// MFEM Example 9 Continuous - Parallel Version // // Author: Madison Sheridan // Created: 05/25/2022 // // Based on Example 9p // // Compile with: make ex9p-continuous // // Sample runs: // mpirun -np 4 ex9p-continuous -m ../data/periodic-segment.mesh -p 0 -dt 0.005 // mpirun -np 4 ex9p-continuous -m ../data/periodic-square.mesh -p 0 -dt 0.01 // mpirun -np 4 ex9p-continuous -m ../data/periodic-hexagon.mesh -p 0 -dt 0.01 // mpirun -np 4 ex9p-continuous -m ../data/periodic-square.mesh -p 1 -dt 0.005 -tf 9 // mpirun -np 4 ex9p-continuous -m ../data/periodic-hexagon.mesh -p 1 -dt 0.005 -tf 9 // mpirun -np 4 ex9p-continuous -m ../data/amr-quad.mesh -p 1 -rp 1 -dt 0.002 -tf 9 // mpirun -np 4 ex9p-continuous -m ../data/amr-quad.mesh -p 1 -rp 1 -dt 0.02 -s 13 -tf 9 // mpirun -np 4 ex9p-continuous -m ../data/star-q3.mesh -p 1 -rp 1 -dt 0.004 -tf 9 // mpirun -np 4 ex9p-continuous -m ../data/star-mixed.mesh -p 1 -rp 1 -dt 0.004 -tf 9 // mpirun -np 4 ex9p-continuous -m ../data/disc-nurbs.mesh -p 1 -rp 1 -dt 0.005 -tf 9 // mpirun -np 4 ex9p-continuous -m ../data/disc-nurbs.mesh -p 2 -rp 1 -dt 0.005 -tf 9 // mpirun -np 4 ex9p-continuous -m ../data/periodic-square.mesh -p 3 -rp 2 -dt 0.0025 -tf 9 -vs 20 // mpirun -np 4 ex9p-continuous -m ../data/periodic-cube.mesh -p 0 -o 2 -rp 1 -dt 0.01 -tf 8 // mpirun -np 4 ex9p-continuous -m ../data/periodic-square.msh -p 0 -rs 2 -dt 0.005 -tf 2 // mpirun -np 4 ex9p-continuous -m ../data/periodic-cube.msh -p 0 -rs 1 -o 2 -tf 2 // mpirun -np 3 ex9p-continuous -m ../data/amr-hex.mesh -p 1 -rs 1 -rp 0 -dt 0.005 -tf 0.5 // // Device sample runs: // mpirun -np 4 ex9p-continuous -pa // mpirun -np 4 ex9p-continuous -ea // mpirun -np 4 ex9p-continuous -fa // mpirun -np 4 ex9p-continuous -pa -m ../data/periodic-cube.mesh // mpirun -np 4 ex9p-continuous -pa -m ../data/periodic-cube.mesh -d cuda // mpirun -np 4 ex9p-continuous -ea -m ../data/periodic-cube.mesh -d cuda // mpirun -np 4 ex9p-continuous -fa -m ../data/periodic-cube.mesh -d cuda // mpirun -np 4 ex9p-continuous -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 Continuous Galerkin // bilinear forms in MFEM (face integrators), the use of 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 #include 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(&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 /** A time-dependent operator for the right-hand side of the ODE. The CG weak form of du/dt = -v.grad(u) is M du/dt = (D + K) u, where M and K are the mass and advection matrices, and D is the artificial viscosity matrix as described in Guermond/Popov 2016. This can be written as a general ODE, du/dt = M^{-1} K u, and this class is used to evaluate the right-hand side. */ class FE_Evolution : public TimeDependentOperator { private: OperatorHandle M, K; ParBilinearForm *D_form; const Vector &b; Solver *M_prec; CGSolver M_solver; const SparseMatrix &K_mat; mutable SparseMatrix *dij_matrix; HypreParMatrix *D; Array K_smap; mutable Vector z; const Vector M_lumped; ParFiniteElementSpace &pfes; public: FE_Evolution(ParBilinearForm &M_, ParBilinearForm &K_, const Vector &b_, const Vector &Mlump, PrecType prec_type); /** FE_Evolution::build_dij_matrix Builds dij_matrix used in the low order approximation, which is based on Guermond/Popov 2016. */ void build_dij_matrix(const Vector &U, const VectorFunctionCoefficient &velocity) ; void ApplyDijMatrix(ParGridFunction &u, Vector &du) const; 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 = 3; int par_ref_levels = 0; int order = 1; bool pa = false; bool ea = false; bool fa = false; const char *device_config = "cpu"; int ode_solver_type = 2; 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 = 2; #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(¶view, "-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 H1 finite element space on the // parallel refined mesh of the given polynomial order. H1_FECollection fec(order, dim); ParFiniteElementSpace *fes = new ParFiniteElementSpace(pmesh, &fec); HYPRE_BigInt global_vSize = fes->GlobalTrueVSize(); if (Mpi::Root()) { cout << "Number of unknowns: " << global_vSize << endl; } // Array ess_tdof_list; // if (pmesh->bdr_attributes.Size()) // { // Array ess_bdr(pmesh->bdr_attributes.Max()); // ess_bdr = 1; // fes->GetEssentialTrueDofs(ess_bdr, ess_tdof_list); // } // 8. Set up and assemble the parallel bilinear and linear forms (and the // parallel hypre matrices) corresponding to the H1 discretization. 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); m->AddDomainIntegrator(new LumpedIntegrator(new MassIntegrator)); constexpr double alpha = -1.0; k->AddDomainIntegrator(new ConvectionIntegrator(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); Vector *Mlump = new Vector; m->SpMat().GetDiag(*Mlump); HypreParMatrix *K = k->ParallelAssemble(); 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-Continuous", pmesh); #else MFEM_ABORT("Must build with MFEM_USE_SIDRE=YES for binary output."); #endif } else { dc = new VisItDataCollection("Example9-Parallel-Continuous", 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-Continuous", 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 = "ex9p-continuous-" + 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); } // 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, *Mlump, prec_type); double t = 0.0; adv.SetTime(t); ode_solver->Init(adv); bool done = false; for (int ti = 0; !done; ) { // Build new D matrix since this matrix is time dependent adv.build_dij_matrix(*U, velocity); 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; // Synchronizes MPI processes. 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 -m ex9-mesh -g ex9-final". { *u = *U; cout << *u << endl; ostringstream sol_name; sol_name << "ex9p-continuous-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 k; delete m; delete b; 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_, const Vector &Mlump, PrecType prec_type) : TimeDependentOperator(M_.Height()), b(b_), pfes(*(M_.ParFESpace())), M_solver(M_.ParFESpace()->GetComm()), z(M_.Height()), M_lumped(Mlump), dij_matrix(&K_.SpMat()), D_form(&K_), K_mat(K_.SpMat()), K_smap() { 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 ess_tdof_list; if (M_.GetAssemblyLevel()==AssemblyLevel::LEGACY) { HypreParMatrix &M_mat = *M.As(); HypreParMatrix &K_mat = *K.As(); HypreSmoother *hypre_prec = new HypreSmoother(M_mat, HypreSmoother::Jacobi); M_prec = hypre_prec; } else { M_prec = new OperatorJacobiSmoother(M_, ess_tdof_list); } 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); // Assuming K is finalized. (From extrapolator.) // K_smap is used later to symmetrically form dij_matrix const int *I = K_mat.GetI(), *J = K_mat.GetJ(), n = K_mat.Size(); K_smap.SetSize(I[n]); for (int row = 0, j = 0; row < n; row++) { for (int end = I[row+1]; j < end; j++) { int col = J[j]; // Find the offset, _j, of the (col,row) entry and store it in smap[j]. for (int _j = I[col], _end = I[col+1]; true; _j++) { MFEM_VERIFY(_j != _end, "Can't find the symmetric entry!"); if (J[_j] == row) { K_smap[j] = _j; break; } } } } } // TODO: Implement an ImplicitSolve function // Solve the equation: // u_t = M^{-1}(Ku), // by solving associated linear system // (M - dt*K) d = K*u void FE_Evolution::ImplicitSolve(const double dt, const Vector &x, Vector &k) { K->Mult(x, z); } void FE_Evolution::build_dij_matrix(const Vector &U, const VectorFunctionCoefficient &velocity) { cout << "Test 3\n"; const int *I = K_mat.HostReadI(), *J = K_mat.HostReadJ(), n = K_mat.Size(); const double *K_data = K_mat.HostReadData(); double *D_data = dij_matrix->HostReadWriteData(); dij_matrix->HostReadWriteI(); dij_matrix->HostReadWriteJ(); cout << "Test 4\n"; for (int i = 0, k = 0; i < n; i++) { double rowsum = 0.; for (int end = I[i+1]; k < end; k++) { int j = J[k]; double kij = K_data[k]; double kji = K_data[K_smap[k]]; double dij = fmax(abs(kij),abs(kji)); D_data[k] = dij; D_data[K_smap[k]] = dij; if (i != j) { rowsum += dij; } } (*dij_matrix)(i,i) = -rowsum; } cout << "Test 1\n"; D = D_form->ParallelAssemble(dij_matrix); cout << "Test 5\n"; /* Check that columns sum to 0. */ // Vector test_v(U.Size()); // test_v = 1.; // cout << "Pre Result: " << test_v[2] << endl; // D.MultTranspose(test_v, test_v); // cout << "Post Result: " << test_v[2] << endl; } /* Deprecated now that ParallelAssemble() is implemented. */ // void FE_Evolution::ApplyDijMatrix(ParGridFunction &u, Vector &du) const // { // const int s = u.Size(); // const int *I = D.HostReadI(), *J = D.HostReadJ(); // const double *D_data = D.HostReadData(); // // u.ExchangeFaceNbrData(); // const Vector &u_np = u.FaceNbrData(); // // for (int i = 0; i < s; i++) // { // du(i) = 0.0; // for (int k = I[i]; k < I[i + 1]; k++) // { // int j = J[k]; // double u_j = (j < s) ? u(j) : u_np[j - s]; // double d_ij = D_data[k]; // du(i) += d_ij * u_j; // } // } // } void FE_Evolution::Mult(const Vector &x, Vector &y) const { // y = Ml^{-1} ((D + K) x) // x = u /* Deprecated now that ParallelAssemble() is implemented. */ // ParGridFunction u_gf(&pfes); // u_gf = x; // ApplyDijMatrix(u_gf, z); D->Mult(x, z); z += b; // Neumann BCs Vector rhs(y.Size()); K->Mult(x, rhs); z+= rhs; // M_solver.Mult(z, y); const int s = y.Size(); for (int i = 0; i < s; i++) { y(i) = z(i) / M_lumped(i); } } FE_Evolution::~FE_Evolution() { delete M_prec; } // 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; }