Files
mfem/examples/ex9p.cpp
T

848 lines
26 KiB
C++

// MFEM Example 9 - Parallel Version
//
// Compile with: make ex9p
//
// Sample runs:
// mpirun -np 4 ex9p -m ../data/periodic-segment.mesh -p 0 -dt 0.005
// mpirun -np 4 ex9p -m ../data/periodic-square.mesh -p 0 -dt 0.01
// mpirun -np 4 ex9p -m ../data/periodic-hexagon.mesh -p 0 -dt 0.01
// mpirun -np 4 ex9p -m ../data/periodic-square.mesh -p 1 -dt 0.005 -tf 9
// mpirun -np 4 ex9p -m ../data/periodic-hexagon.mesh -p 1 -dt 0.005 -tf 9
// mpirun -np 4 ex9p -m ../data/amr-quad.mesh -p 1 -rp 1 -dt 0.002 -tf 9
// mpirun -np 4 ex9p -m ../data/amr-quad.mesh -p 1 -rp 1 -dt 0.02 -s 13 -tf 9
// mpirun -np 4 ex9p -m ../data/star-q3.mesh -p 1 -rp 1 -dt 0.004 -tf 9
// mpirun -np 4 ex9p -m ../data/star-mixed.mesh -p 1 -rp 1 -dt 0.004 -tf 9
// mpirun -np 4 ex9p -m ../data/disc-nurbs.mesh -p 1 -rp 1 -dt 0.005 -tf 9
// mpirun -np 4 ex9p -m ../data/disc-nurbs.mesh -p 2 -rp 1 -dt 0.005 -tf 9
// mpirun -np 4 ex9p -m ../data/periodic-square.mesh -p 3 -rp 2 -dt 0.0025 -tf 9 -vs 20
// mpirun -np 4 ex9p -m ../data/periodic-cube.mesh -p 0 -o 2 -rp 1 -dt 0.01 -tf 8
// mpirun -np 4 ex9p -m ../data/periodic-square.msh -p 0 -rs 2 -dt 0.005 -tf 2
// mpirun -np 4 ex9p -m ../data/periodic-cube.msh -p 0 -rs 1 -o 2 -tf 2
// mpirun -np 3 ex9p -m ../data/amr-hex.mesh -p 1 -rs 1 -rp 0 -dt 0.005 -tf 0.5
//
// Device sample runs:
// mpirun -np 4 ex9p -pa
// mpirun -np 4 ex9p -ea
// mpirun -np 4 ex9p -fa
// mpirun -np 4 ex9p -pa -m ../data/periodic-cube.mesh
// mpirun -np 4 ex9p -pa -m ../data/periodic-cube.mesh -d cuda
// mpirun -np 4 ex9p -ea -m ../data/periodic-cube.mesh -d cuda
// mpirun -np 4 ex9p -fa -m ../data/periodic-cube.mesh -d cuda
// mpirun -np 4 ex9p -pa -m ../data/amr-quad.mesh -p 1 -rp 1 -dt 0.002 -tf 9 -d cuda
//
// Description: This example code solves the time-dependent advection equation
// du/dt + v.grad(u) = 0, where v is a given fluid velocity, and
// u0(x)=u(0,x) is a given initial condition.
//
// The example demonstrates the use of Discontinuous Galerkin (DG)
// bilinear forms in MFEM (face integrators), the use of implicit
// and explicit ODE time integrators, the definition of periodic
// boundary conditions through periodic meshes, as well as the use
// of GLVis for persistent visualization of a time-evolving
// solution. Saving of time-dependent data files for visualization
// with VisIt (visit.llnl.gov) and ParaView (paraview.org), as
// well as the optional saving with ADIOS2 (adios2.readthedocs.io)
// are also illustrated.
#include "mfem.hpp"
#include <fstream>
#include <iostream>
using namespace std;
using namespace mfem;
// Choice for the problem setup. The fluid velocity, initial condition and
// inflow boundary condition are chosen based on this parameter.
int problem;
// Velocity coefficient
void velocity_function(const Vector &x, Vector &v);
// Initial condition
double u0_function(const Vector &x);
// Inflow boundary condition
double inflow_function(const Vector &x);
// Mesh bounding box
Vector bb_min, bb_max;
// Type of preconditioner for implicit time integrator
enum class PrecType : int
{
ILU = 0,
AIR = 1
};
#if MFEM_HYPRE_VERSION >= 21800
// Algebraic multigrid preconditioner for advective problems based on
// approximate ideal restriction (AIR). Most effective when matrix is
// first scaled by DG block inverse, and AIR applied to scaled matrix.
// See https://doi.org/10.1137/17M1144350.
class AIR_prec : public Solver
{
private:
const HypreParMatrix *A;
// Copy of A scaled by block-diagonal inverse
HypreParMatrix A_s;
HypreBoomerAMG *AIR_solver;
int blocksize;
public:
AIR_prec(int blocksize_) : AIR_solver(NULL), blocksize(blocksize_) { }
void SetOperator(const Operator &op)
{
width = op.Width();
height = op.Height();
A = dynamic_cast<const HypreParMatrix *>(&op);
MFEM_VERIFY(A != NULL, "AIR_prec requires a HypreParMatrix.")
// Scale A by block-diagonal inverse
BlockInverseScale(A, &A_s, NULL, NULL, blocksize,
BlockInverseScaleJob::MATRIX_ONLY);
delete AIR_solver;
AIR_solver = new HypreBoomerAMG(A_s);
AIR_solver->SetAdvectiveOptions(1, "", "FA");
AIR_solver->SetPrintLevel(0);
AIR_solver->SetMaxLevels(50);
}
virtual void Mult(const Vector &x, Vector &y) const
{
// Scale the rhs by block inverse and solve system
HypreParVector z_s;
BlockInverseScale(A, NULL, &x, &z_s, blocksize,
BlockInverseScaleJob::RHS_ONLY);
AIR_solver->Mult(z_s, y);
}
~AIR_prec()
{
delete AIR_solver;
}
};
#endif
class DG_Solver : public Solver
{
private:
HypreParMatrix &M, &K;
SparseMatrix M_diag;
HypreParMatrix *A;
GMRESSolver linear_solver;
Solver *prec;
double dt;
public:
DG_Solver(HypreParMatrix &M_, HypreParMatrix &K_, const FiniteElementSpace &fes,
PrecType prec_type)
: M(M_),
K(K_),
A(NULL),
linear_solver(M.GetComm()),
dt(-1.0)
{
int block_size = fes.GetFE(0)->GetDof();
if (prec_type == PrecType::ILU)
{
prec = new BlockILU(block_size,
BlockILU::Reordering::MINIMUM_DISCARDED_FILL);
}
else if (prec_type == PrecType::AIR)
{
#if MFEM_HYPRE_VERSION >= 21800
prec = new AIR_prec(block_size);
#else
MFEM_ABORT("Must have MFEM_HYPRE_VERSION >= 21800 to use AIR.\n");
#endif
}
linear_solver.iterative_mode = false;
linear_solver.SetRelTol(1e-9);
linear_solver.SetAbsTol(0.0);
linear_solver.SetMaxIter(100);
linear_solver.SetPrintLevel(0);
linear_solver.SetPreconditioner(*prec);
M.GetDiag(M_diag);
}
void SetTimeStep(double dt_)
{
if (dt_ != dt)
{
dt = dt_;
// Form operator A = M - dt*K
delete A;
A = Add(-dt, K, 0.0, K);
SparseMatrix A_diag;
A->GetDiag(A_diag);
A_diag.Add(1.0, M_diag);
// this will also call SetOperator on the preconditioner
linear_solver.SetOperator(*A);
}
}
void SetOperator(const Operator &op)
{
linear_solver.SetOperator(op);
}
virtual void Mult(const Vector &x, Vector &y) const
{
linear_solver.Mult(x, y);
}
~DG_Solver()
{
delete prec;
delete A;
}
};
/** A time-dependent operator for the right-hand side of the ODE. The DG weak
form of du/dt = -v.grad(u) is M du/dt = K u + b, where M and K are the mass
and advection matrices, and b describes the flow on the boundary. This can
be written as a general ODE, du/dt = M^{-1} (K u + b), and this class is
used to evaluate the right-hand side. */
class FE_Evolution : public TimeDependentOperator
{
private:
OperatorHandle M, K;
const Vector &b;
Solver *M_prec;
CGSolver M_solver;
DG_Solver *dg_solver;
mutable Vector z;
public:
FE_Evolution(ParBilinearForm &M_, ParBilinearForm &K_, const Vector &b_,
PrecType prec_type);
virtual void Mult(const Vector &x, Vector &y) const;
virtual void ImplicitSolve(const double dt, const Vector &x, Vector &k);
virtual ~FE_Evolution();
};
int main(int argc, char *argv[])
{
// 1. Initialize MPI and HYPRE.
Mpi::Init();
int num_procs = Mpi::WorldSize();
int myid = Mpi::WorldRank();
Hypre::Init();
// 2. Parse command-line options.
problem = 0;
const char *mesh_file = "../data/periodic-hexagon.mesh";
int ser_ref_levels = 2;
int par_ref_levels = 0;
int order = 3;
bool pa = false;
bool ea = false;
bool fa = false;
const char *device_config = "cpu";
int ode_solver_type = 4;
double t_final = 10.0;
double dt = 0.01;
bool visualization = true;
bool visit = false;
bool paraview = false;
bool adios2 = false;
bool binary = false;
int vis_steps = 5;
#if MFEM_HYPRE_VERSION >= 21800
PrecType prec_type = PrecType::AIR;
#else
PrecType prec_type = PrecType::ILU;
#endif
int precision = 8;
cout.precision(precision);
OptionsParser args(argc, argv);
args.AddOption(&mesh_file, "-m", "--mesh",
"Mesh file to use.");
args.AddOption(&problem, "-p", "--problem",
"Problem setup to use. See options in velocity_function().");
args.AddOption(&ser_ref_levels, "-rs", "--refine-serial",
"Number of times to refine the mesh uniformly in serial.");
args.AddOption(&par_ref_levels, "-rp", "--refine-parallel",
"Number of times to refine the mesh uniformly in parallel.");
args.AddOption(&order, "-o", "--order",
"Order (degree) of the finite elements.");
args.AddOption(&pa, "-pa", "--partial-assembly", "-no-pa",
"--no-partial-assembly", "Enable Partial Assembly.");
args.AddOption(&ea, "-ea", "--element-assembly", "-no-ea",
"--no-element-assembly", "Enable Element Assembly.");
args.AddOption(&fa, "-fa", "--full-assembly", "-no-fa",
"--no-full-assembly", "Enable Full Assembly.");
args.AddOption(&device_config, "-d", "--device",
"Device configuration string, see Device::Configure().");
args.AddOption(&ode_solver_type, "-s", "--ode-solver",
"ODE solver: 1 - Forward Euler,\n\t"
" 2 - RK2 SSP, 3 - RK3 SSP, 4 - RK4, 6 - RK6,\n\t"
" 11 - Backward Euler,\n\t"
" 12 - SDIRK23 (L-stable), 13 - SDIRK33,\n\t"
" 22 - Implicit Midpoint Method,\n\t"
" 23 - SDIRK23 (A-stable), 24 - SDIRK34");
args.AddOption(&t_final, "-tf", "--t-final",
"Final time; start time is 0.");
args.AddOption(&dt, "-dt", "--time-step",
"Time step.");
args.AddOption((int *)&prec_type, "-pt", "--prec-type", "Preconditioner for "
"implicit solves. 0 for ILU, 1 for pAIR-AMG.");
args.AddOption(&visualization, "-vis", "--visualization", "-no-vis",
"--no-visualization",
"Enable or disable GLVis visualization.");
args.AddOption(&visit, "-visit", "--visit-datafiles", "-no-visit",
"--no-visit-datafiles",
"Save data files for VisIt (visit.llnl.gov) visualization.");
args.AddOption(&paraview, "-paraview", "--paraview-datafiles", "-no-paraview",
"--no-paraview-datafiles",
"Save data files for ParaView (paraview.org) visualization.");
args.AddOption(&adios2, "-adios2", "--adios2-streams", "-no-adios2",
"--no-adios2-streams",
"Save data using adios2 streams.");
args.AddOption(&binary, "-binary", "--binary-datafiles", "-ascii",
"--ascii-datafiles",
"Use binary (Sidre) or ascii format for VisIt data files.");
args.AddOption(&vis_steps, "-vs", "--visualization-steps",
"Visualize every n-th timestep.");
args.Parse();
if (!args.Good())
{
if (Mpi::Root())
{
args.PrintUsage(cout);
}
return 1;
}
if (Mpi::Root())
{
args.PrintOptions(cout);
}
Device device(device_config);
if (Mpi::Root()) { device.Print(); }
// 3. Read the serial mesh from the given mesh file on all processors. We can
// handle geometrically periodic meshes in this code.
Mesh *mesh = new Mesh(mesh_file, 1, 1);
int dim = mesh->Dimension();
// 4. Define the ODE solver used for time integration. Several explicit
// Runge-Kutta methods are available.
ODESolver *ode_solver = NULL;
switch (ode_solver_type)
{
// Explicit methods
case 1: ode_solver = new ForwardEulerSolver; break;
case 2: ode_solver = new RK2Solver(1.0); break;
case 3: ode_solver = new RK3SSPSolver; break;
case 4: ode_solver = new RK4Solver; break;
case 6: ode_solver = new RK6Solver; break;
// Implicit (L-stable) methods
case 11: ode_solver = new BackwardEulerSolver; break;
case 12: ode_solver = new SDIRK23Solver(2); break;
case 13: ode_solver = new SDIRK33Solver; break;
// Implicit A-stable methods (not L-stable)
case 22: ode_solver = new ImplicitMidpointSolver; break;
case 23: ode_solver = new SDIRK23Solver; break;
case 24: ode_solver = new SDIRK34Solver; break;
default:
if (Mpi::Root())
{
cout << "Unknown ODE solver type: " << ode_solver_type << '\n';
}
delete mesh;
return 3;
}
// 5. Refine the mesh in serial to increase the resolution. In this example
// we do 'ser_ref_levels' of uniform refinement, where 'ser_ref_levels' is
// a command-line parameter. If the mesh is of NURBS type, we convert it
// to a (piecewise-polynomial) high-order mesh.
for (int lev = 0; lev < ser_ref_levels; lev++)
{
mesh->UniformRefinement();
}
if (mesh->NURBSext)
{
mesh->SetCurvature(max(order, 1));
}
mesh->GetBoundingBox(bb_min, bb_max, max(order, 1));
// 6. Define the parallel mesh by a partitioning of the serial mesh. Refine
// this mesh further in parallel to increase the resolution. Once the
// parallel mesh is defined, the serial mesh can be deleted.
ParMesh *pmesh = new ParMesh(MPI_COMM_WORLD, *mesh);
delete mesh;
for (int lev = 0; lev < par_ref_levels; lev++)
{
pmesh->UniformRefinement();
}
// 7. Define the parallel discontinuous DG finite element space on the
// parallel refined mesh of the given polynomial order.
DG_FECollection fec(order, dim, BasisType::GaussLobatto);
ParFiniteElementSpace *fes = new ParFiniteElementSpace(pmesh, &fec);
HYPRE_BigInt global_vSize = fes->GlobalTrueVSize();
if (Mpi::Root())
{
cout << "Number of unknowns: " << global_vSize << endl;
}
// 8. Set up and assemble the parallel bilinear and linear forms (and the
// parallel hypre matrices) corresponding to the DG discretization. The
// DGTraceIntegrator involves integrals over mesh interior faces.
VectorFunctionCoefficient velocity(dim, velocity_function);
FunctionCoefficient inflow(inflow_function);
FunctionCoefficient u0(u0_function);
ParBilinearForm *m = new ParBilinearForm(fes);
ParBilinearForm *k = new ParBilinearForm(fes);
if (pa)
{
m->SetAssemblyLevel(AssemblyLevel::PARTIAL);
k->SetAssemblyLevel(AssemblyLevel::PARTIAL);
}
else if (ea)
{
m->SetAssemblyLevel(AssemblyLevel::ELEMENT);
k->SetAssemblyLevel(AssemblyLevel::ELEMENT);
}
else if (fa)
{
m->SetAssemblyLevel(AssemblyLevel::FULL);
k->SetAssemblyLevel(AssemblyLevel::FULL);
}
m->AddDomainIntegrator(new MassIntegrator);
constexpr double alpha = -1.0;
k->AddDomainIntegrator(new ConvectionIntegrator(velocity, alpha));
k->AddInteriorFaceIntegrator(
new NonconservativeDGTraceIntegrator(velocity, alpha));
k->AddBdrFaceIntegrator(
new NonconservativeDGTraceIntegrator(velocity, alpha));
ParLinearForm *b = new ParLinearForm(fes);
b->AddBdrFaceIntegrator(
new BoundaryFlowIntegrator(inflow, velocity, alpha));
int skip_zeros = 0;
m->Assemble();
k->Assemble(skip_zeros);
b->Assemble();
m->Finalize();
k->Finalize(skip_zeros);
HypreParVector *B = b->ParallelAssemble();
// 9. Define the initial conditions, save the corresponding grid function to
// a file and (optionally) save data in the VisIt format and initialize
// GLVis visualization.
ParGridFunction *u = new ParGridFunction(fes);
u->ProjectCoefficient(u0);
HypreParVector *U = u->GetTrueDofs();
{
ostringstream mesh_name, sol_name;
mesh_name << "ex9-mesh." << setfill('0') << setw(6) << myid;
sol_name << "ex9-init." << setfill('0') << setw(6) << myid;
ofstream omesh(mesh_name.str().c_str());
omesh.precision(precision);
pmesh->Print(omesh);
ofstream osol(sol_name.str().c_str());
osol.precision(precision);
u->Save(osol);
}
// Create data collection for solution output: either VisItDataCollection for
// ascii data files, or SidreDataCollection for binary data files.
DataCollection *dc = NULL;
if (visit)
{
if (binary)
{
#ifdef MFEM_USE_SIDRE
dc = new SidreDataCollection("Example9-Parallel", pmesh);
#else
MFEM_ABORT("Must build with MFEM_USE_SIDRE=YES for binary output.");
#endif
}
else
{
dc = new VisItDataCollection("Example9-Parallel", pmesh);
dc->SetPrecision(precision);
// To save the mesh using MFEM's parallel mesh format:
// dc->SetFormat(DataCollection::PARALLEL_FORMAT);
}
dc->RegisterField("solution", u);
dc->SetCycle(0);
dc->SetTime(0.0);
dc->Save();
}
ParaViewDataCollection *pd = NULL;
if (paraview)
{
pd = new ParaViewDataCollection("Example9P", pmesh);
pd->SetPrefixPath("ParaView");
pd->RegisterField("solution", u);
pd->SetLevelsOfDetail(order);
pd->SetDataFormat(VTKFormat::BINARY);
pd->SetHighOrderOutput(true);
pd->SetCycle(0);
pd->SetTime(0.0);
pd->Save();
}
// Optionally output a BP (binary pack) file using ADIOS2. This can be
// visualized with the ParaView VTX reader.
#ifdef MFEM_USE_ADIOS2
ADIOS2DataCollection *adios2_dc = NULL;
if (adios2)
{
std::string postfix(mesh_file);
postfix.erase(0, std::string("../data/").size() );
postfix += "_o" + std::to_string(order);
const std::string collection_name = "ex9-p-" + postfix + ".bp";
adios2_dc = new ADIOS2DataCollection(MPI_COMM_WORLD, collection_name, pmesh);
// output data substreams are half the number of mpi processes
adios2_dc->SetParameter("SubStreams", std::to_string(num_procs/2) );
// adios2_dc->SetLevelsOfDetail(2);
adios2_dc->RegisterField("solution", u);
adios2_dc->SetCycle(0);
adios2_dc->SetTime(0.0);
adios2_dc->Save();
}
#endif
socketstream sout;
if (visualization)
{
char vishost[] = "localhost";
int visport = 19916;
sout.open(vishost, visport);
if (!sout)
{
if (Mpi::Root())
cout << "Unable to connect to GLVis server at "
<< vishost << ':' << visport << endl;
visualization = false;
if (Mpi::Root())
{
cout << "GLVis visualization disabled.\n";
}
}
else
{
sout << "parallel " << num_procs << " " << myid << "\n";
sout.precision(precision);
sout << "solution\n" << *pmesh << *u;
sout << "pause\n";
sout << flush;
if (Mpi::Root())
cout << "GLVis visualization paused."
<< " Press space (in the GLVis window) to resume it.\n";
}
}
// 10. Define the time-dependent evolution operator describing the ODE
// right-hand side, and perform time-integration (looping over the time
// iterations, ti, with a time-step dt).
FE_Evolution adv(*m, *k, *B, prec_type);
double t = 0.0;
adv.SetTime(t);
ode_solver->Init(adv);
bool done = false;
for (int ti = 0; !done; )
{
double dt_real = min(dt, t_final - t);
ode_solver->Step(*U, t, dt_real);
ti++;
done = (t >= t_final - 1e-8*dt);
if (done || ti % vis_steps == 0)
{
if (Mpi::Root())
{
cout << "time step: " << ti << ", time: " << t << endl;
}
// 11. Extract the parallel grid function corresponding to the finite
// element approximation U (the local solution on each processor).
*u = *U;
if (visualization)
{
sout << "parallel " << num_procs << " " << myid << "\n";
sout << "solution\n" << *pmesh << *u << flush;
}
if (visit)
{
dc->SetCycle(ti);
dc->SetTime(t);
dc->Save();
}
if (paraview)
{
pd->SetCycle(ti);
pd->SetTime(t);
pd->Save();
}
#ifdef MFEM_USE_ADIOS2
// transient solutions can be visualized with ParaView
if (adios2)
{
adios2_dc->SetCycle(ti);
adios2_dc->SetTime(t);
adios2_dc->Save();
}
#endif
}
}
// 12. Save the final solution in parallel. This output can be viewed later
// using GLVis: "glvis -np <np> -m ex9-mesh -g ex9-final".
{
*u = *U;
ostringstream sol_name;
sol_name << "ex9-final." << setfill('0') << setw(6) << myid;
ofstream osol(sol_name.str().c_str());
osol.precision(precision);
u->Save(osol);
}
// 13. Free the used memory.
delete U;
delete u;
delete B;
delete b;
delete k;
delete m;
delete fes;
delete pmesh;
delete ode_solver;
delete pd;
#ifdef MFEM_USE_ADIOS2
if (adios2)
{
delete adios2_dc;
}
#endif
delete dc;
return 0;
}
// Implementation of class FE_Evolution
FE_Evolution::FE_Evolution(ParBilinearForm &M_, ParBilinearForm &K_,
const Vector &b_, PrecType prec_type)
: TimeDependentOperator(M_.Height()), b(b_),
M_solver(M_.ParFESpace()->GetComm()),
z(M_.Height())
{
if (M_.GetAssemblyLevel()==AssemblyLevel::LEGACY)
{
M.Reset(M_.ParallelAssemble(), true);
K.Reset(K_.ParallelAssemble(), true);
}
else
{
M.Reset(&M_, false);
K.Reset(&K_, false);
}
M_solver.SetOperator(*M);
Array<int> ess_tdof_list;
if (M_.GetAssemblyLevel()==AssemblyLevel::LEGACY)
{
HypreParMatrix &M_mat = *M.As<HypreParMatrix>();
HypreParMatrix &K_mat = *K.As<HypreParMatrix>();
HypreSmoother *hypre_prec = new HypreSmoother(M_mat, HypreSmoother::Jacobi);
M_prec = hypre_prec;
dg_solver = new DG_Solver(M_mat, K_mat, *M_.FESpace(), prec_type);
}
else
{
M_prec = new OperatorJacobiSmoother(M_, ess_tdof_list);
dg_solver = NULL;
}
M_solver.SetPreconditioner(*M_prec);
M_solver.iterative_mode = false;
M_solver.SetRelTol(1e-9);
M_solver.SetAbsTol(0.0);
M_solver.SetMaxIter(100);
M_solver.SetPrintLevel(0);
}
// Solve the equation:
// u_t = M^{-1}(Ku + b),
// by solving associated linear system
// (M - dt*K) d = K*u + b
void FE_Evolution::ImplicitSolve(const double dt, const Vector &x, Vector &k)
{
K->Mult(x, z);
z += b;
dg_solver->SetTimeStep(dt);
dg_solver->Mult(z, k);
}
void FE_Evolution::Mult(const Vector &x, Vector &y) const
{
// y = M^{-1} (K x + b)
K->Mult(x, z);
z += b;
M_solver.Mult(z, y);
}
FE_Evolution::~FE_Evolution()
{
delete M_prec;
delete dg_solver;
}
// Velocity coefficient
void velocity_function(const Vector &x, Vector &v)
{
int dim = x.Size();
// map to the reference [-1,1] domain
Vector X(dim);
for (int i = 0; i < dim; i++)
{
double center = (bb_min[i] + bb_max[i]) * 0.5;
X(i) = 2 * (x(i) - center) / (bb_max[i] - bb_min[i]);
}
switch (problem)
{
case 0:
{
// Translations in 1D, 2D, and 3D
switch (dim)
{
case 1: v(0) = 1.0; break;
case 2: v(0) = sqrt(2./3.); v(1) = sqrt(1./3.); break;
case 3: v(0) = sqrt(3./6.); v(1) = sqrt(2./6.); v(2) = sqrt(1./6.);
break;
}
break;
}
case 1:
case 2:
{
// Clockwise rotation in 2D around the origin
const double w = M_PI/2;
switch (dim)
{
case 1: v(0) = 1.0; break;
case 2: v(0) = w*X(1); v(1) = -w*X(0); break;
case 3: v(0) = w*X(1); v(1) = -w*X(0); v(2) = 0.0; break;
}
break;
}
case 3:
{
// Clockwise twisting rotation in 2D around the origin
const double w = M_PI/2;
double d = max((X(0)+1.)*(1.-X(0)),0.) * max((X(1)+1.)*(1.-X(1)),0.);
d = d*d;
switch (dim)
{
case 1: v(0) = 1.0; break;
case 2: v(0) = d*w*X(1); v(1) = -d*w*X(0); break;
case 3: v(0) = d*w*X(1); v(1) = -d*w*X(0); v(2) = 0.0; break;
}
break;
}
}
}
// Initial condition
double u0_function(const Vector &x)
{
int dim = x.Size();
// map to the reference [-1,1] domain
Vector X(dim);
for (int i = 0; i < dim; i++)
{
double center = (bb_min[i] + bb_max[i]) * 0.5;
X(i) = 2 * (x(i) - center) / (bb_max[i] - bb_min[i]);
}
switch (problem)
{
case 0:
case 1:
{
switch (dim)
{
case 1:
return exp(-40.*pow(X(0)-0.5,2));
case 2:
case 3:
{
double rx = 0.45, ry = 0.25, cx = 0., cy = -0.2, w = 10.;
if (dim == 3)
{
const double s = (1. + 0.25*cos(2*M_PI*X(2)));
rx *= s;
ry *= s;
}
return ( erfc(w*(X(0)-cx-rx))*erfc(-w*(X(0)-cx+rx)) *
erfc(w*(X(1)-cy-ry))*erfc(-w*(X(1)-cy+ry)) )/16;
}
}
}
case 2:
{
double x_ = X(0), y_ = X(1), rho, phi;
rho = hypot(x_, y_);
phi = atan2(y_, x_);
return pow(sin(M_PI*rho),2)*sin(3*phi);
}
case 3:
{
const double f = M_PI;
return sin(f*X(0))*sin(f*X(1));
}
}
return 0.0;
}
// Inflow boundary condition (zero for the problems considered in this example)
double inflow_function(const Vector &x)
{
switch (problem)
{
case 0:
case 1:
case 2:
case 3: return 0.0;
}
return 0.0;
}