(meshsim, rhs)
# computation
#
cfl = 1.
finit = sod.fdata(meshsim)
fsol = solver.solve(finit, cfl, [endtime])
fref = sod.fdata(meshsim, endtime)
#
for name in ['density', 'pressure', 'mach']:
error = np.sqrt(
np.sum((fsol[-1].phydata(name) - fref.phydata(name))**2)) / np.sum(
np.abs(fref.phydata(name)))
assert error < 1.e-2
import flowdyn.modeldisc as modeldisc
import flowdyn.solution.euler_riemann as sol
meshsim = unimesh(ncell=200, length=10., x0=-4.)
meshref = unimesh(ncell=1000, length=10., x0=-4.)
model1 = euler.model()
model2 = euler.model()
sod = sol.Sod_subsonic(model1) # sol.Sod_supersonic(model1) #
bcL = { 'type': 'dirichlet', 'prim': sod.bcL() }
bcR = { 'type': 'dirichlet', 'prim': sod.bcR() }
xnum1 = muscl(minmod) #
xnum2 = muscl(vanalbada) #
rhs1 = modeldisc.fvm(model1, meshsim, xnum1, numflux='hlle', bcL=bcL, bcR=bcR)
solver1 = tnum.rk3ssp(meshsim, rhs1)
rhs2 = modeldisc.fvm(model2, meshsim, xnum2, numflux='hlle', bcL=bcL, bcR=bcR)
solver2 = tnum.rk3ssp(meshsim, rhs2)
# computation
#
endtime = 2.8 # 2.8 for subsonic, 2.8 for supersonic
cfl = 1.
finit = sod.fdata(meshsim)
fsol1 = solver1.solve(finit, cfl, [endtime])
solver1.show_perf()
fsol2 = solver2.solve(finit, cfl, [endtime])
solver2.show_perf()
#from flowdyn.field import *
from flowdyn.xnum import *
import flowdyn.integration as tnum
import flowdyn.modelphy.euler as euler
import flowdyn.modeldisc as modeldisc
#import flowdyn.solution.euler_riemann as sol
nx = 50
meshsim = unimesh(ncell=nx, length=10.)
model = euler.model()
bcL = {'type': 'insub', 'ptot': 1.4, 'rttot': 1.}
bcR = {'type': 'outsub', 'p': 1.}
rhs = modeldisc.fvm(model, meshsim, muscl(minmod), bcL=bcL, bcR=bcR)
solver1 = tnum.rk3ssp(meshsim, rhs)
solver2 = tnum.gear(meshsim, rhs)
# computation
#
endtime = 100.
cfl1 = .8
cfl2 = 20.
finit = rhs.fdata_fromprim([1., 0.1, 1.]) # rho, u, p
fsol1 = solver1.solve(finit, cfl1, [endtime])
solver1.show_perf()
