// MFEM Example 1 // // Compile with: make ex23 // // Sample runs: ex23 -m ../data/line-space-time.mesh // ex23 -m ../data/square-space-time.mesh // ex23 -m ../data/cube-space-time.mesh // // Description: This example code demonstrates the use of MFEM to define a // simple space-time finite element discretization of the Heat equation problem // d_t u -Delta_x u = 1 with homogeneous inital and Dirichlet boundary conditions. // Specifically, we discretize using a conforming FE space of the specified // order. The space-time FEM used can be found under // https://doi.org/10.1515/cmam-2015-0026 // // The example highlights the use of mesh refinement, finite // element grid functions, as well as linear and bilinear forms // corresponding to the left-hand side and right-hand side of the // discrete linear system. We also cover the explicit elimination // of essential boundary conditions, static condensation, and the // optional connection to the GLVis tool for visualization. #include "mfem.hpp" #include #include using namespace std; using namespace mfem; int main(int argc, char *argv[]) { // 1. Parse command-line options. const char *mesh_file = "../data/square-space-time.mesh"; int order = 1; bool static_cond = false; bool visualization = 1; OptionsParser args(argc, argv); args.AddOption(&mesh_file, "-m", "--mesh", "Mesh file to use."); args.AddOption(&order, "-o", "--order", "Finite element order (polynomial degree) or -1 for" " isoparametric space."); args.AddOption(&static_cond, "-sc", "--static-condensation", "-no-sc", "--no-static-condensation", "Enable static condensation."); args.AddOption(&visualization, "-vis", "--visualization", "-no-vis", "--no-visualization", "Enable or disable GLVis visualization."); args.Parse(); if (!args.Good()) { args.PrintUsage(cout); return 1; } args.PrintOptions(cout); // 2. Read the mesh from the given mesh file. We can handle triangular, // quadrilateral, tetrahedral, hexahedral, surface and volume meshes with // the same code. Mesh *mesh = new Mesh(mesh_file, 1, 1); int dim = mesh->Dimension(); // 3. Refine the mesh to increase the resolution. In this example we do // 'ref_levels' of uniform refinement. We choose 'ref_levels' to be the // largest number that gives a final mesh with no more than 50,000 // elements. { int ref_levels = (int)floor(log(50000./mesh->GetNE())/log(2.)/dim); for (int l = 0; l < ref_levels; l++) { mesh->UniformRefinement(); } } // 4. Define a finite element space on the mesh. Here we use continuous // Lagrange finite elements of the specified order. If order < 1, we // instead use an isoparametric/isogeometric space. FiniteElementCollection *fec; if (order > 0) { fec = new H1_FECollection(order, dim); } else { fec = new H1_FECollection(order = 1, dim); } FiniteElementSpace *fespace = new FiniteElementSpace(mesh, fec); cout << "Number of finite element unknowns: " << fespace->GetTrueVSize() << endl; // 5. Determine the list of true (i.e. conforming) essential boundary dofs. // In this example, the boundary conditions are defined by marking all // but the last boundary attributes from the mesh as essential (Dirichlet) // and converting them to a list of true dofs. We assume that the last // boundary attribute corresponds to the top of the space-time cylinder. Array ess_tdof_list; if (mesh->bdr_attributes.Size()) { Array ess_bdr(mesh->bdr_attributes.Max()); ess_bdr = 1; ess_bdr.Last() = 0; fespace->GetEssentialTrueDofs(ess_bdr, ess_tdof_list); } // 6. Set up the linear form b(.) which corresponds to the right-hand side of // the FEM linear system, which in this case is (1,phi_i) where phi_i are // the basis functions in the finite element fespace. LinearForm *b = new LinearForm(fespace); ConstantCoefficient one(1.0); b->AddDomainIntegrator(new DomainLFIntegrator(one)); b->Assemble(); // 7. Define the solution vector x as a finite element grid function // corresponding to fespace. Initialize x with initial guess of zero, // which satisfies the boundary conditions. GridFunction x(fespace); x = 0.0; // 8. Set up the bilinear form a(.,.) on the finite element space // corresponding to the Heat equation operator d_t-Delta_x, by adding the // HeatEquation domain integrator. BilinearForm *a = new BilinearForm(fespace); a->AddDomainIntegrator(new HeatEquationIntegrator(one)); // 9. Assemble the bilinear form and the corresponding linear system, // applying any necessary transformations such as: eliminating boundary // conditions, applying conforming constraints for non-conforming AMR, // static condensation, etc. if (static_cond) { a->EnableStaticCondensation(); } a->Assemble(); SparseMatrix A; Vector B, X; a->FormLinearSystem(ess_tdof_list, x, *b, A, X, B); cout << "Size of linear system: " << A.Height() << endl; #ifndef MFEM_USE_SUITESPARSE // 10. Define a simple symmetric Gauss-Seidel preconditioner and use it to // solve the system A X = B with GMRES without restarts. GSSmoother M(A); GMRES(A, M, B, X, 1, 200, 200, 1e-8, 0.0); #else // 10. If MFEM was compiled with SuiteSparse, use UMFPACK to solve the system. UMFPackSolver umf_solver; umf_solver.Control[UMFPACK_ORDERING] = UMFPACK_ORDERING_METIS; umf_solver.SetOperator(A); umf_solver.Mult(B, X); #endif // 11. Recover the solution as a finite element grid function. a->RecoverFEMSolution(X, *b, x); // 12. Save the refined mesh and the solution. This output can be viewed later // using GLVis: "glvis -m refined.mesh -g sol.gf". ofstream mesh_ofs("refined.mesh"); mesh_ofs.precision(8); mesh->Print(mesh_ofs); ofstream sol_ofs("sol.gf"); sol_ofs.precision(8); x.Save(sol_ofs); // 13. Send the solution by socket to a GLVis server. if (visualization && dim < 4) { char vishost[] = "localhost"; int visport = 19916; socketstream sol_sock(vishost, visport); sol_sock.precision(8); sol_sock << "solution\n" << *mesh << x << flush; } // 14. Free the used memory. delete a; delete b; delete fespace; if (order > 0) { delete fec; } delete mesh; return 0; }