def get_N_form(self):
try:
return self.N_form
except AttributeError:
pass
# Set up magnetic field and equivalent electric current forms
H_r = -curl(self.E_i)/(self.k0*Z0)
H_i = curl(self.E_r)/(self.k0*Z0)
J_r = cross(self.n, H_r)
J_i = cross(self.n, H_i)
#------------------------------
# Set up form for far field potential N
theta_hat = self.theta_hat
phi_hat = self.phi_hat
phase = self.phase
N_r = J_r*dolfin.cos(phase) - J_i*dolfin.sin(phase)
N_i = J_r*dolfin.sin(phase) + J_i*dolfin.cos(phase)
# UFL does not seem to like vector valued functionals, so we split the
# final functional from into theta and phi components
self.N_form = dict(
r_theta=dot(theta_hat, N_r)*ds,
r_phi=dot(phi_hat, N_r)*ds,
i_theta=dot(theta_hat, N_i)*ds,
i_phi=dot(phi_hat, N_i)*ds)
return self.N_form
def neumann_linear_form(self, V, neumann_boundary, g, L=None):
"""Return or add up the linear form L(v) coming from the Neumann boundary"""
v = dolfin.TrialFunction(V)
for g_j, ds_j in self.neumann_form_list(neumann_boundary, g, V.mesh()):
if L is None:
L = dot(g_j, v) * ds_j
else:
L += dot(g_j, v) * ds_j
return L
def force(self, state, turbine_field):
""" Computes the force field over turbine field
:param state: Current solution state.
:type state: UFL
:param turbine_field: Turbine friction field
:type turbine_field: UFL
"""
return self.rho * turbine_field * dot(state[0], state[0]) + dot(state[1], state[1])
def power(self, state, turbine_field):
""" Computes the power field over the domain.
:param state: Current solution state.
:type state: UFL
:param turbine_field: Turbine friction field
:type turbine_field: UFL
"""
return (self.rho * turbine_field * (dot(state[0], state[0]) +
dot(state[1], state[1])) ** 1.5)
def _speed_squared(self, state):
""" The velocity speed with turbine cut in and out speed limits """
speed_sq = dot(state[0], state[0]) + dot(state[1], state[1])
if self._cut_in_speed is not None:
speed_sq *= conditional(speed_sq < self._cut_in_speed**2, self._eps, 1)
if self._cut_out_speed is not None:
speed_sq = conditional(speed_sq > self._cut_out_speed**2,
self._cut_out_speed**2, speed_sq)
return speed_sq
def weak_F(t, u_t, u, v):
# Define the differential equation.
mesh = v.function_space().mesh()
n = FacetNormal(mesh)
r = Expression('x[0]', degree=1, cell=triangle)
# All time-dependent components be set to t.
f.t = t
b.t = t
kappa.t = t
F = - inner(b, grad(u)) * v * dx \
- 1.0 / (rho * cp) * dot(r * kappa * grad(u), grad(v / r)) * dx \
+ 1.0 / (rho * cp) * dot(r * kappa * grad(u), n) * v / r * ds \
+ 1.0 / (rho * cp) * f * v * dx
return F
def flux_derivative(self, u, coeff):
a = coeff
Du = self.differential_op(u)
Dsigma = dot(nabla_grad(a), Du)
if element_degree(u) >= 2:
Dsigma += a * div(Du)
return Dsigma
def get_stiffness_form(self):
"""Get 'stiffness' / curl . curl matrix form"""
u = self.trial_function
v = self.test_function
mu_r = self.material_functions['mu_r']
s = dot(curl(v), curl(u))/mu_r*dx
return s
def test_pointsource_vector_fs(mesh, point):
"""Tests point source when given constructor PointSource(V, point,
mag) with a vector for a vector function space that isn't placed
at a node for 1D, 2D and 3D. Global points given to constructor
from rank 0 processor.
"""
rank = MPI.rank(mesh.mpi_comm())
V = VectorFunctionSpace(mesh, "CG", 1)
v = TestFunction(V)
b = assemble(dot(Constant([0.0]*mesh.geometry().dim()), v)*dx)
if rank == 0:
ps = PointSource(V, point, 10.0)
else:
ps = PointSource(V, [])
ps.apply(b)
# Checks array sums to correct value
b_sum = b.sum()
assert round(b_sum - 10.0*V.num_sub_spaces()) == 0
# Checks point source is added to correct part of the array
v2d = vertex_to_dof_map(V)
for v in vertices(mesh):
if near(v.midpoint().distance(point), 0.0):
for spc_idx in range(V.num_sub_spaces()):
ind = v2d[v.index()*V.num_sub_spaces() + spc_idx]
if ind < len(b.get_local()):
assert np.round(b.get_local()[ind] - 10.0) == 0
def __init__(self, ui, time_step_method, rho, mu, u, p0, dt, bcs, f, my_dx):
super(TentativeVelocityProblem, self).__init__()
W = ui.function_space()
v = TestFunction(W)
self.bcs = bcs
r = SpatialCoordinate(ui.function_space().mesh())[0]
def me(uu, ff):
return _momentum_equation(uu, v, p0, ff, rho, mu, my_dx)
self.F0 = rho * dot(ui - u[0], v) / dt * 2 * pi * r * my_dx
if time_step_method == "forward euler":
self.F0 += me(u[0], f[0])
elif time_step_method == "backward euler":
self.F0 += me(ui, f[1])
else:
assert (
time_step_method == "crank-nicolson"
), "Unknown time stepper '{}'".format(
time_step_method
)
self.F0 += 0.5 * (me(u[0], f[0]) + me(ui, f[1]))
self.jacobian = derivative(self.F0, ui)
self.reset_sparsity = True
return
def test_multi_ps_matrix(mesh):
"""Tests point source PointSource(V, source) for mulitple point
sources applied to a matrix for 1D, 2D and 3D. Global points given
to constructor from rank 0 processor.
"""
c_ids = [0, 1, 2]
rank = MPI.rank(mesh.mpi_comm())
V = VectorFunctionSpace(mesh, "CG", 1, dim=2)
u, v = TrialFunction(V), TestFunction(V)
A = assemble(Constant(0.0)*dot(u, v)*dx)
source = []
if rank == 0:
for c_id in c_ids:
cell = Cell(mesh, c_id)
point = cell.midpoint()
source.append((point, 10.0))
ps = PointSource(V, source)
ps.apply(A)
# Checks b sums to correct value
a_sum = MPI.sum(mesh.mpi_comm(), np.sum(A.array()))
assert round(a_sum - 2*len(c_ids)*10) == 0
def test_pointsource_mixed_space(mesh, point):
"""Tests point source when given constructor PointSource(V, point,
mag) with a vector for a mixed function space that isn't placed at
a node for 1D, 2D and 3D. Global points given to constructor from
rank 0 processor.
"""
rank = MPI.rank(mesh.mpi_comm())
ele1 = FiniteElement("CG", mesh.ufl_cell(), 1)
ele2 = FiniteElement("DG", mesh.ufl_cell(), 2)
ele3 = VectorElement("CG", mesh.ufl_cell(), 2)
V = FunctionSpace(mesh, MixedElement([ele1, ele2, ele3]))
value_dimension = V.element().value_dimension(0)
v = TestFunction(V)
b = assemble(dot(Constant([0.0]*value_dimension), v)*dx)
if rank == 0:
ps = PointSource(V, point, 10.0)
else:
ps = PointSource(V, [])
ps.apply(b)
# Checks array sums to correct value
b_sum = b.sum()
assert round(b_sum - 10.0*value_dimension) == 0
def divergence_matrix(mesh):
CR = VectorFunctionSpace(mesh, 'CR', 1)
DG = FunctionSpace(mesh, 'DG', 0)
A = cg1_cr_interpolation_matrix(mesh)
M = assemble(dot(div(TrialFunction(CR)), TestFunction(DG))*dx())
C = compiled_cr_module.cr_divergence_matrix(M, A, DG, CR)
return C
def les_update(nut_, nut_form, A_mass, At, u_, dt, bc_ksgs, bt, ksgs_sol,
KineticEnergySGS, CG1, ksgs, delta, **NS_namespace):
p, q = TrialFunction(CG1), TestFunction(CG1)
Ck = KineticEnergySGS["Ck"]
Ce = KineticEnergySGS["Ce"]
Sij = sym(grad(u_))
assemble(dt*inner(dot(u_, 0.5*grad(p)), q)*dx
+ inner((dt*Ce*sqrt(ksgs)/delta)*0.5*p, q)*dx
+ inner(dt*Ck*sqrt(ksgs)*delta*grad(0.5*p), grad(q))*dx, tensor=At)
assemble(dt*2*Ck*delta*sqrt(ksgs)*inner(Sij,grad(u_))*q*dx, tensor=bt)
bt.axpy(1.0, A_mass*ksgs.vector())
bt.axpy(-1.0, At*ksgs.vector())
At.axpy(1.0, A_mass, True)
# Solve for ksgs
bc_ksgs.apply(At, bt)
ksgs_sol.solve(At, ksgs.vector(), bt)
ksgs.vector().set_local(ksgs.vector().array().clip(min=1e-7))
ksgs.vector().apply("insert")
# Update nut_
nut_()
def __init__(self, V, u, v, b,
kappa, rho, cp,
source,
dirichlet_bcs=[],
neumann_bcs={},
robin_bcs={},
dx=dx,
ds=ds
):
super(HeatCylindrical, self).__init__()
self.dirichlet_bcs = dirichlet_bcs
r = Expression('x[0]', degree=1, domain=V.mesh())
self.V = V
self.dx_multiplier = 2*pi*r
self.F0 = kappa * r * dot(grad(u), grad(v / (rho * cp))) \
* 2*pi * dx
#F -= dot(b, grad(u)) * v * 2*pi*r * dx_workpiece(0)
if b:
self.F0 += (b[0] * u.dx(0) + b[1] * u.dx(1)) * v * 2*pi*r * dx
# Joule heat
self.F0 -= 1.0 / (rho * cp) * source * v * 2*pi*r * dx
# Neumann boundary conditions
for k, nGradT in neumann_bcs.iteritems():
self.F0 -= r * kappa * nGradT * v / (rho * cp) \
* 2 * pi * ds(k)
# Robin boundary conditions
for k, value in robin_bcs.iteritems():
alpha, u0 = value
self.F0 -= r * kappa * alpha * (u - u0) * v / (rho * cp) \
* 2 * pi * ds(k)
return
def compute_velocity_correction(
ui, p0, p1, u_bcs, rho, mu, dt, rotational_form, my_dx, tol, verbose
):
"""Compute the velocity correction according to
.. math::
U = u_0 - \\frac{dt}{\\rho} \\nabla (p_1-p_0).
"""
W = ui.function_space()
P = p1.function_space()
u = TrialFunction(W)
v = TestFunction(W)
a3 = dot(u, v) * my_dx
phi = Function(P)
phi.assign(p1)
if p0:
phi -= p0
if rotational_form:
r = SpatialCoordinate(W.mesh())[0]
div_ui = 1 / r * (r * ui[0]).dx(0) + ui[1].dx(1)
phi += mu * div_ui
L3 = dot(ui, v) * my_dx - dt / rho * (phi.dx(0) * v[0] + phi.dx(1) * v[1]) * my_dx
u1 = Function(W)
solve(
a3 == L3,
u1,
bcs=u_bcs,
solver_parameters={
"linear_solver": "iterative",
"symmetric": True,
"preconditioner": "hypre_amg",
"krylov_solver": {
"relative_tolerance": tol,
"absolute_tolerance": 0.0,
"maximum_iterations": 100,
"monitor_convergence": verbose,
},
},
)
# u = project(ui - k/rho * grad(phi), V)
# div_u = 1/r * div(r*u)
r = SpatialCoordinate(W.mesh())[0]
div_u1 = 1.0 / r * (r * u1[0]).dx(0) + u1[1].dx(1)
info("||u||_div = {:e}".format(sqrt(assemble(div_u1 * div_u1 * my_dx))))
return u1
def weak_F(t, u_t, u, v):
# All time-dependent components be set to t.
u0.t = t
f.t = f
F = - 1.0 / (rho * cp) * kappa * dot(grad(u), grad(v)) * dx \
+ 1.0 / (rho * cp) * kappa * (u*u*u*u - u0*u0*u0*u0) * v * ds \
+ 1.0 / (rho * cp) * f * v * dx
return F
def _get_form(self):
n = self.function_space.cell().n
k0 = self.k0
E_i = self.E_i
E_r = self.E_r
mu_r = self._get_mur_function()
return (1/k0/Z0)*dolfin.dot(n, (dolfin.cross(E_r, -dolfin.curl(E_i)/mu_r) +
dolfin.cross(E_i, dolfin.curl(E_r)/mu_r)))*dolfin.ds
def __init__(self, ui, theta,
rho, mu,
u, p0, dt,
bcs,
f0, f1,
stabilization=False,
dx=dx
):
super(TentativeVelocityProblem, self).__init__()
W = ui.function_space()
v = TestFunction(W)
self.bcs = bcs
r = Expression('x[0]', degree=1, domain=ui.function_space().mesh())
#self.F0 = rho * dot(3*ui - 4*u[-1] + u[-2], v) / (2*Constant(dt)) \
# * 2*pi*r*dx
#self.F0 += momentum_equation(ui, v,
# p0,
# f1,
# rho, mu,
# stabilization=stabilization,
# dx=dx
# )
self.F0 = rho * dot(ui - u[-1], v) / Constant(dt) \
* 2*pi*r*dx
if abs(theta) > DOLFIN_EPS:
# Implicit terms.
if f1 is None:
raise RuntimeError('Implicit schemes need right-hand side '
'at target step (f1).')
self.F0 += theta \
* momentum_equation(ui, v,
p0,
f1,
rho, mu,
stabilization=stabilization,
dx=dx
)
if abs(1.0 - theta) > DOLFIN_EPS:
# Explicit terms.
if f0 is None:
raise RuntimeError('Explicit schemes need right-hand side '
'at current step (f0).')
self.F0 += (1.0 - theta) \
* momentum_equation(u[-1], v,
p0,
f0,
rho, mu,
stabilization=stabilization,
dx=dx
)
self.jacobian = derivative(self.F0, ui)
self.reset_sparsity = True
return
def _build_residuals(V, dx, phi, omega, Mu, Sigma, convections, voltages):
#class OuterBoundary(SubDomain):
# def inside(self, x, on_boundary):
# return on_boundary and abs(x[0]) > DOLFIN_EPS
#boundaries = FacetFunction('size_t', mesh)
#boundaries.set_all(0)
#outer_boundary = OuterBoundary()
#outer_boundary.mark(boundaries, 1)
#ds = Measure('ds')[boundaries]
r = Expression('x[0]', degree=1, domain=V.mesh())
subdomain_indices = Mu.keys()
#u = TrialFunction(V)
v = TestFunction(V)
r_r = zero() * dx(0)
for i in subdomain_indices:
r_r += 1.0 / (Mu[i] * r) * dot(grad(r * phi[0]), grad(r * v)) * 2 * pi * dx(i) \
- omega * Sigma[i] * phi[1] * v * 2 * pi * r * dx(i)
# convections
for i, conv in convections.items():
r_r += dot(conv, grad(r * phi[0])) * v * 2 * pi * dx(i)
# rhs
for i, voltage in voltages.items():
r_r -= Sigma[i] * voltage.real * v * dx(i)
## boundaries
#r_r += 1.0/Mu[i] * phi[0] * v * 2*pi*ds(1)
# imaginary part
r_i = zero() * dx(0)
for i in subdomain_indices:
r_i += 1.0 / (Mu[i] * r) * dot(grad(r * phi[1]), grad(r * v)) * 2 * pi * dx(i) \
+ omega * Sigma[i] * phi[0] * v * 2 * pi * r * dx(i)
# convections
for i, conv in convections.items():
r_i += dot(conv, grad(r * phi[1])) * v * 2 * pi * dx(i)
# rhs
for i, voltage in voltages.items():
r_r -= Sigma[i] * voltage.imag * v * dx(i)
## boundaries
#r_i += 1.0/Mu[i] * phi[1] * v * 2*pi*ds(1)
return r_r, r_i
def divergence_matrix(mesh):
CR = VectorFunctionSpace(mesh, 'CR', 1)
DG = FunctionSpace(mesh, 'DG', 0)
A = cg1_cr_interpolation_matrix(mesh)
M = assemble(dot(div(TrialFunction(CR)), TestFunction(DG))*dx())
compiled_cr_module.cr_divergence_matrix(M, A, DG, CR)
M_mat = as_backend_type(M).mat()
M_mat.matMult(A.mat())
return M
def compute(self, get):
u = get("Velocity")
assemble(dot(u[1].dx(0)-u[0].dx(1), self.q)*dx(), tensor=self.L)
self.bc.apply(self.L)
self.solver.solve(self.psi.vector(), self.L)
#solve(self.A, self.psi.vector(), self.L)
return self.psi
def flux_derivative(self, u, coeff):
"""First derivative of flux."""
lmbda, mu = coeff
Du = self.differential_op(u)
I = Identity(u.cell().d)
Dsigma = 2.0 * mu * div(Du) + dot(nabla_grad(lmbda), tr(Du) * I)
if element_degree(u) >= 2:
Dsigma += lmbda * div(tr(Du) * I)
return Dsigma
def _momentum_equation(u, v, p, f, rho, mu, my_dx):
"""Weak form of the momentum equation.
"""
# rho and my are Constant() functions
assert rho.values()[0] > 0.0
assert mu.values()[0] > 0.0
# Skew-symmetric formulation.
# Don't include the boundary term
#
# - mu *inner(r*grad(u2)*n , v2) * 2*pi*ds.
#
# This effectively means that at all boundaries where no sufficient
# Dirichlet-conditions are posed, we assume grad(u)*n to vanish.
#
# The original term
# u2[0]/(r*r) * v2[0]
# doesn't explode iff u2[0]~r and v2[0]~r at r=0. Hence, we need to enforce
# homogeneous Dirichlet-conditions for n.u at r=0. This corresponds to no
# flow in normal direction through the symmetry axis -- makes sense.
# When using the 2*pi*r weighting, we can even be a bit lax on the
# enforcement on u2[0].
#
# For this to be well defined, u[0]/r and u[2]/r must be bounded for r=0,
# so u[0]~u[2]~r must hold. This either needs to be enforced in the
# boundary conditions (homogeneous Dirichlet for u[0], u[2] at r=0) or must
# follow from the dynamics of the system.
#
# TODO some more explanation for the following lines of code
mesh = v.function_space().mesh()
r = SpatialCoordinate(mesh)[0]
F = (
rho * 0.5 * (dot(grad(u) * u, v) - dot(grad(v) * u, u)) * 2 * pi * r * my_dx
+ mu * inner(r * grad(u), grad(v)) * 2 * pi * my_dx
+ mu * u[0] / r * v[0] * 2 * pi * my_dx
- dot(f, v) * 2 * pi * r * my_dx
)
if p:
F += (p.dx(0) * v[0] + p.dx(1) * v[1]) * 2 * pi * r * my_dx
if len(u) == 3:
F += rho * (-u[2] * u[2] * v[0] + u[0] * u[2] * v[2]) * 2 * pi * my_dx
F += mu * u[2] / r * v[2] * 2 * pi * my_dx
return F
def get_L_form(self):
try:
return self.L_form
except AttributeError:
pass
# Set up equivalent magnetic current forms
M_r = -cross(self.n, self.E_r)
M_i = -cross(self.n, self.E_i)
#------------------------------
# Set up form for far field potential L
theta_hat = self.theta_hat
phi_hat = self.phi_hat
phase = self.phase
L_r = M_r*dolfin.cos(phase) - M_i*dolfin.sin(phase)
L_i = M_r*dolfin.sin(phase) + M_i*dolfin.cos(phase)
self.L_form = dict(
r_theta=dot(theta_hat, L_r)*ds,
r_phi=dot(phi_hat, L_r)*ds,
i_theta=dot(theta_hat, L_i)*ds,
i_phi=dot(phi_hat, L_i)*ds)
return self.L_form
def compute(self, get):
u = get("Velocity")
mu = get("DynamicViscosity")
if isinstance(mu, (float, int)):
mu = Constant(mu)
n = self._n
T = -mu*dot((grad(u) + grad(u).T), n)
Tn = dot(T, n)
Tt = T - Tn*n
tau_form = dot(self.v, Tt)*ds()
assemble(tau_form, tensor=self.tau.vector())
#self.b[self._keys] = self.tau.vector()[self._values] # FIXME: This is not safe!!!
get_set_vector(self.b, self._keys, self.tau.vector(), self._values, self._temp_array)
# Ensure proper scaling
self.solver.solve(self.tau_boundary.vector(), self.b)
return self.tau_boundary
def _get_forms(self):
if self.dirty:
E_r, E_i, g_r, g_i = self.E_r, self.E_i, self.g_r, self.g_i
k0 = self.k0
eps_r = self._get_epsr_function()
mu_r = self._get_mur_function()
form_r = (dot(curl(E_r)/mu_r, curl(g_r)) - dot(curl(E_i)/mu_r, curl(g_i)) \
- k0**2*(dot(eps_r*E_r, g_r) - dot(eps_r*E_i, g_i)))*self.dx
form_i = (dot(curl(E_r)/mu_r, curl(g_i)) + dot(curl(E_i)/mu_r, curl(g_r)) \
- k0**2*(dot(eps_r*E_r, g_i) + dot(eps_r*E_i, g_r)))*self.dx
self.form_r, self.form_i = form_r, form_i
self.dirty = False
return self.form_r, self.form_i
def neumann_residual(self, coeff, v, nu, mesh, homogeneous=False):
"""Neumann boundary residual."""
form = []
a = coeff
boundaries = self.neumann_boundary
g = self.g
if boundaries is not None:
if homogeneous:
g = zero_function(v.function_space())
for g_j, ds_j in self.weak_form.neumann_form_list(boundaries, g, mesh):
r_j = g_j - a * dot(self.weak_form.flux(v, coeff), nu)
form.append((r_j, ds_j))
return form
def neumann_residual(self, coeff, v, nu, mesh, homogeneous=False):
# the coefficient field does not influence the Neumann boundary for Navier-Lame!
"""Neumann boundary residual."""
form = []
boundaries = self.neumann_boundary
g = self.g
if boundaries is not None:
if homogeneous:
g = zero_function(v.function_space())
for g_j, ds_j in self.weak_form.neumann_form_list(boundaries, g, mesh):
r_j = g_j - dot(self.weak_form.flux(v, coeff), nu)
form.append((r_j, ds_j))
return form
def _residual_strong(dx, v, phi, mu, sigma, omega, conv, voltages):
'''Get the residual in strong form, projected onto V.
'''
r = Expression('x[0]', degree=1, cell=triangle)
R = [zero() * dx(0),
zero() * dx(0)]
subdomain_indices = mu.keys()
for i in subdomain_indices:
# diffusion, reaction
R_r = - div(1 / (mu[i] * r) * grad(r * phi[0])) \
- sigma[i] * omega * phi[1]
R_i = - div(1 / (mu[i] * r) * grad(r * phi[1])) \
+ sigma[i] * omega * phi[0]
# convection
if i in conv:
R_r += dot(conv[i], 1 / r * grad(r * phi[0]))
R_i += dot(conv[i], 1 / r * grad(r * phi[1]))
# right-hand side
if i in voltages:
R_r -= sigma[i] * voltages[i].real / (2 * pi * r)
R_i -= sigma[i] * voltages[i].imag / (2 * pi * r)
R[0] += R_r * v * dx(i)
R[1] += R_i * v * dx(i)
return R
def run_and_calculate_error(N, dt, tmax, polydeg_rho, last=False):
"""
Run Ocellaris and return L2 & H1 errors in the last time step
"""
say(N, dt, tmax, polydeg_rho)
# Setup and run simulation
sim = Simulation()
sim.input.read_yaml('transport.inp')
mesh_type = sim.input.get_value('mesh/type')
if mesh_type == 'XML':
# Create unstructured mesh with gmsh
cmd1 = [
'gmsh', '-string',
'lc = %f;' % (3.14 / N), '-o',
'disc_%d.msh' % N, '-2',
'../convergence-variable-density-disk/disc.geo'
]
cmd2 = ['dolfin-convert', 'disc_%d.msh' % N, 'disc.xml']
with open('/dev/null', 'w') as devnull:
for cmd in (cmd1, cmd2):
say(' '.join(cmd))
if ISROOT:
subprocess.call(cmd, stdout=devnull, stderr=devnull)
elif mesh_type == 'UnitDisc':
sim.input.set_value('mesh/N', N // 2)
else:
sim.input.set_value('mesh/Nx', N)
sim.input.set_value('mesh/Ny', N)
sim.input.set_value('time/dt', dt)
sim.input.set_value('time/tmax', tmax)
sim.input.set_value('multiphase_solver/polynomial_degree_rho', polydeg_rho)
sim.input.set_value('output/stdout_enabled', False)
say('Running with multiphase solver %s ...' %
(sim.input.get_value('multiphase_solver/type')))
t1 = time.time()
setup_simulation(sim)
run_simulation(sim)
duration = time.time() - t1
say('DONE')
# Interpolate the analytical solution to the same function space
Vu = sim.data['Vu']
Vp = sim.data['Vp']
Vr = sim.data['Vrho']
polydeg_r = Vr.ufl_element().degree()
vals = dict(t=sim.time, dt=sim.dt)
rho_e = dolfin.Expression(
sim.input.get_value('initial_conditions/rho_p/cpp_code'),
degree=polydeg_r,
**vals)
rho_a = dolfin.project(rho_e, Vr)
rho_e.t = 0
rho_0 = dolfin.project(rho_e, Vr)
# Calculate L2 errors
err_rho = calc_err(sim.data['rho'], rho_a)
# Calculate H1 errors
err_rho_H1 = calc_err(sim.data['rho'], rho_a, 'H1')
mesh = sim.data['mesh']
n = dolfin.FacetNormal(mesh)
reports = sim.reporting.timestep_xy_reports
say('Num time steps:', sim.timestep)
say('Num cells:', mesh.num_cells())
say('Co_max:', numpy.max(reports['Co']))
say('rho_min went from %r to %r' %
(reports['min(rho)'][0], reports['min(rho)'][-1]))
say('rho_max went from %r to %r' %
(reports['max(rho)'][0], reports['max(rho)'][-1]))
m0, m1 = reports['mass'][0], reports['mass'][-1]
say('mass error %.3e (%.3e)' % (m1 - m0, (m1 - m0) / m0))
say('vel compat error %.3e' %
dolfin.assemble(dolfin.dot(sim.data['u'], n) * dolfin.ds))
int_p = dolfin.assemble(sim.data['p'] * dolfin.dx)
say('p*dx', int_p)
div_u_Vp = abs(
dolfin.project(dolfin.div(sim.data['u']),
Vp).vector().get_local()).max()
say('div(u)|Vp', div_u_Vp)
div_u_Vu = abs(
dolfin.project(dolfin.div(sim.data['u']),
Vu).vector().get_local()).max()
say('div(u)|Vu', div_u_Vu)
Vdg0 = dolfin.FunctionSpace(mesh, "DG", 0)
div_u_DG0 = abs(
dolfin.project(dolfin.div(sim.data['u']),
Vdg0).vector().get_local()).max()
say('div(u)|DG0', div_u_DG0)
Vdg1 = dolfin.FunctionSpace(mesh, "DG", 1)
div_u_DG1 = abs(
dolfin.project(dolfin.div(sim.data['u']),
Vdg1).vector().get_local()).max()
say('div(u)|DG1', div_u_DG1)
isoparam = mesh.ufl_coordinate_element().degree() > 1
if last and (not isoparam
or sim.input.get_value('mesh/type') == 'UnitDisc'):
# Plot the results
for fa, name in ((rho_a, 'rho'), ):
fh = sim.data[name]
if isoparam:
# Bug in matplotlib plotting for isoparametric elements
mesh2 = dolfin.UnitDiscMesh(dolfin.MPI.comm_world, N // 2, 1,
2)
ue = fa.function_space().ufl_element()
V2 = dolfin.FunctionSpace(mesh2, ue.family(), ue.degree())
fa2, fh2 = dolfin.Function(V2), dolfin.Function(V2)
fa2.vector().set_local(fa.vector().get_local())
fh2.vector().set_local(fh.vector().get_local())
fa, fh = fa2, fh2
plot(fh - fa, name + ' diff', '%g_%g_%s_diff' % (N, dt, name))
plot(fa, name + ' analytical',
'%g_%g_%s_analytical' % (N, dt, name))
plot(fh, name + ' numerical', '%g_%g_%s_numerical' % (N, dt, name))
plot(rho_0, name + ' initial', '%g_%g_%s_initial' % (N, dt, name))
hmin = mesh.hmin()
return err_rho, err_rho_H1, hmin, dt, duration
displacements_function = df.Function(displacements_function_space)
v = df.TestFunction(displacements_function_space)
residual_form = get_residual_form(displacements_function, v, density_function,
density_function_space, tractionBC, f, 1)
pde_problem.add_state('displacements', displacements_function, residual_form,
'density')
# Add output-avg_density to the PDE problem:
volume = df.assemble(df.Constant(1.) * df.dx(domain=mesh))
avg_density_form = density_function / (df.Constant(
1. * volume)) * df.dx(domain=mesh)
pde_problem.add_scalar_output('avg_density', avg_density_form, 'density')
# Add output-compliance to the PDE problem:
compliance_form = df.dot(f, displacements_function) * dss(6)
pde_problem.add_scalar_output('compliance', compliance_form, 'displacements')
# Add boundary conditions to the PDE problem:
pde_problem.add_bc(
df.DirichletBC(displacements_function_space, df.Constant((0.0, 0.0)),
'(abs(x[0]-0.) < DOLFIN_EPS)'))
# Define the OpenMDAO problem and model
prob = om.Problem()
num_dof_density = pde_problem.inputs_dict['density'][
'function'].function_space().dim()
comp = om.IndepVarComp()
comp.add_output(
def test_moving_mesh():
t = 0.
dt = 0.025
num_steps = 20
xmin, ymin = 0., 0.
xmax, ymax = 2., 2.
xc, yc = 1., 1.
nx, ny = 20, 20
pres = 150
k = 1
mesh = RectangleMesh(Point(xmin, ymin), Point(xmax, ymax), nx, ny)
n = FacetNormal(mesh)
# Class for mesh motion
dU = PeriodicVelocity(xmin, xmax, dt, t, degree=1)
Qcg = VectorFunctionSpace(mesh, 'CG', 1)
boundaries = MeshFunction("size_t", mesh, mesh.topology().dim()-1)
boundaries.set_all(0)
leftbound = Left(xmin)
leftbound.mark(boundaries, 99)
ds = Measure('ds', domain=mesh, subdomain_data=boundaries)
# Create function spaces
Q_E_Rho = FiniteElement("DG", mesh.ufl_cell(), k)
T_1 = FunctionSpace(mesh, 'DG', 0)
Qbar_E = FiniteElement("DGT", mesh.ufl_cell(), k)
Q_Rho = FunctionSpace(mesh, Q_E_Rho)
Qbar = FunctionSpace(mesh, Qbar_E)
phih, phih0 = Function(Q_Rho), Function(Q_Rho)
phibar = Function(Qbar)
# Advective velocity
uh = Function(Qcg)
uh.assign(Constant((0., 0.)))
# Mesh velocity
umesh = Function(Qcg)
# Total velocity
uadvect = uh-umesh
# Now throw in the particles
x = RandomRectangle(Point(xmin, ymin), Point(xmax, ymax)).generate([pres, pres])
s = assign_particle_values(x, GaussianPulse(center=(xc, yc), sigma=float(0.25),
U=[0, 0], time=0., height=1., degree=3))
x = comm.bcast(x, root=0)
s = comm.bcast(s, root=0)
p = particles(x, [s], mesh)
# Define projections problem
FuncSpace_adv = {'FuncSpace_local': Q_Rho, 'FuncSpace_lambda': T_1, 'FuncSpace_bar': Qbar}
FormsPDE = FormsPDEMap(mesh, FuncSpace_adv, ds=ds)
forms_pde = FormsPDE.forms_theta_linear(phih0, uadvect, dt, Constant(1.0), zeta=Constant(0.))
pde_projection = PDEStaticCondensation(mesh, p,
forms_pde['N_a'], forms_pde['G_a'], forms_pde['L_a'],
forms_pde['H_a'],
forms_pde['B_a'],
forms_pde['Q_a'], forms_pde['R_a'], forms_pde['S_a'],
[], 1)
# Initialize the initial condition at mesh by an l2 projection
lstsq_rho = l2projection(p, Q_Rho, 1)
lstsq_rho.project(phih0.cpp_object())
for step in range(num_steps):
# Compute old area at old configuration
old_area = assemble(phih0*dx)
# Pre-assemble rhs
pde_projection.assemble_state_rhs()
# Move mesh
dU.compute_ubc()
umesh.assign(project(dU, Qcg))
ALE.move(mesh, project(dU * dt, Qcg))
dU.update()
# Relocate particles as a result of mesh motion
# NOTE: if particles were advected themselve,
# we had to run update_facets_info() here as well
p.relocate()
# Assemble left-hand side on new config, but not the right-hand side
pde_projection.assemble(True, False)
pde_projection.solve_problem(phibar.cpp_object(), phih.cpp_object(),
'mumps', 'none')
# Needed to compute conservation, note that there
# is an outgoing flux at left boundary
new_area = assemble(phih*dx)
gamma = conditional(ge(dot(uadvect, n), 0), 0, 1)
bflux = assemble((1-gamma) * dot(uadvect, n) * phih * ds)
# Update solution
assign(phih0, phih)
# Put assertion on (global) mass balance, local mass balance is
# too time consuming but should pass also
assert new_area - old_area + bflux * dt < 1e-12
# Assert that max value of phih stays close to 2 and
# min value close to 0. This typically will fail if
# we do not do a correct relocate of particles
assert np.amin(phih.vector().get_local()) > -0.015
assert np.amax(phih.vector().get_local()) < 1.04
def __init__(self, centers, J, n):
self.centers = centers
self.J = J
self.target = 0.002
self.J /= self.target
# dir_path = os.path.dirname(os.path.realpath(__file__))
# with open(os.path.join(dir_path, '../colorio/data/gamut_triangulation.yaml')) as f:
# data = yaml.safe_load(f)
# self.points = np.column_stack([
# data['points'], np.zeros(len(data['points']))
# ])
# self.cells = np.array(data['cells'])
# self.points, self.cells = colorio.xy_gamut_mesh(0.15)
self.points, self.cells = meshzoo.triangle(
n, corners=np.array([[0.0, 0.0], [1.0, 0.0], [0.0, 1.0]])
)
# https://bitbucket.org/fenics-project/dolfin/issues/845/initialize-mesh-from-vertices
editor = MeshEditor()
mesh = Mesh()
editor.open(mesh, "triangle", 2, 2)
editor.init_vertices(self.points.shape[0])
editor.init_cells(self.cells.shape[0])
for k, point in enumerate(self.points):
editor.add_vertex(k, point)
for k, cell in enumerate(self.cells):
editor.add_cell(k, cell)
editor.close()
self.V = FunctionSpace(mesh, "CG", 1)
self.Vgrad = VectorFunctionSpace(mesh, "DG", 0)
# self.ux0 = Function(self.V)
# self.uy0 = Function(self.V)
# 0 starting guess
# ax = np.zeros(self.V.dim())
# ay = np.zeros(self.V.dim())
# Use F(x, y) = (x, y) as starting guess
self.ux0 = project(Expression("x[0]", degree=1), self.V)
self.uy0 = project(Expression("x[1]", degree=1), self.V)
ax = self.ux0.vector().get_local()
ay = self.uy0.vector().get_local()
# Note that alpha doesn't contain the values in the order that one might expect,
# see
# <https://www.allanswered.com/post/awevg/projectexpressionx0-v-vector-get_local-not-in-order/>.
self.alpha = np.concatenate([ax, ay])
self.num_f_eval = 0
# Build L as scipy.csr_matrix
u = TrialFunction(self.V)
v = TestFunction(self.V)
L = assemble(dot(grad(u), grad(v)) * dx)
Lmat = as_backend_type(L).mat()
indptr, indices, data = Lmat.getValuesCSR()
size = Lmat.getSize()
self.L = sparse.csr_matrix((data, indices, indptr), shape=size)
self.LT = self.L.getH()
self.dx, self.dy = build_grad_matrices(self.V, centers)
self.dxT = self.dx.getH()
self.dyT = self.dy.getH()
return
tol = 1E-14
def boundary_D(x, on_boundary):
return on_boundary and (near(x[0], 0, tol) or near(x[0], 1.0, tol))
bc = DirichletBC(V, u_D, boundary_D)
u = TrialFunction(V)
v = TestFunction(V)
f = Expression("10 * exp( - (pow(x[0] - 0.5, 2) + pow(x[1] - 0.5, 2) \
+ pow(x[2] - 0.5, 2)) / 1)",
degree=6)
g = Expression("sin(5.0*x[0])*sin(5.0*x[1])", degree=6)
a = dot(grad(u), grad(v)) * dx
L = f * v * dx + g * v * ds
A = PETScMatrix()
b = PETScVector()
assemble_system(a, L, bc, A_tensor=A, b_tensor=b)
A = A.mat()
b = b.vec()
# =========================================================================
# Construct the alist for systems on levels from fine to coarse
# construct the transfer operators first
ruse = [None] * (nl - 1)
Alist = [None] * (nl)
def Cost(xp):
global x_old, rho_old
comm = nMPI.COMM_WORLD
mpi_rank = comm.Get_rank()
x1, x2 = xp
rs = 8.0 # radiation boundary radius
l = x1 # Patch length
w = 4.5 # Patch width
s1 = x2 * x1 / 2.0 # Feed offset
h = 1.0 # Patch height
t = 0.05 # Metal thickness
lc = 1.0 # Coax length
rc = 0.25 # Coax shield radius
cc = 0.107 #Coax center conductor 50 ohm air diel
eps = 1.0e-4
tol = 1.0e-6
eta = 377.0
eps_c = 1.0
k0 = 2.45 * 2.0 * np.pi / 30.0 # Frequency in GHz
ls = 0.025
lm = 0.8
lw = 0.06
lp = 0.3
if mpi_rank == 0:
print("x[0] = {0:<f}, x[1] = {1:<f} ".format(xp[0], xp[1]))
print("length = {0:<f}, width = {1:<f}, feed offset = {2:<f}".format(l, w, s1))
gmsh.initialize()
gmsh.option.setNumber('General.Terminal', 1)
gmsh.model.add("SimplePatchOpt")
# Radiation sphere
gmsh.model.occ.addSphere(0.0, 0.0, 0.0, rs, 1)
gmsh.model.occ.addBox(0.0, -rs, 0.0, rs, 2*rs, rs, 2)
gmsh.model.occ.intersect([(3,1)],[(3,2)], 3, removeObject=True, removeTool=True)
# Patch
gmsh.model.occ.addBox(0.0, -l/2, h, w/2, l, t, 4)
# coax center
gmsh.model.occ.addCylinder(0.0, s1, -lc, 0.0, 0.0, lc+h, cc, 5, 2.0*np.pi)
# patch center gnd via
#gmsh.model.occ.addCylinder(0.0, 0.0, 0.0, 0.0, 0.0, h, cc, 6, 2.0*np.pi)
# coax shield
gmsh.model.occ.addCylinder(0.0, s1, -lc, 0.0, 0.0, lc, rc, 7)
gmsh.model.occ.addBox(0.0, s1-rc, -lc, rc, 2.0*rc, lc, 8)
gmsh.model.occ.intersect([(3,7)], [(3,8)], 9, removeObject=True, removeTool=True)
gmsh.model.occ.fuse([(3,3)], [(3,9)], 10, removeObject=True, removeTool=True)
# cutout internal boundaries
#gmsh.model.occ.cut([(3,10)], [(3,4),(3,5),(3,6)], 11, removeObject=True, removeTool=True)
gmsh.model.occ.cut([(3,10)], [(3,4),(3,5)], 11, removeObject=True, removeTool=True)
gmsh.option.setNumber('Mesh.MeshSizeMin', ls)
gmsh.option.setNumber('Mesh.MeshSizeMax', lm)
gmsh.option.setNumber('Mesh.Algorithm', 6)
gmsh.option.setNumber('Mesh.Algorithm3D', 1)
# gmsh.option.setNumber('Mesh.MshFileVersion', 2.2)
gmsh.option.setNumber('Mesh.MshFileVersion', 4.1)
gmsh.option.setNumber('Mesh.Format', 1)
gmsh.option.setNumber('Mesh.MinimumCirclePoints', 36)
gmsh.option.setNumber('Mesh.CharacteristicLengthFromCurvature', 1)
gmsh.model.occ.synchronize()
pts = gmsh.model.getEntities(0)
gmsh.model.mesh.setSize(pts, lm) #Set background mesh density
pts = gmsh.model.getEntitiesInBoundingBox(-eps, -l/2-eps, h-eps, w/2+eps, l/2+eps, h+t+eps)
gmsh.model.mesh.setSize(pts, ls)
pts = gmsh.model.getEntitiesInBoundingBox(-eps, s1-rc-eps, -lc-eps, rc+eps, s1+rc+eps, h+eps)
gmsh.model.mesh.setSize(pts, lw)
pts = gmsh.model.getEntitiesInBoundingBox(-eps, -rc-eps, -eps, rc+eps, rc+eps, eps)
gmsh.model.mesh.setSize(pts, lw)
# Embed points to reduce mesh density on patch faces
fce1 = gmsh.model.getEntitiesInBoundingBox(-eps, -l/2-eps, h+t-eps, w/2+eps, l/2+eps, h+t+eps, 2)
gmsh.model.occ.synchronize()
gmsh.model.geo.addPoint(w/4, -l/4, h+t, lp, 1000)
gmsh.model.geo.addPoint(w/4, 0.0, h+t, lp, 1001)
gmsh.model.geo.addPoint(w/4, l/4, h+t, lp, 1002)
gmsh.model.geo.synchronize()
# sf1 = gmsh.model.occ.fragment(fce1, [(0,1000),(0,1001), (0,1002)], -1, True, True)
gmsh.model.occ.synchronize()
print(fce1)
fce2 = gmsh.model.getEntitiesInBoundingBox(-eps, -l/2-eps, h-eps, w/2+eps, l/2+eps, h+eps, 2)
gmsh.model.geo.addPoint(w/4, -9*l/32, h, lp, 1003)
gmsh.model.geo.addPoint(w/4, 0.0, h, lp, 1004)
gmsh.model.geo.addPoint(w/4, 9*l/32, h, lp, 1005)
gmsh.model.geo.synchronize()
for tt in fce1:
gmsh.model.mesh.embed(0, [1000, 1001, 1002], 2, tt[1])
for tt in fce2:
gmsh.model.mesh.embed(0, [1003, 1004, 1005], 2, tt[1])
# sf2 = gmsh.model.occ.fragment(fce2, [(0,1003),(0,1004), (0,1005)], -1, True, True)
print(fce2)
gmsh.model.occ.remove(fce1)
gmsh.model.occ.remove(fce2)
gmsh.model.occ.synchronize()
gmsh.model.addPhysicalGroup(3, [11], 1)
gmsh.model.setPhysicalName(3, 1, "Air")
gmsh.model.mesh.optimize("Relocate3D", niter=5)
gmsh.model.mesh.generate(3)
gmsh.write("SimplePatch.msh")
# gmsh.fltk.run()
gmsh.finalize()
msh = meshio.read("SimplePatch.msh")
for cell in msh.cells:
if cell.type == "tetra":
tetra_cells = cell.data
for key in msh.cell_data_dict["gmsh:physical"].keys():
if key == "tetra":
tetra_data = msh.cell_data_dict["gmsh:physical"][key]
tetra_mesh = meshio.Mesh(points=msh.points, cells={"tetra": tetra_cells},
cell_data={"VolumeRegions":[tetra_data]})
meshio.write("mesh.xdmf", tetra_mesh)
mesh = dolfin.Mesh()
with dolfin.XDMFFile("mesh.xdmf") as infile:
infile.read(mesh)
mvc = dolfin.MeshValueCollection("size_t", mesh, 3)
with dolfin.XDMFFile("mesh.xdmf") as infile:
infile.read(mvc, "VolumeRegions")
cf = dolfin.cpp.mesh.MeshFunctionSizet(mesh, mvc)
class PEC(dolfin.SubDomain):
def inside(self, x, on_boundary):
return on_boundary
class InputBC(dolfin.SubDomain):
def inside(self, x, on_boundary):
return on_boundary and dolfin.near(x[2], -lc, tol)
class OutputBC(dolfin.SubDomain):
def inside(self, x, on_boundary):
rr = np.sqrt(x[0]*x[0]+x[1]*x[1]+x[2]*x[2])
return on_boundary and dolfin.near(rr, 8.0, 1.0e-1)
class PMC(dolfin.SubDomain):
def inside(self, x, on_boundary):
return on_boundary and dolfin.near(x[0], 0.0, tol)
# Volume domains
dolfin.File("VolSubDomains.pvd").write(cf)
dolfin.File("Mesh.pvd").write(mesh)
# Mark boundaries
sub_domains = dolfin.MeshFunction("size_t", mesh, mesh.topology().dim() - 1)
sub_domains.set_all(4)
pec = PEC()
pec.mark(sub_domains, 0)
in_port = InputBC()
in_port.mark(sub_domains, 1)
out_port = OutputBC()
out_port.mark(sub_domains, 2)
pmc = PMC()
pmc.mark(sub_domains, 3)
dolfin.File("BoxSubDomains.pvd").write(sub_domains)
# Set up function spaces
cell = dolfin.tetrahedron
ele_type = dolfin.FiniteElement('N1curl', cell, 2, variant="integral") # H(curl) element for EM
V2 = dolfin.FunctionSpace(mesh, ele_type * ele_type)
V = dolfin.FunctionSpace(mesh, ele_type)
(u_r, u_i) = dolfin.TrialFunctions(V2)
(v_r, v_i) = dolfin.TestFunctions(V2)
dolfin.info(mesh)
#surface integral definitions from boundaries
ds = dolfin.Measure('ds', domain = mesh, subdomain_data = sub_domains)
#volume regions
dx_air = dolfin.Measure('dx', domain = mesh, subdomain_data = cf, subdomain_id = 1)
dx_subst = dolfin.Measure('dx', domain = mesh, subdomain_data = cf, subdomain_id = 2)
# with source and sink terms
u0 = dolfin.Constant((0.0, 0.0, 0.0)) #PEC definition
h_src = dolfin.Expression(('-(x[1] - s) / (2.0 * pi * (pow(x[0], 2.0) + pow(x[1] - s,2.0)))', 'x[0] / (2.0 * pi *(pow(x[0],2.0) + pow(x[1] - s,2.0)))', 0.0), degree = 2, s = s1)
e_src = dolfin.Expression(('x[0] / (2.0 * pi * (pow(x[0], 2.0) + pow(x[1] - s,2.0)))', 'x[1] / (2.0 * pi *(pow(x[0],2.0) + pow(x[1] - s,2.0)))', 0.0), degree = 2, s = s1)
Rrad = dolfin.Expression(('sqrt(x[0] * x[0] + x[1] * x[1] + x[2] * x[2])'), degree = 2)
#Boundary condition dictionary
boundary_conditions = {0: {'PEC' : u0},
1: {'InputBC': (h_src)},
2: {'OutputBC': Rrad}}
n = dolfin.FacetNormal(mesh)
#Build PEC boundary conditions for real and imaginary parts
bcs = []
for i in boundary_conditions:
if 'PEC' in boundary_conditions[i]:
bc = dolfin.DirichletBC(V2.sub(0), boundary_conditions[i]['PEC'], sub_domains, i)
bcs.append(bc)
bc = dolfin.DirichletBC(V2.sub(1), boundary_conditions[i]['PEC'], sub_domains, i)
bcs.append(bc)
# Build input BC source term and loading term
integral_source = []
integrals_load =[]
for i in boundary_conditions:
if 'InputBC' in boundary_conditions[i]:
r = boundary_conditions[i]['InputBC']
bb1 = 2.0 * (k0 * eta) * dolfin.inner(v_i, dolfin.cross(n, r)) * ds(i) #Factor of two from field equivalence principle
integral_source.append(bb1)
bb2 = dolfin.inner(dolfin.cross(n, v_i), dolfin.cross(n, u_r)) * k0 * np.sqrt(eps_c) * ds(i)
integrals_load.append(bb2)
bb2 = dolfin.inner(-dolfin.cross(n, v_r), dolfin.cross(n, u_i)) * k0 * np.sqrt(eps_c) * ds(i)
integrals_load.append(bb2)
for i in boundary_conditions:
if 'OutputBC' in boundary_conditions[i]:
r = boundary_conditions[i]['OutputBC']
bb2 = (dolfin.inner(dolfin.cross(n, v_i), dolfin.cross(n, u_r)) * k0 + 1.0 * dolfin.inner(dolfin.cross(n, v_i), dolfin.cross(n, u_i)) / r)* ds(i)
integrals_load.append(bb2)
bb2 = (dolfin.inner(-dolfin.cross(n, v_r), dolfin.cross(n, u_i)) * k0 + 1.0 * dolfin.inner(dolfin.cross(n, v_r), dolfin.cross(n, u_r)) / r)* ds(i)
integrals_load.append(bb2)
# for PMC, do nothing. Natural BC.
a = (dolfin.inner(dolfin.curl(v_r), dolfin.curl(u_r)) + dolfin.inner(dolfin.curl(v_i), dolfin.curl(u_i)) - eps_c * k0 * k0 * (dolfin.inner(v_r, u_r) + dolfin.inner(v_i, u_i))) * dx_subst + (dolfin.inner(dolfin.curl(v_r), dolfin.curl(u_r)) + dolfin.inner(dolfin.curl(v_i), dolfin.curl(u_i)) - k0 * k0 * (dolfin.inner(v_r, u_r) + dolfin.inner(v_i, u_i))) * dx_air + sum(integrals_load)
L = sum(integral_source)
u1 = dolfin.Function(V2)
vdim = u1.vector().size()
print("Solution vector size =", vdim)
dolfin.solve(a == L, u1, bcs, solver_parameters = {'linear_solver' : 'mumps'})
u1_r, u1_i = u1.split(True)
fp = dolfin.File("EField_r.pvd")
fp << u1_r
fp = dolfin.File("EField_i.pvd")
fp << u1_i
#fp = File('WaveFile.pvd')
#ut = u1_r.copy(deepcopy=True)
#for i in range(50):
# ut.vector().zero()
# ut.vector().axpy(cos(pi * i / 25.0 + pi / 2.0), u1_i.vector())
# ut.vector().axpy(cos(pi * i / 25.0), u1_r.vector())
# fp << (ut, i)
H = dolfin.interpolate(h_src, V) # Get input field
P = dolfin.assemble((-dolfin.dot(u1_r,dolfin.cross(dolfin.curl(u1_i),n))+dolfin.dot(u1_i,dolfin.cross(dolfin.curl(u1_r),n))) * ds(2))
P_refl = dolfin.assemble((-dolfin.dot(u1_i,dolfin.cross(dolfin.curl(u1_r), n)) + dolfin.dot(u1_r, dolfin.cross(dolfin.curl(u1_i), n))) * ds(1))
P_inc = dolfin.assemble((dolfin.dot(H, H) * eta / (2.0 * np.sqrt(eps_c))) * ds(1))
print("Integrated power on port 2:", P/(2.0 * k0 * eta))
print("Incident power at port 1:", P_inc)
print("Integrated reflected power on port 1:", P_inc - P_refl / (2.0 * k0 * eta))
rho_old = (P_inc - P_refl / (2.0 * k0 * eta)) / P_inc #Fraction of incident power reflected as objective function
return rho_old
def j(self, t, u):
return Problem_Basic.j(self, t, dol.assemble(dol.dot(u,self.v)*dol.dx).get_local())
def k_plus(k, n):
return dot(dot(n('+'), k('+')), n('+'))
cell = mesh.ufl_cell()
displacement_fe = df.VectorElement("CG", cell, 1)
temperature_fe = df.FiniteElement("CG", cell, 1)
mixed_fs = df.FunctionSpace(mesh,
df.MixedElement([displacement_fe, temperature_fe]))
mixed_fs.sub(1).dofmap().dofs()
mixed_function = df.Function(mixed_fs)
displacements_function, temperature_function = df.split(mixed_function)
v, T_hat = df.TestFunctions(mixed_fs)
residual_form = get_residual_form(displacements_function, v, density_function,
temperature_function, T_hat, KAPPA, K, ALPHA)
residual_form -= (df.dot(f_r, v) * dss(10) + df.dot(f_t, v) * dss(14) + \
q*T_hat*dss(5) + q_half*T_hat*dss(6) + q_quart*T_hat*dss(7))
print("get residual_form-------")
pde_problem.add_state('mixed_states', mixed_function, residual_form, 'density')
'''
4. 3. Add outputs
'''
# Add output-avg_density to the PDE problem:
volume = df.assemble(df.Constant(1.) * df.dx(domain=mesh))
avg_density_form = density_function / (df.Constant(
1. * volume)) * df.dx(domain=mesh)
pde_problem.add_scalar_output('avg_density', avg_density_form, 'density')
print("Add output-avg_density-------")
# Add output-compliance to the PDE problem:
def ns_IPCS_convection_supg(VQL, mesh, bcs, dt, parameter):
mu, rho, nu, D = parameter
V, Q, L = VQL
vu, vp, vr = TestFunction(V), TestFunction(Q), TestFunction(
L) # for integration
u_, p_, r_ = Function(V), Function(Q), Function(L) # for the solution
u_1, p_1, r_1 = Function(V), Function(Q), Function(
L) # for the prev. solution
u, p, r = TrialFunction(V), TrialFunction(Q), TrialFunction(L) # unknown!
tau_SUPG = Function(L)
bcu = [bcs[0], bcs[1]] # note: no-slip at cylinder wall is no longer used!
bcp = [bcs[2]]
bcr = [DirichletBC(L, rho, inlet)]
# print(h)
# print(h.min(), h.max(), h.mean())
# # C++ version (does not work)
# ue_code = '''
# //https://fenicsproject.discourse.group/t/pass-function-to-c-expression/1081
# #include <pybind11/pybind11.h>
# #include <pybind11/eigen.h>
# #include <dolfin/mesh/Vertex.h>
# namespace py = pybind11;
# #include <dolfin/function/Expression.h>
# #include <dolfin/function/Function.h>
# #include <dolfin/mesh/Mesh.h>
# class SUPG : public dolfin::Expression
# {
# public:
# double D;
# // std::shared_ptr<Mesh> mesh; // doesn work
# std::shared_ptr<dolfin::Function> velocity;
# SUPG(std::shared_ptr<dolfin::Function> u_) : dolfin::Expression(2)
# {
# velocity = u_;
# }
# void eval(Eigen::Ref<Eigen::VectorXd> values,
# Eigen::Ref<const Eigen::VectorXd> x,
# const ufc::cell& cell) const override
# {
# //Cell cell(*mesh, c.index);
# velocity->eval(values, x); // values now holds the velocity?
# double tau = 0.0;
# //double h = cell.h();
# //double h = cell.diameter();
# double h = 0.015;
# double magnitude = 0.0; // pythagoras
# for (uint i=0; i<x.size(); ++i)
# {
# magnitude += values[i] * values[i];
# }
# magnitude = sqrt(magnitude);
# double Pe = magnitude * h / (2.0 * D);
# if (Pe > DOLFIN_EPS)
# {
# tau = h / (2.0*magnitude) * (1.0/tanh(Pe) - 1.0/Pe);
# }
# values[0] = tau;
# };
# };
# PYBIND11_MODULE(SIGNATURE, m)
# {
# py::class_<SUPG, std::shared_ptr<SUPG>, dolfin::Expression>
# (m, "SUPG")
# .def(py::init<std::shared_ptr<dolfin::Function>>())
# .def_readwrite("D", &SUPG::D)
# .def_readwrite("velocity", &SUPG::velocity);
# }
# '''
# compiled = compile_cpp_code(ue_code)
# expr = CompiledExpression(compiled.SUPG(u_.cpp_object()), D=D, degree=1)
# tau_supg_from_expr = project(expr, mesh=mesh).vector().vec().array
# print(tau_supg_from_expr)
# class _rho_(UserExpression):
# def eval(self, values, x):
# if (x[0]-.2)*(x[0]-.2) + (x[1]-.2)*(x[1]-.2) < 0.0025:
# values[0] = rho*5
# else:
# values[0] = rho
# f0 = _rho_(degree=2, element=L.ufl_element())
# r_1.assign(project(f0, mesh=mesh))
x, y = np.split(L.tabulate_dof_coordinates(), 2, 1)
x, y = x.ravel(), y.ravel()
ll = (x - .2) * (x - .2) + (y - .2) * (y - .2) < 0.0025 # logic list
r_1.vector().vec().array = rho
r_1.vector().vec().array[ll] = rho * 5
# cells_mapped = np.empty((mesh.num_cells(), 3), dtype=np.int32)
# for i in range(mesh.num_cells()): # len(mesh.cells())
# # print(cells_mapped[i], L.dofmap().cell_dofs(i))
# cells_mapped[i] = L.dofmap().cell_dofs(i)
# data_mapped = r_1.vector().vec().array
# fig, ax = plt.subplots()
# ax.tricontourf(x, y, cells_mapped, data_mapped, levels=15)
# ax.set_aspect("equal")
# plt.suptitle("initial density")
# plt.show()
n = FacetNormal(mesh)
u_mid = (u + u_1) / 2.0
F1 = r_1*dot((u - u_1) / dt, vu)*dx \
+ r_1*dot(dot(u_1, nabla_grad(u_1)), vu)*dx \
+ inner(sigma(u_mid, p_1, mu), epsilon(vu))*dx \
+ dot(p_1*n, vu)*ds - dot(mu*nabla_grad(u_mid)*n, vu)*ds
a1 = lhs(F1)
L1 = rhs(F1)
# Define variational problem for step 2
a2 = dot(nabla_grad(p), nabla_grad(vp)) * dx
L2 = dot(nabla_grad(p_1),
nabla_grad(vp)) * dx - (1 / dt) * div(u_) * vp * dx
# Define variational problem for step 3
a3 = dot(u, vu) * dx
L3 = dot(u_, vu) * dx - dt * dot(nabla_grad(p_ - p_1), vu) * dx
# Step 4: Transport of rho / Convection-diffusion and SUPG
vr = vr + tau_SUPG * inner(u_, grad(vr)) # SUPG stabilization
r_mid = (r + r_1) / 2.0
F4 = dot((r - r_1) / dt, vr) * dx \
+ dot(dot(u_, grad(r_mid)), vr) * dx
if D > 0.0:
F4 += dot(D * grad(r_mid), grad(vr)) * dx
# F4 += beta * dot(dot(u_, grad(r_mid)), dot(u_, grad(vr))) * dx
a4 = lhs(F4)
L4 = rhs(F4)
# Assemble matrices
A1 = assemble(a1)
A2 = assemble(a2)
A3 = assemble(a3)
# A4 = assemble(a4)
# Apply boundary conditions to matrices
[bc.apply(A1) for bc in bcu]
[bc.apply(A2) for bc in bcp]
return (u_, p_, r_, u_1, p_1, r_1, tau_SUPG, D, L1, a1, L2, A2, L3, A3, L4,
a4, bcu, bcp, bcr)
def k_normal(k, n):
return dot(dot(np.transpose(n), k), n)
Vh = dlfn.FunctionSpace(mesh, P1Curl * P1)
# rhs function
jumpM = dlfn.Constant((0.0, 0.0, -1.0))
# trial functions
A, phi = dlfn.TrialFunctions(Vh)
# test functions
delA, psi = dlfn.TestFunctions(Vh)
# geometric objects
n = dlfn.FacetNormal(mesh)
P = dlfn.Identity(dim) - dlfn.outer(n, n)
# Dirichlet boundary condition on exterior surface
bcA = dlfn.DirichletBC(Vh.sub(0), dlfn.Constant((0.0, 0.0, 0.0)), facetIds,
bndryId)
bcPhi = dlfn.DirichletBC(Vh.sub(1), dlfn.Constant(0.0), facetIds, bndryId)
# bilinear form
a = dlfn.dot(dlfn.curl(A), dlfn.curl(delA)) * dV() \
+ dlfn.dot(A, dlfn.grad(psi)) * dV() \
+ dlfn.dot(dlfn.grad(phi), delA) * dV()
# rhs form
l = dlfn.dot(dlfn.cross(n("+"), jumpM("+")), delA("+")) * dA(intrfcId)
# compute solution
sol = dlfn.Function(Vh)
lin_problem = dlfn.LinearVariationalProblem(a, l, sol, bcs=[bcA, bcPhi])
lin_solver = dlfn.LinearVariationalSolver(lin_problem)
lin_solver_parameters = lin_solver.parameters
lin_solver.solve()
# sub solutions
solA = sol.sub(0)
solPhi = sol.sub(1)
# output to pvd
pvd_A = dlfn.File("solution-A.pvd")
np.array([1, 2], dtype=np.uintp), theta_p, step)
if step == 2:
theta_L.assign(theta_next)
# Probably can be combined into one file?
xdmf_u.write(Uh.sub(0), t)
xdmf_p.write(Uh.sub(1), t)
del (t1)
timer.stop()
# Compute errors
u_exact.t = t
p_exact.t = t
u_error = sqrt(assemble(dot(Uh.sub(0) - u_exact, Uh.sub(0) - u_exact) * dx))
p_error = sqrt(assemble(dot(Uh.sub(1) - p_exact, Uh.sub(1) - p_exact) * dx))
udiv = sqrt(assemble(div(Uh.sub(0)) * div(Uh.sub(0)) * dx))
momentum = assemble((dot(Uh.sub(0), ex) + dot(Uh.sub(0), ey)) * dx)
if comm.Get_rank() == 0:
print("Velocity error " + str(u_error))
print("Pressure error " + str(p_error))
print("Momentum " + str(momentum))
print("Divergence " + str(udiv))
print('Elapsed time ' + str(timer.elapsed()[0]))
list_timings(TimingClear.keep, [TimingType.wall])
def F(
u,
v,
kappa,
rho,
cp,
convection,
source,
r,
neumann_bcs,
robin_bcs,
my_dx,
my_ds,
stabilization,
):
"""
Compute
.. math::
F(u) =
\\int_\\Omega \\kappa r
\\langle\\nabla u, \\nabla \\frac{v}{\\rho c_p}\\rangle
\\, 2\\pi \\, \\text{d}x
+ \\int_\\Omega \\langle c, \\nabla u\\rangle v
\\, 2\\pi r\\,\\text{d}x
- \\int_\\Omega \\frac{1}{\\rho c_p} f v
\\, 2\\pi r \\,\\text{d}x\\\\
- \\int_\\Gamma r \\kappa \\langle n, \\nabla T\\rangle v
\\frac{1}{\\rho c_p} 2\\pi \\,\\text{d}s
- \\int_\\Gamma r \\kappa \\alpha (u - u_0) v
\\frac{1}{\\rho c_p} \\, 2\\pi \\,\\text{d}s,
used for time-stepping
.. math::
u' = F(u).
"""
rho_cp = rho * cp
F0 = kappa * r * dot(grad(u), grad(v / rho_cp)) * 2 * pi * my_dx
# F -= dot(b, grad(u)) * v * 2*pi*r * dx_workpiece(0)
if convection is not None:
c = as_vector([convection[0], convection[1]])
F0 += dot(c, grad(u)) * v * 2 * pi * r * my_dx
# Joule heat
F0 -= source * v / rho_cp * 2 * pi * r * my_dx
# Neumann boundary conditions
for k, n_grad_T in neumann_bcs.items():
F0 -= r * kappa * n_grad_T * v / rho_cp * 2 * pi * my_ds(k)
# Robin boundary conditions
for k, value in robin_bcs.items():
alpha, u0 = value
F0 -= r * kappa * alpha * (u - u0) * v / rho_cp * 2 * pi * my_ds(k)
if stabilization == "supg":
# Add SUPG stabilization.
assert convection is not None
# TODO u_t?
R = (-div(kappa * r * grad(u)) / rho_cp * 2 * pi +
dot(c, grad(u)) * 2 * pi * r - source / rho_cp * 2 * pi * r)
mesh = v.function_space().mesh()
element_degree = v.ufl_element().degree()
tau = stab.supg(mesh, convection, kappa, element_degree)
F0 += R * tau * dot(convection, grad(v)) * my_dx
else:
assert stabilization is None
return F0
editor.add_cell(k, cell)
editor.close()
return mesh
mesh = UnitSquareMesh(200, 200)
# mesh = create_dolfin_mesh(*meshzoo.triangle(1500, corners=[[0, 0], [1, 0], [0, 1]]))
V = FunctionSpace(mesh, "CG", 1)
u = TrialFunction(V)
v = TestFunction(V)
n = FacetNormal(mesh)
# A = assemble(dot(grad(u), grad(v)) * dx - dot(n, grad(u)) * v * ds)
A = assemble(dot(grad(u), grad(v)) * dx - dot(n, grad(u)) * v * ds)
M = assemble(u * v * dx)
f = Expression("sin(pi * x[0]) * sin(pi * x[1])", element=V.ufl_element())
x = project(f, V)
Ax = A * x.vector()
Minv_Ax = Function(V).vector()
solve(M, Minv_Ax, Ax)
val = Ax.inner(Minv_Ax)
print(val)
# Exact value
x = sympy.Symbol("x")
y = sympy.Symbol("y")
def __div__(self, other):
# We use Claas Abert's 'point measure hack' for the vertex-wise operation.
a = self.coerce_scalar_field(other)
w = df.TestFunction(self.functionspace)
v_res = df.assemble(df.dot(self.f / a.f, w) * df.dP)
return Field(self.functionspace, value=v_res)
psi_h.cpp_object(), 'gmres',
'hypre_amg')
# Update old solution
assign(psi0_h, psi_h)
# Store
# if step % store_step is 0 or step is 1:
output_field << psi_h
timer.stop()
# Compute error (we should accurately recover initial condition)
l2_error = sqrt(
abs(
assemble(
dot(psi_h - psi0_expression, psi_h - psi0_expression) *
dx)))
# The global mass conservation error should be zero
area_end = assemble(psi_h * dx)
if comm.Get_rank() == 0:
print("l2 error " + str(l2_error))
# Store in error error table
num_cells_t = mesh.num_entities_global(2)
num_particles = len(x)
area_error_end = np.float64((area_end - area_0))
with open(output_table, "a") as write_file:
write_file.write(
"%-12.5g %-15d %-20d %-10.2e %-20.3g %-20.3g \n" %
def h_u(M, u, reg_u=dl.Constant(dl.DOLFIN_SQRT_EPS)):
"""
Compute the mesh size in the direction u.
"""
return dl.sqrt(dl.dot(u, u) / (dl.dot(dl.dot(u, M), u) + reg_u))
def get_spherical(self):
"""
Transform magnetisation coordinates to spherical coordinates
theta = arctan(m_r / m_z) ; m_r = sqrt(m_x ^ 2 + m_y ^ 2)
phi = arctan(m_y / m_x)
The theta and phi generalised coordinates are stored in
self.theta and self.phi respectively.
When this function is called, the two dolfin functions
are returned
"""
# Create an scalar Function Space to compute the cylindrical radius (x^2 + y^2)
# and the angles phi and theta
S1 = df.FunctionSpace(self.functionspace.mesh(), 'CG', 1)
# Create a dolfin function from the FS
m_r = df.Function(S1)
# Compute the radius using the assemble method with dolfin dP
# (like a dirac delta to get values on every node of the mesh)
# This returns a dolfin vector
cyl_vector = df.assemble(
df.dot(df.sqrt(self.f[0] * self.f[0] + self.f[1] * self.f[1]),
df.TestFunction(S1)) * df.dP, )
# Set the vector values to the dolfin function
m_r.vector().set_local(cyl_vector.get_local())
# Now we compute the theta and phi angles to describe the magnetisation
# and save them to the coresponding variables
self.theta = df.Function(S1)
self.phi = df.Function(S1)
# We will use the same vector variable than the one used to
# compute m_r, in order to save memory
# Theta = arctan(m_r / m_z)
cyl_vector = df.assemble(
df.dot(df.atan_2(m_r, self.f[2]), df.TestFunction(S1)) * df.dP,
tensor=cyl_vector)
# Instead of:
# self.theta.vector().set_local(cyl_vector.get_local())
# We will use:
self.theta.vector().axpy(1, cyl_vector)
# which adds: 1 * cyl_vector
# to self.theta.vector() and is much faster
# (we assume self.theta.vector() is empty, i.e. only made of zeros)
# See: Fenics Book, page 44
# Phi = arctan(m_y / m_x)
cyl_vector = df.assemble(
df.dot(df.atan_2(self.f[1], self.f[0]), df.TestFunction(S1)) *
df.dP,
tensor=cyl_vector)
# We will save this line just in case:
# self.phi.vector().set_local(cyl_vector.get_local())
self.phi.vector().axpy(1, cyl_vector)
return self.theta, self.phi
def h_linear(integrator_type, mesh, subdomains, boundaries, t_start, dt, T, solution0, \
alpha_0, K_0, mu_l_0, lmbda_l_0, Ks_0, \
alpha_1, K_1, mu_l_1, lmbda_l_1, Ks_1, \
alpha, K, mu_l, lmbda_l, Ks, \
cf_0, phi_0, rho_0, mu_0, k_0,\
cf_1, phi_1, rho_1, mu_1, k_1,\
cf, phi, rho, mu, k, \
sigma_v_freeze, dphi_c_dt):
# Create mesh and define function space
parameters["ghost_mode"] = "shared_facet" # required by dS
dx = Measure('dx', domain=mesh, subdomain_data=subdomains)
ds = Measure('ds', domain=mesh, subdomain_data=boundaries)
dS = Measure('dS', domain=mesh, subdomain_data=boundaries)
BDM = FiniteElement("BDM", mesh.ufl_cell(), 1)
PDG = FiniteElement("DG", mesh.ufl_cell(), 0)
BDM_F = FunctionSpace(mesh, BDM)
PDG_F = FunctionSpace(mesh, PDG)
W = BlockFunctionSpace([BDM_F, PDG_F], restrict=[None, None])
TM = TensorFunctionSpace(mesh, 'DG', 0)
PM = FunctionSpace(mesh, 'DG', 0)
n = FacetNormal(mesh)
vc = CellVolume(mesh)
fc = FacetArea(mesh)
h = vc / fc
h_avg = (vc('+') + vc('-')) / (2 * avg(fc))
I = Identity(mesh.topology().dim())
monitor_dt = dt
p_outlet = 0.1e6
p_inlet = 1000.0
M_inv = phi_0 * cf + (alpha - phi_0) / Ks
# Define variational problem
trial = BlockTrialFunction(W)
dv, dp = block_split(trial)
trial_dot = BlockTrialFunction(W)
dv_dot, dp_dot = block_split(trial_dot)
test = BlockTestFunction(W)
psiv, psip = block_split(test)
block_w = BlockFunction(W)
v, p = block_split(block_w)
block_w_dot = BlockFunction(W)
v_dot, p_dot = block_split(block_w_dot)
a_time = Constant(0.0) * inner(v_dot, psiv) * dx #quasi static
# k is a function of phi
#k = perm_update_rutqvist_newton(p,p0,phi0,phi,coeff)
lhs_a = inner(dot(v, mu * inv(k)), psiv) * dx - p * div(
psiv
) * dx #+ 6.0*inner(psiv,n)*ds(2) # - inner(gravity*(rho-rho0), psiv)*dx
b_time = (M_inv + pow(alpha, 2.) / K) * p_dot * psip * dx
lhs_b = div(v) * psip * dx #div(rho*v)*psip*dx #TODO rho
rhs_v = -p_outlet * inner(psiv, n) * ds(3)
rhs_p = -alpha / K * sigma_v_freeze * psip * dx - dphi_c_dt * psip * dx
r_u = [lhs_a, lhs_b]
j_u = block_derivative(r_u, block_w, trial)
r_u_dot = [a_time, b_time]
j_u_dot = block_derivative(r_u_dot, block_w_dot, trial_dot)
r = [r_u_dot[0] + r_u[0] - rhs_v, \
r_u_dot[1] + r_u[1] - rhs_p]
def bc(t):
#bc_v = [DirichletBC(W.sub(0), (.0, .0), boundaries, 4)]
v1 = DirichletBC(W.sub(0), (1.e-4 * 2.0, 0.0), boundaries, 1)
v2 = DirichletBC(W.sub(0), (0.0, 0.0), boundaries, 2)
v4 = DirichletBC(W.sub(0), (0.0, 0.0), boundaries, 4)
bc_v = [v1, v2, v4]
return BlockDirichletBC([bc_v, None])
# Define problem wrapper
class ProblemWrapper(object):
def set_time(self, t):
pass
#g.t = t
# Residual and jacobian functions
def residual_eval(self, t, solution, solution_dot):
#print(as_backend_type(assemble(p_time - p_time_error)).vec().norm())
#print("gravity effect", as_backend_type(assemble(inner(gravity*(rho-rho0), psiv)*dx)).vec().norm())
return r
def jacobian_eval(self, t, solution, solution_dot,
solution_dot_coefficient):
return [[Constant(solution_dot_coefficient)*j_u_dot[0, 0] + j_u[0, 0], \
Constant(solution_dot_coefficient)*j_u_dot[0, 1] + j_u[0, 1]], \
[Constant(solution_dot_coefficient)*j_u_dot[1, 0] + j_u[1, 0], \
Constant(solution_dot_coefficient)*j_u_dot[1, 1] + j_u[1, 1]]]
# Define boundary condition
def bc_eval(self, t):
return bc(t)
# Define initial condition
def ic_eval(self):
return solution0
# Define custom monitor to plot the solution
def monitor(self, t, solution, solution_dot):
pass
# Solve the time dependent problem
problem_wrapper = ProblemWrapper()
(solution, solution_dot) = (block_w, block_w_dot)
solver = TimeStepping(problem_wrapper, solution, solution_dot)
solver.set_parameters({
"initial_time": t_start,
"time_step_size": dt,
"monitor": {
"time_step_size": monitor_dt,
},
"final_time": T,
"exact_final_time": "stepover",
"integrator_type": integrator_type,
"problem_type": "linear",
"linear_solver": "mumps",
"report": True
})
export_solution = solver.solve()
return export_solution, T
def equilibrium_EC(w_, x_, test_functions, solutes, permittivity, mesh, dx, ds,
normal, dirichlet_bcs, neumann_bcs, boundary_to_mark,
use_iterative_solvers, c_lagrange, V_lagrange, **namespace):
""" Electrochemistry equilibrium solver. Nonlinear! """
num_solutes = len(solutes)
cV = df.split(w_["EC"])
c, V = cV[:num_solutes], cV[num_solutes]
if c_lagrange:
c0, V0 = cV[num_solutes + 1:2 * num_solutes + 1], cV[2 * num_solutes +
1]
if V_lagrange:
V0 = cV[-1]
b = test_functions["EC"][:num_solutes]
U = test_functions["EC"][num_solutes]
if c_lagrange:
b0, U0 = cV[num_solutes + 1:2 * num_solutes + 1], cV[2 * num_solutes +
1]
if V_lagrange:
U0 = test_functions["EC"][-1]
phi = x_["phi"]
q = []
sum_zx = sum([solute[1] * xj for solute, xj in zip(solutes, composition)])
for solute, xj in zip(solutes, composition):
q.append(-xj * Q / (area * sum_zx))
z = [] # Charge z[species]
K = [] # Diffusivity K[species]
beta = []
for solute in solutes:
z.append(solute[1])
K.append(ramp(phi, solute[2:4]))
beta.append(ramp(phi, solute[4:6]))
rho_e = sum([c_e * z_e for c_e, z_e in zip(c, z)])
veps = ramp(phi, permittivity)
F_c = []
for ci, bi, c0i, b0i, solute, qi, betai, Ki in zip(c, b, c0, b0, solutes,
q, beta, K):
zi = solute[1]
F_ci = Ki * (df.dot(
df.grad(bi),
df.grad(ci) + df.grad(betai) + zi * ci * df.grad(V))) * dx
if c_lagrange:
F_ci += b0i * (ci - df.Constant(qi)) * dx + c0i * bi * dx
F_V = veps * df.dot(df.grad(U), df.grad(V)) * dx
for boundary_name, sigma_e in neumann_bcs["V"].iteritems():
F_V += -sigma_e * U * ds(boundary_to_mark[boundary_name])
if rho_e != 0:
F_V += -rho_e * U * dx
if V_lagrange:
F_V += V0 * U * dx + V * U0 * dx
F = sum(F_c) + F_V
J = df.derivative(F, w_["EC"])
problem = df.NonlinearVariationalProblem(F, w_["EC"], dirichlet_bcs["EC"],
J)
solver = df.NonlinearVariationalSolver(problem)
solver.parameters["newton_solver"]["relative_tolerance"] = 1e-7
if use_iterative_solvers:
solver.parameters["newton_solver"]["linear_solver"] = "bicgstab"
if not V_lagrange:
solver.parameters["newton_solver"]["preconditioner"] = "hypre_amg"
solver.solve()
def setup_NS(w_NS, u, p, v, q, p0, q0, dx, ds, normal, dirichlet_bcs,
neumann_bcs, boundary_to_mark, u_1, phi_, rho_, rho_1, g_, M_,
mu_, rho_e_, c_, V_, c_1, V_1, dbeta, solutes, per_tau, drho,
sigma_bar, eps, dveps, grav, enable_PF, enable_EC,
use_iterative_solvers, use_pressure_stabilization, p_lagrange,
q_rhs):
""" Set up the Navier-Stokes subproblem. """
# F = (
# per_tau * rho_ * df.dot(u - u_1, v)*dx
# + rho_*df.inner(df.grad(u), df.outer(u_1, v))*dx
# + 2*mu_*df.inner(df.sym(df.grad(u)), df.grad(v))*dx
# - p * df.div(v)*dx
# + df.div(u)*q*dx
# - df.dot(rho_*grav, v)*dx
# )
mom_1 = rho_1 * u_1
if enable_PF:
mom_1 += -M_ * drho * df.nabla_grad(g_)
F = (per_tau * rho_1 * df.dot(u - u_1, v) * dx + 2 * mu_ *
df.inner(df.sym(df.nabla_grad(u)), df.sym(df.nabla_grad(v))) * dx -
p * df.div(v) * dx - q * df.div(u) * dx +
df.inner(df.nabla_grad(u), df.outer(mom_1, v)) * dx + 0.5 *
(per_tau * (rho_ - rho_1) * df.dot(u, v) -
df.dot(mom_1, df.nabla_grad(df.dot(u, v)))) * dx -
rho_ * df.dot(grav, v) * dx)
for boundary_name, slip_length in neumann_bcs["u"].iteritems():
F += 1./slip_length * \
df.dot(u, v) * ds(boundary_to_mark[boundary_name])
for boundary_name, pressure in neumann_bcs["p"].iteritems():
F += pressure * df.inner(normal, v) * ds(
boundary_to_mark[boundary_name])
if enable_PF:
F += phi_ * df.dot(df.grad(g_), v) * dx
if enable_EC:
for ci_, ci_1, dbetai, solute in zip(c_, c_1, dbeta, solutes):
zi = solute[1]
F += df.dot(df.grad(ci_), v)*dx \
+ zi*ci_1*df.dot(df.grad(V_), v)*dx
if enable_PF:
F += ci_ * dbetai * df.dot(df.grad(phi_), v) * dx
if p_lagrange:
F += (p * q0 + q * p0) * dx
if "u" in q_rhs:
F += -df.dot(q_rhs["u"], v) * dx
a, L = df.lhs(F), df.rhs(F)
problem = df.LinearVariationalProblem(a, L, w_NS, dirichlet_bcs)
solver = df.LinearVariationalSolver(problem)
if use_iterative_solvers and use_pressure_stabilization:
solver.parameters["linear_solver"] = "gmres"
# solver.parameters["preconditioner"] = "ilu"
return solver
def run_and_calculate_error(N, dt, tmax, polydeg_u, polydeg_p, nu, last=False):
"""
Run Ocellaris and return L2 & H1 errors in the last time step
"""
say(N, dt, tmax, polydeg_u, polydeg_p)
# Setup and run simulation
timingtypes = [
dolfin.TimingType.user, dolfin.TimingType.system,
dolfin.TimingType.wall
]
dolfin.timings(dolfin.TimingClear_clear, timingtypes)
sim = Simulation()
sim.input.read_yaml('disc.inp')
mesh_type = sim.input.get_value('mesh/type')
if mesh_type == 'XML':
# Create unstructured mesh with gmsh
cmd1 = [
'gmsh', '-string',
'lc = %f;' % (3.14 / N), '-o',
'disc_%d.msh' % N, '-2', 'disc.geo'
]
cmd2 = ['dolfin-convert', 'disc_%d.msh' % N, 'disc.xml']
with open('/dev/null', 'w') as devnull:
for cmd in (cmd1, cmd2):
say(' '.join(cmd))
subprocess.call(cmd, stdout=devnull, stderr=devnull)
elif mesh_type == 'UnitDisc':
sim.input.set_value('mesh/N', N // 2)
else:
sim.input.set_value('mesh/Nx', N)
sim.input.set_value('mesh/Ny', N)
sim.input.set_value('time/dt', dt)
sim.input.set_value('time/tmax', tmax)
sim.input.set_value('solver/polynomial_degree_velocity', polydeg_u)
sim.input.set_value('solver/polynomial_degree_pressure', polydeg_p)
sim.input.set_value('physical_properties/nu', nu)
sim.input.set_value('output/stdout_enabled', False)
say('Running with %s %s solver ...' %
(sim.input.get_value('solver/type'),
sim.input.get_value('solver/function_space_velocity')))
t1 = time.time()
setup_simulation(sim)
run_simulation(sim)
duration = time.time() - t1
say('DONE')
# Interpolate the analytical solution to the same function space
Vu = sim.data['Vu']
Vp = sim.data['Vp']
Vr = sim.data['Vrho']
polydeg_r = Vr.ufl_element().degree()
vals = dict(t=sim.time,
dt=sim.dt,
Q=sim.input.get_value('user_code/constants/Q'))
rho_e = dolfin.Expression(
sim.input.get_value('initial_conditions/rho_p/cpp_code'),
degree=polydeg_r,
**vals)
u0e = dolfin.Expression(
sim.input.get_value('initial_conditions/up0/cpp_code'),
degree=polydeg_u,
**vals)
u1e = dolfin.Expression(
sim.input.get_value('initial_conditions/up1/cpp_code'),
degree=polydeg_u,
**vals)
pe = dolfin.Expression(
sim.input.get_value('initial_conditions/p/cpp_code'),
degree=polydeg_p,
**vals)
rho_a = dolfin.project(rho_e, Vr)
u0a = dolfin.project(u0e, Vu)
u1a = dolfin.project(u1e, Vu)
pa = dolfin.project(pe, Vp)
mesh = sim.data['mesh']
n = dolfin.FacetNormal(mesh)
# Correct for possible non-zero average p
int_p = dolfin.assemble(sim.data['p'] * dolfin.dx)
int_pa = dolfin.assemble(pa * dolfin.dx)
vol = dolfin.assemble(dolfin.Constant(1.0) * dolfin.dx(domain=mesh))
pa_avg = int_pa / vol
sim.data['p'].vector()[:] += pa_avg
# Calculate L2 errors
err_rho = calc_err(sim.data['rho'], rho_a)
err_u0 = calc_err(sim.data['u0'], u0a)
err_u1 = calc_err(sim.data['u1'], u1a)
err_p = calc_err(sim.data['p'], pa)
# Calculate H1 errors
err_rho_H1 = calc_err(sim.data['rho'], rho_a, 'H1')
err_u0_H1 = calc_err(sim.data['u0'], u0a, 'H1')
err_u1_H1 = calc_err(sim.data['u1'], u1a, 'H1')
err_p_H1 = calc_err(sim.data['p'], pa, 'H1')
reports = sim.reporting.timestep_xy_reports
say('Num time steps:', sim.timestep)
say('Num cells:', mesh.num_cells())
Co_max, Pe_max = numpy.max(reports['Co']), numpy.max(reports['Pe'])
say('Co_max:', Co_max)
say('Pe_max:', Pe_max)
say('rho_min went from %r to %r' %
(reports['min(rho)'][0], reports['min(rho)'][-1]))
say('rho_max went from %r to %r' %
(reports['max(rho)'][0], reports['max(rho)'][-1]))
m0, m1 = reports['mass'][0], reports['mass'][-1]
say('mass error %.3e (%.3e)' % (m1 - m0, (m1 - m0) / m0))
say('vel repr error %.3e' %
dolfin.assemble(dolfin.dot(sim.data['u'], n) * dolfin.ds))
say('p*dx', int_p)
div_u_Vp = abs(
dolfin.project(dolfin.div(sim.data['u']),
Vp).vector().get_local()).max()
say('div(u)|Vp', div_u_Vp)
div_u_Vu = abs(
dolfin.project(dolfin.div(sim.data['u']),
Vu).vector().get_local()).max()
say('div(u)|Vu', div_u_Vu)
Vdg0 = dolfin.FunctionSpace(mesh, "DG", 0)
div_u_DG0 = abs(
dolfin.project(dolfin.div(sim.data['u']),
Vdg0).vector().get_local()).max()
say('div(u)|DG0', div_u_DG0)
Vdg1 = dolfin.FunctionSpace(mesh, "DG", 1)
div_u_DG1 = abs(
dolfin.project(dolfin.div(sim.data['u']),
Vdg1).vector().get_local()).max()
say('div(u)|DG1', div_u_DG1)
isoparam = mesh.ufl_coordinate_element().degree() > 1
allways_plot = True
if (last or allways_plot) and (
not isoparam or sim.input.get_value('mesh/type') == 'UnitDisc'):
# Plot the results
for fa, name in ((u0a, 'u0'), (u1a, 'u1'), (pa, 'p'), (rho_a, 'rho')):
fh = sim.data[name]
if isoparam:
# Bug in matplotlib plotting for isoparametric elements
mesh2 = dolfin.UnitDiscMesh(dolfin.MPI.comm_world, N // 2, 1,
2)
ue = fa.function_space().ufl_element()
V2 = dolfin.FunctionSpace(mesh2, ue.family(), ue.degree())
fa2, fh2 = dolfin.Function(V2), dolfin.Function(V2)
fa2.vector().set_local(fa.vector().get_local())
fh2.vector().set_local(fh.vector().get_local())
fa, fh = fa2, fh2
discr = '' # '%g_%g_' % (N, dt)
plot(fa, name + ' analytical', '%s%s_1analytical' % (discr, name))
plot(fh, name + ' numerical', '%s%s_2numerical' % (discr, name))
plot(fh - fa, name + ' diff', '%s%s_3diff' % (discr, name))
hmin = mesh.hmin()
return err_rho, err_u0, err_u1, err_p, err_rho_H1, err_u0_H1, err_u1_H1, err_p_H1, hmin, dt, Co_max, Pe_max, duration
def __init__(self, V, viscosity=1e-2, penalty=1e5):
'''
Parameters
----------
V : dolfin.FunctionSpace
Function space for the distance function.
viscosity: float or dolfin.Constant
Stabilization for the unique solution of the distance problem.
penalty: float or dolfin.Constant
Penalty for weakly enforcing the zero-distance boundary conditions.
'''
if not isinstance(V, dolfin.FunctionSpace):
raise TypeError('Parameter `V` must be a `dolfin.FunctionSpace`')
if not isinstance(viscosity, Constant):
if not isinstance(viscosity, (float, int)):
raise TypeError('`Parameter `viscosity`')
viscosity = Constant(viscosity)
if not isinstance(penalty, Constant):
if not isinstance(penalty, (float, int)):
raise TypeError('Parameter `penalty`')
penalty = Constant(penalty)
self._viscosity = viscosity
self._penalty = penalty
mesh = V.mesh()
xs = mesh.coordinates()
l0 = (xs.max(0) - xs.min(0)).min()
self._d = d = Function(V)
self._Q = dolfin.FunctionSpace(mesh, 'DG', 0)
self._mf = dolfin.MeshFunction('size_t', mesh,
mesh.geometric_dimension())
self._dx_penalty = dx(subdomain_id=1,
subdomain_data=self._mf,
domain=mesh)
v0 = dolfin.TestFunction(V)
v1 = dolfin.TrialFunction(V)
target_gradient = Constant(1.0)
scaled_penalty = penalty / mesh.hmax()
lhs_F0 = l0*dot(grad(v0), grad(v1))*dx \
+ scaled_penalty*v0*v1*self._dx_penalty
rhs_F0 = v0 * target_gradient * dx
problem = dolfin.LinearVariationalProblem(lhs_F0, rhs_F0, d)
self._linear_solver = dolfin.LinearVariationalSolver(problem)
self._linear_solver.parameters["symmetric"] = True
F = v0*(grad(d)**2-target_gradient)*dx \
+ viscosity*l0*dot(grad(v0), grad(d))*dx \
+ scaled_penalty*v0*d*self._dx_penalty
J = dolfin.derivative(F, d, v1)
problem = dolfin.NonlinearVariationalProblem(F, d, bcs=None, J=J)
self._nonlinear_solver = dolfin.NonlinearVariationalSolver(problem)
self._nonlinear_solver.parameters['nonlinear_solver'] = 'newton'
self._nonlinear_solver.parameters['symmetric'] = False
self._solve_initdist_problem = self._linear_solver.solve
self._solve_distance_problem = self._nonlinear_solver.solve
@function.expression.numba_eval
def ui_eval(values, x, cell_idx):
values[:, 0] = np.exp(1.0j * k0 *
(np.cos(theta) * x[:, 0] + np.sin(theta) * x[:, 1]))
# Test and trial function space
V = FunctionSpace(mesh, ("Lagrange", deg))
# Prepare Expression as FE function
ui = interpolate(Expression(ui_eval), V)
# Define variational problem
u = TrialFunction(V)
v = TestFunction(V)
g = dot(grad(ui), n) + 1j * k0 * ui
a = inner(grad(u), grad(v)) * dx - k0**2 * inner(u, v) * dx + 1j * k0 * inner(
u, v) * ds
L = inner(g, v) * ds
# Compute solution
u = Function(V)
solve(a == L, u, [])
# Save solution in XDMF format (to be viewed in Paraview, for example)
with XDMFFile(MPI.comm_world,
"plane_wave.xdmf",
encoding=XDMFFile.Encoding.HDF5) as file:
file.write(u)
"""Calculate L2 and H1 errors of FEM solution and best approximation.
This demonstrates the error bounds given in Ihlenburg. Pollution errors
def update_charge(self, phi):
bnd_id = self.domain_args[1]
projection = df.dot(df.grad(phi), self.n) * self.dss(bnd_id)
self.charge = df.assemble(projection)
return self.charge
def setup_scalar_equation(self):
sim = self.simulation
V = sim.data['Vphi']
mesh = V.mesh()
P = V.ufl_element().degree()
# Source term
source_cpp = sim.input.get_value('solver/source', '0', 'string')
f = dolfin.Expression(source_cpp, degree=P)
# Create the solution function
sim.data['phi'] = dolfin.Function(V)
# DG elliptic penalty
penalty = define_penalty(mesh, P, k_min=1.0, k_max=1.0)
penalty_dS = dolfin.Constant(penalty)
penalty_ds = dolfin.Constant(penalty * 2)
yh = dolfin.Constant(1 / (penalty * 2))
# Define weak form
u, v = dolfin.TrialFunction(V), dolfin.TestFunction(V)
a = dot(grad(u), grad(v)) * dx
L = f * v * dx
# Symmetric Interior Penalty method for -∇⋅∇φ
n = dolfin.FacetNormal(mesh)
a -= dot(n('+'), avg(grad(u))) * jump(v) * dS
a -= dot(n('+'), avg(grad(v))) * jump(u) * dS
# Symmetric Interior Penalty coercivity term
a += penalty_dS * jump(u) * jump(v) * dS
# Dirichlet boundary conditions
# Nitsche's (1971) method, see e.g. Epshteyn and Rivière (2007)
dirichlet_bcs = sim.data['dirichlet_bcs'].get('phi', [])
for dbc in dirichlet_bcs:
bcval, dds = dbc.func(), dbc.ds()
# SIPG for -∇⋅∇φ
a -= dot(n, grad(u)) * v * dds
a -= dot(n, grad(v)) * u * dds
L -= dot(n, grad(v)) * bcval * dds
# Weak Dirichlet
a += penalty_ds * u * v * dds
L += penalty_ds * bcval * v * dds
# Neumann boundary conditions
neumann_bcs = sim.data['neumann_bcs'].get('phi', [])
for nbc in neumann_bcs:
L += nbc.func() * v * nbc.ds()
# Robin boundary conditions
# See Juntunen and Stenberg (2009)
# n⋅∇φ = (φ0 - φ)/b + g
robin_bcs = sim.data['robin_bcs'].get('phi', [])
for rbc in robin_bcs:
b, rds = rbc.blend(), rbc.ds()
dval, nval = rbc.dfunc(), rbc.nfunc()
# From IBP of the main equation
a -= dot(n, grad(u)) * v * rds
# Test functions for the Robin BC
z1 = 1 / (b + yh) * v
z2 = -yh / (b + yh) * dot(n, grad(v))
# Robin BC added twice with different test functions
for z in [z1, z2]:
a += b * dot(n, grad(u)) * z * rds
a += u * z * rds
L += dval * z * rds
L += b * nval * z * rds
# Does the system have a null-space?
self.has_null_space = len(dirichlet_bcs) + len(robin_bcs) == 0
self.form_lhs = a
self.form_rhs = L
def __init__(self, Vh, covariance, mean=None):
"""
Constructor
Inputs:
- :code:`Vh`: Finite element space on which the prior is
defined. Must be the Real space with one global
degree of freedom
- :code:`covariance`: The covariance of the prior. Must be a
:code:`numpy.ndarray` of appropriate size
- :code:`mean`(optional): Mean of the prior distribution. Must be of
type `dolfin.Vector()`
"""
self.Vh = Vh
if Vh.dim() != covariance.shape[0] or Vh.dim() != covariance.shape[1]:
raise ValueError(
"Covariance incompatible with Finite Element space")
if not np.issubdtype(covariance.dtype, np.floating):
raise TypeError("Covariance matrix must be a float array")
self.covariance = covariance
#np.linalg.cholesky automatically provides more error checking,
#so use those
self.chol = np.linalg.cholesky(self.covariance)
self.chol_inv = scila.solve_triangular(self.chol,
np.identity(Vh.dim()),
lower=True)
self.precision = np.dot(self.chol_inv.T, self.chol_inv)
trial = dl.TrialFunction(Vh)
test = dl.TestFunction(Vh)
domain_measure_inv = dl.Constant(1.0 \
/ dl.assemble(dl.Constant(1.) * dl.dx(Vh.mesh())))
#Identity mass matrix
self.M = dl.assemble(domain_measure_inv * dl.inner(trial, test) *
dl.dx)
self.Msolver = Operator2Solver(self.M)
if mean:
self.mean = mean
else:
tmp = dl.Vector()
self.M.init_vector(tmp, 0)
tmp.zero()
self.mean = tmp
if Vh.dim() == 1:
trial = dl.as_matrix([[trial]])
test = dl.as_matrix([[test]])
#Create form matrices
covariance_op = dl.as_matrix(list(map(list, self.covariance)))
precision_op = dl.as_matrix(list(map(list, self.precision)))
chol_op = dl.as_matrix(list(map(list, self.chol)))
chol_inv_op = dl.as_matrix(list(map(list, self.chol_inv)))
#variational for the regularization operator, or the precision matrix
var_form_R = domain_measure_inv \
* dl.inner(test, dl.dot(precision_op, trial)) * dl.dx
#variational for the inverse regularization operator, or the covariance
#matrix
var_form_Rinv = domain_measure_inv \
* dl.inner(test, dl.dot(covariance_op, trial)) * dl.dx
#variational form for the square root of the regularization operator
var_form_R_sqrt = domain_measure_inv \
* dl.inner(test, dl.dot(chol_inv_op.T, trial)) * dl.dx
#variational form for the square root of the inverse regularization
#operator
var_form_Rinv_sqrt = domain_measure_inv \
* dl.inner(test, dl.dot(chol_op, trial)) * dl.dx
self.R = dl.assemble(var_form_R)
self.RSolverOp = dl.assemble(var_form_Rinv)
self.Rsolver = Operator2Solver(self.RSolverOp)
self.sqrtR = dl.assemble(var_form_R_sqrt)
self.sqrtRinv = dl.assemble(var_form_Rinv_sqrt)
def end_hook(x_, enable_NS, dx, **namespace):
u_norm = 0.
if enable_NS:
u_norm = df.assemble(df.dot(x_["u"], x_["u"])*dx)
info("Velocity norm = {:e}".format(u_norm))
def assemble_laplacian(self):
print("Assembling laplacians")
# laplacian discretisation
self.laplacian = assemble(dot(grad(self.w), grad(self.u)) * dx)