コード例 #1
0
ファイル: main.cpp プロジェクト: certik/hermes-examples
int main(int argc, char* argv[])
{
  // Load the mesh.
  Mesh mesh_whole_domain, mesh_with_hole;
  Hermes::vector<Mesh*> meshes (&mesh_whole_domain, &mesh_with_hole);
  MeshReaderH2DXML mloader;
  mloader.load("domain.xml", meshes);

  // Temperature mesh: Initial uniform mesh refinements in graphite.
  meshes[0]->refine_by_criterion(element_in_graphite, INIT_REF_NUM_TEMPERATURE_GRAPHITE);

  // Temperature mesh: Initial uniform mesh refinements in fluid.
  meshes[0]->refine_by_criterion(element_in_fluid, INIT_REF_NUM_TEMPERATURE_FLUID);

  // Fluid mesh: Initial uniform mesh refinements.
  for(int i = 0; i < INIT_REF_NUM_FLUID; i++)
    meshes[1]->refine_all_elements();

  // Initial refinements towards boundary of graphite.
  for(unsigned int meshes_i = 0; meshes_i < meshes.size(); meshes_i++)
    meshes[meshes_i]->refine_towards_boundary("Inner Wall", INIT_REF_NUM_BDY_GRAPHITE);

  // Initial refinements towards the top and bottom edges.
  for(unsigned int meshes_i = 0; meshes_i < meshes.size(); meshes_i++)
    meshes[meshes_i]->refine_towards_boundary("Outer Wall", INIT_REF_NUM_BDY_WALL);

  /* View both meshes. */
  MeshView m1("Mesh for temperature"), m2("Mesh for fluid");
  m1.show(&mesh_whole_domain);
  m2.show(&mesh_with_hole);

  // Initialize boundary conditions.
  EssentialBCNonConst bc_inlet_vel_x("Inlet", VEL_INLET, H, STARTUP_TIME);
  DefaultEssentialBCConst<double> bc_other_vel_x(Hermes::vector<std::string>("Outer Wall", "Inner Wall"), 0.0);
  EssentialBCs<double> bcs_vel_x(Hermes::vector<EssentialBoundaryCondition<double> *>(&bc_inlet_vel_x, &bc_other_vel_x));
  DefaultEssentialBCConst<double> bc_vel_y(Hermes::vector<std::string>("Inlet", "Outer Wall", "Inner Wall"), 0.0);
  EssentialBCs<double> bcs_vel_y(&bc_vel_y);
  EssentialBCs<double> bcs_pressure;
  DefaultEssentialBCConst<double> bc_temperature(Hermes::vector<std::string>("Outer Wall", "Inlet"), 20.0);
  EssentialBCs<double> bcs_temperature(&bc_temperature);

  // Spaces for velocity components, pressure and temperature.
  H1Space<double> xvel_space(&mesh_with_hole, &bcs_vel_x, P_INIT_VEL);
  H1Space<double> yvel_space(&mesh_with_hole, &bcs_vel_y, P_INIT_VEL);
#ifdef PRESSURE_IN_L2
  L2Space<double> p_space(&mesh_with_hole, P_INIT_PRESSURE);
#else
  H1Space<double> p_space(&mesh_with_hole, &bcs_pressure, P_INIT_PRESSURE);
#endif
  H1Space<double> temperature_space(&mesh_whole_domain, &bcs_temperature, P_INIT_TEMPERATURE);
  Hermes::vector<Space<double> *> all_spaces(&xvel_space, 
      &yvel_space, &p_space, &temperature_space);
  Hermes::vector<const Space<double> *> all_spaces_const(&xvel_space, 
      &yvel_space, &p_space, &temperature_space);

  // Calculate and report the number of degrees of freedom.
  int ndof = Space<double>::get_num_dofs(Hermes::vector<const Space<double> *>(&xvel_space, 
      &yvel_space, &p_space, &temperature_space));
  info("ndof = %d.", ndof);

  // Define projection norms.
  ProjNormType vel_proj_norm = HERMES_H1_NORM;
#ifdef PRESSURE_IN_L2
  ProjNormType p_proj_norm = HERMES_L2_NORM;
#else
  ProjNormType p_proj_norm = HERMES_H1_NORM;
#endif
  ProjNormType temperature_proj_norm = HERMES_H1_NORM;
  Hermes::vector<ProjNormType> all_proj_norms = Hermes::vector<ProjNormType>(vel_proj_norm, 
      vel_proj_norm, p_proj_norm, temperature_proj_norm);

  // Initial conditions and such.
  info("Setting initial conditions.");
  ZeroSolution xvel_prev_time(&mesh_with_hole), yvel_prev_time(&mesh_with_hole), p_prev_time(&mesh_with_hole);
  CustomInitialConditionTemperature temperature_init_cond(&mesh_whole_domain, HOLE_MID_X, HOLE_MID_Y, 
      0.5*OBSTACLE_DIAMETER, TEMPERATURE_INIT_FLUID, TEMPERATURE_INIT_GRAPHITE); 
  Solution<double> temperature_prev_time;
  Hermes::vector<Solution<double> *> all_solutions = Hermes::vector<Solution<double> *>(&xvel_prev_time, 
      &yvel_prev_time, &p_prev_time, &temperature_prev_time);
  Hermes::vector<MeshFunction<double> *> all_meshfns = Hermes::vector<MeshFunction<double> *>(&xvel_prev_time, 
      &yvel_prev_time, &p_prev_time, &temperature_init_cond);

  // Project all initial conditions on their FE spaces to obtain aninitial
  // coefficient vector for the Newton's method. We use local projection
  // to avoid oscillations in temperature on the graphite-fluid interface
  // FIXME - currently the LocalProjection only does the lowest-order part (linear
  // interpolation) at the moment. Higher-order part needs to be added.
  double* coeff_vec = new double[ndof];
  info("Projecting initial condition to obtain initial vector for the Newton's method.");
  //OGProjection<double>::project_global(all_spaces, all_meshfns, coeff_vec, matrix_solver, all_proj_norms);
  LocalProjection<double>::project_local(all_spaces_const, all_meshfns, coeff_vec, matrix_solver, all_proj_norms);

  // Translate the solution vector back to Solutions. This is needed to replace
  // the discontinuous initial condition for temperature_prev_time with its projection.
  Solution<double>::vector_to_solutions(coeff_vec, all_spaces_const, all_solutions);

  // Calculate Reynolds number.
  double reynolds_number = VEL_INLET * OBSTACLE_DIAMETER / KINEMATIC_VISCOSITY_FLUID;
  info("RE = %g", reynolds_number);
  if (reynolds_number < 1e-8) error("Re == 0 will not work - the equations use 1/Re.");

  // Initialize weak formulation.
  CustomWeakFormHeatAndFlow wf(STOKES, reynolds_number, time_step, &xvel_prev_time, &yvel_prev_time, &temperature_prev_time, 
      HEAT_SOURCE_GRAPHITE, SPECIFIC_HEAT_GRAPHITE, SPECIFIC_HEAT_FLUID, RHO_GRAPHITE, RHO_FLUID, 
      THERMAL_CONDUCTIVITY_GRAPHITE, THERMAL_CONDUCTIVITY_FLUID, SIMPLE_TEMPERATURE_ADVECTION);
  
  // Initialize the FE problem.
  DiscreteProblem<double> dp(&wf, all_spaces_const);

  // Initialize the Newton solver.
  NewtonSolver<double> newton(&dp, matrix_solver);

  // Initialize views.
  Views::VectorView vview("velocity [m/s]", new Views::WinGeom(0, 0, 700, 360));
  Views::ScalarView pview("pressure [Pa]", new Views::WinGeom(0, 415, 700, 350));
  Views::ScalarView tempview("temperature [C]", new Views::WinGeom(0, 795, 700, 350));
  //vview.set_min_max_range(0, 0.5);
  vview.fix_scale_width(80);
  //pview.set_min_max_range(-0.9, 1.0);
  pview.fix_scale_width(80);
  pview.show_mesh(false);
  tempview.fix_scale_width(80);
  tempview.show_mesh(false);

  // Time-stepping loop:
  char title[100];
  int num_time_steps = T_FINAL / time_step;
  double current_time = 0.0;
  for (int ts = 1; ts <= num_time_steps; ts++)
  {
    current_time += time_step;
    info("---- Time step %d, time = %g:", ts, current_time);

    // Update time-dependent essential BCs.
    if (current_time <= STARTUP_TIME) 
    {
      info("Updating time-dependent essential BC.");
      Space<double>::update_essential_bc_values(Hermes::vector<Space<double> *>(&xvel_space, &yvel_space, &p_space, 
                                                &temperature_space), current_time);
    }

    // Perform Newton's iteration.
    info("Solving nonlinear problem:");
    bool verbose = true;
    // Perform Newton's iteration and translate the resulting coefficient vector into previous time level solutions.
    newton.set_verbose_output(verbose);
    try
    {
      newton.solve(coeff_vec, NEWTON_TOL, NEWTON_MAX_ITER);
    }
    catch(Hermes::Exceptions::Exception e)
    {
      e.printMsg();
      error("Newton's iteration failed.");
    };
    {
      Hermes::vector<Solution<double> *> tmp(&xvel_prev_time, &yvel_prev_time, &p_prev_time, &temperature_prev_time);
      Solution<double>::vector_to_solutions(newton.get_sln_vector(), Hermes::vector<const Space<double> *>(&xvel_space, 
          &yvel_space, &p_space, &temperature_space), tmp);
    }
    
    // Show the solution at the end of time step.
    sprintf(title, "Velocity [m/s], time %g s", current_time);
    vview.set_title(title);
    vview.show(&xvel_prev_time, &yvel_prev_time);
    sprintf(title, "Pressure [Pa], time %g s", current_time);
    pview.set_title(title);
    pview.show(&p_prev_time);
    sprintf(title, "Temperature [C], time %g s", current_time);
    tempview.set_title(title);
    tempview.show(&temperature_prev_time,  Views::HERMES_EPS_HIGH);
  }

  delete [] coeff_vec;

  // Wait for all views to be closed.
  Views::View::wait();
  return 0;
}
コード例 #2
0
ファイル: main.cpp プロジェクト: fauzisd/hermes-examples
int main(int argc, char* argv[])
{
  // Load the mesh.
  Mesh mesh;
  MeshReaderH2D mloader;
  mloader.load("domain.mesh", &mesh);

  // Initial mesh refinements.
  mesh.refine_all_elements();
  mesh.refine_towards_boundary(BDY_OBSTACLE, 4, false);
  mesh.refine_towards_boundary(BDY_TOP, 4, true);     // '4' is the number of levels,
  mesh.refine_towards_boundary(BDY_BOTTOM, 4, true);  // 'true' stands for anisotropic refinements.

  // Initialize boundary conditions.
  EssentialBCNonConst bc_left_vel_x(BDY_LEFT, VEL_INLET, H, STARTUP_TIME);
  DefaultEssentialBCConst<double> bc_other_vel_x(Hermes::vector<std::string>(BDY_BOTTOM, BDY_TOP, BDY_OBSTACLE), 0.0);
  EssentialBCs<double> bcs_vel_x(Hermes::vector<EssentialBoundaryCondition<double> *>(&bc_left_vel_x, &bc_other_vel_x));
  DefaultEssentialBCConst<double> bc_vel_y(Hermes::vector<std::string>(BDY_LEFT, BDY_BOTTOM, BDY_TOP, BDY_OBSTACLE), 0.0);
  EssentialBCs<double> bcs_vel_y(&bc_vel_y);

  // Spaces for velocity components and pressure.
  H1Space<double> xvel_space(&mesh, &bcs_vel_x, P_INIT_VEL);
  H1Space<double> yvel_space(&mesh, &bcs_vel_y, P_INIT_VEL);
#ifdef PRESSURE_IN_L2
  L2Space<double> p_space(&mesh, P_INIT_PRESSURE);
#else
  H1Space<double> p_space(&mesh, P_INIT_PRESSURE);
#endif

  // Calculate and report the number of degrees of freedom.
  int ndof = Space<double>::get_num_dofs(Hermes::vector<Space<double>*>(&xvel_space, &yvel_space, &p_space));
  info("ndof = %d.", ndof);

  // Define projection norms.
  ProjNormType vel_proj_norm = HERMES_H1_NORM;
#ifdef PRESSURE_IN_L2
  ProjNormType p_proj_norm = HERMES_L2_NORM;
#else
  ProjNormType p_proj_norm = HERMES_H1_NORM;
#endif

  // Solutions for the Newton's iteration and time stepping.
  info("Setting initial conditions.");
  ZeroSolution xvel_prev_time(&mesh);
  ZeroSolution yvel_prev_time(&mesh);
  ZeroSolution p_prev_time(&mesh);

  // Initialize weak formulation.
  WeakForm<double>* wf;
  if (NEWTON)
    wf = new WeakFormNSNewton(STOKES, RE, TAU, &xvel_prev_time, &yvel_prev_time);
  else
    wf = new WeakFormNSSimpleLinearization(STOKES, RE, TAU, &xvel_prev_time, &yvel_prev_time);

  // Initialize the FE problem.
  DiscreteProblem<double> dp(wf, Hermes::vector<Space<double>*>(&xvel_space, &yvel_space, &p_space));

  // Set up the solver, matrix, and rhs according to the solver selection.
  SparseMatrix<double>* matrix = create_matrix<double>(matrix_solver_type);
  Vector<double>* rhs = create_vector<double>(matrix_solver_type);
  LinearSolver<double>* solver = create_linear_solver<double>(matrix_solver_type, matrix, rhs);

  // Initialize views.
  VectorView vview("velocity [m/s]", new WinGeom(0, 0, 750, 240));
  ScalarView pview("pressure [Pa]", new WinGeom(0, 290, 750, 240));
  vview.set_min_max_range(0, 1.6);
  vview.fix_scale_width(80);
  //pview.set_min_max_range(-0.9, 1.0);
  pview.fix_scale_width(80);
  pview.show_mesh(true);

  // Project the initial condition on the FE space to obtain initial
  // coefficient vector for the Newton's method.
  double* coeff_vec = new double[Space<double>::get_num_dofs(Hermes::vector<Space<double>*>(&xvel_space, &yvel_space, &p_space))];
  if (NEWTON) 
  {
    info("Projecting initial condition to obtain initial vector for the Newton's method.");
    OGProjection<double>::project_global(Hermes::vector<Space<double>*>(&xvel_space, &yvel_space, &p_space),
                   Hermes::vector<MeshFunction<double>*>(&xvel_prev_time, &yvel_prev_time, &p_prev_time),
                   coeff_vec, matrix_solver_type,
                   Hermes::vector<ProjNormType>(vel_proj_norm, vel_proj_norm, p_proj_norm));
  }

  // Time-stepping loop:
  char title[100];
  int num_time_steps = T_FINAL / TAU;
  for (int ts = 1; ts <= num_time_steps; ts++)
  {
    current_time += TAU;
    info("---- Time step %d, time = %g:", ts, current_time);

    // Update time-dependent essential BCs.
    if (current_time <= STARTUP_TIME) {
      info("Updating time-dependent essential BC.");
      Space<double>::update_essential_bc_values(Hermes::vector<Space<double>*>(&xvel_space, &yvel_space, &p_space), current_time);
    }

    if (NEWTON)
    {
      // Perform Newton's iteration.
      info("Solving nonlinear problem:");
      Hermes::Hermes2D::NewtonSolver<double> newton(&dp, matrix_solver_type);
      try
      {
        newton.solve(coeff_vec, NEWTON_TOL, NEWTON_MAX_ITER);
      }
      catch(Hermes::Exceptions::Exception e)
      {
        e.printMsg();
        error("Newton's iteration failed.");
      };

      // Update previous time level solutions.
      Solution<double>::vector_to_solutions(coeff_vec, Hermes::vector<Space<double>*>(&xvel_space, &yvel_space, &p_space),
                                    Hermes::vector<Solution<double>*>(&xvel_prev_time, &yvel_prev_time, &p_prev_time));
    }
    else 
    {
      // Linear solve.
      info("Assembling and solving linear problem.");
      dp.assemble(matrix, rhs, false);
      if(solver->solve())
        Solution<double>::vector_to_solutions(solver->get_sln_vector(),
                  Hermes::vector<Space<double>*>(&xvel_space, &yvel_space, &p_space),
                  Hermes::vector<Solution<double>*>(&xvel_prev_time, &yvel_prev_time, &p_prev_time));
      else
        error ("Matrix solver failed.\n");
    }

    // Show the solution at the end of time step.
    sprintf(title, "Velocity, time %g", current_time);
    vview.set_title(title);
    vview.show(&xvel_prev_time, &yvel_prev_time, HERMES_EPS_LOW);
    sprintf(title, "Pressure, time %g", current_time);
    pview.set_title(title);
    pview.show(&p_prev_time);
  }

  delete [] coeff_vec;
  delete matrix;
  delete rhs;
  delete solver;

  // Wait for all views to be closed.
  View::wait();
  return 0;
}
コード例 #3
0
ファイル: main.cpp プロジェクト: hpfem/hermes-examples
int main(int argc, char* argv[])
{
  // Load the mesh.
  MeshSharedPtr mesh(new Mesh);
  MeshReaderH2D mloader;
  mloader.load("domain.mesh", mesh);

  // Initial mesh refinements.
  mesh->refine_all_elements();
  mesh->refine_all_elements();
  mesh->refine_towards_boundary(BDY_OBSTACLE, 2, false);
  // 'true' stands for anisotropic refinements.
  mesh->refine_towards_boundary(BDY_TOP, 2, true);
  mesh->refine_towards_boundary(BDY_BOTTOM, 2, true);

  // Show mesh.
  MeshView mv;
  mv.show(mesh);
  Hermes::Mixins::Loggable::Static::info("Close mesh window to continue.");

  // Initialize boundary conditions.
  EssentialBCNonConst bc_left_vel_x(BDY_LEFT, VEL_INLET, H, STARTUP_TIME);
  DefaultEssentialBCConst<double> bc_other_vel_x({ BDY_BOTTOM, BDY_TOP, BDY_OBSTACLE }, 0.0);
  EssentialBCs<double> bcs_vel_x({ &bc_left_vel_x, &bc_other_vel_x });
  DefaultEssentialBCConst<double> bc_vel_y({ BDY_LEFT, BDY_BOTTOM, BDY_TOP, BDY_OBSTACLE }, 0.0);
  EssentialBCs<double> bcs_vel_y(&bc_vel_y);

  SpaceSharedPtr<double> xvel_space(new H1Space<double>(mesh, &bcs_vel_x, P_INIT_VEL));
  SpaceSharedPtr<double> yvel_space(new H1Space<double>(mesh, &bcs_vel_y, P_INIT_VEL));
#ifdef PRESSURE_IN_L2
  SpaceSharedPtr<double> p_space(new L2Space<double>(mesh, P_INIT_PRESSURE));
#else
  SpaceSharedPtr<double> p_space(new H1Space<double>(mesh, P_INIT_PRESSURE));
#endif
  std::vector<SpaceSharedPtr<double> > spaces({ xvel_space, yvel_space, p_space });

  // Calculate and report the number of degrees of freedom.
  int ndof = Space<double>::get_num_dofs(spaces);
  Hermes::Mixins::Loggable::Static::info("ndof = %d.", ndof);

  // Define projection norms.
  NormType vel_proj_norm = HERMES_H1_NORM;
#ifdef PRESSURE_IN_L2
  NormType p_proj_norm = HERMES_L2_NORM;
#else
  NormType p_proj_norm = HERMES_H1_NORM;
#endif

  // Solutions for the Newton's iteration and time stepping.
  Hermes::Mixins::Loggable::Static::info("Setting zero initial conditions.");
  MeshFunctionSharedPtr<double>  xvel_prev_time(new ZeroSolution<double>(mesh));
  MeshFunctionSharedPtr<double>  yvel_prev_time(new ZeroSolution<double>(mesh));
  MeshFunctionSharedPtr<double>  p_prev_time(new ZeroSolution<double>(mesh));

  // Initialize weak formulation.
  WeakFormSharedPtr<double> wf(new WeakFormNSNewton(STOKES, RE, TAU, xvel_prev_time, yvel_prev_time));

  // Initialize the FE problem.
  Hermes::Hermes2D::NewtonSolver<double> newton(wf, spaces);
  Hermes::Mixins::Loggable::Static::info("Solving nonlinear problem:");
  newton.set_max_allowed_iterations(NEWTON_MAX_ITER);
  newton.set_tolerance(NEWTON_TOL, Hermes::Solvers::ResidualNormAbsolute);
  newton.set_jacobian_constant();

  // Initialize views.
  VectorView vview("velocity [m/s]", new WinGeom(0, 0, 750, 240));
  ScalarView pview("pressure [Pa]", new WinGeom(0, 290, 750, 240));
  vview.set_min_max_range(0, 1.6);
  vview.fix_scale_width(80);
  //pview.set_min_max_range(-0.9, 1.0);
  pview.fix_scale_width(80);
  pview.show_mesh(true);

  // Time-stepping loop:
  char title[100];
  int num_time_steps = T_FINAL / TAU;
  for (int ts = 1; ts <= num_time_steps; ts++)
  {
    current_time += TAU;
    Hermes::Mixins::Loggable::Static::info("---- Time step %d, time = %g:", ts, current_time);

    // Update time-dependent essential BCs.
    if (current_time <= STARTUP_TIME) {
      Hermes::Mixins::Loggable::Static::info("Updating time-dependent essential BC.");
      Space<double>::update_essential_bc_values(spaces, current_time);
    }

    // Perform Newton's iteration.
    try
    {
      newton.solve();
    }
    catch (Hermes::Exceptions::Exception e)
    {
      e.print_msg();
    };

    // Update previous time level solutions.
    Solution<double>::vector_to_solutions(newton.get_sln_vector(), spaces, { xvel_prev_time, yvel_prev_time, p_prev_time });

    // Visualization.
    // Hermes visualization.
    if (HERMES_VISUALIZATION)
    {
      // Show the solution at the end of time step.
      sprintf(title, "Velocity, time %g", current_time);
      vview.set_title(title);
      vview.show(xvel_prev_time, yvel_prev_time);
      sprintf(title, "Pressure, time %g", current_time);
      pview.set_title(title);
      pview.show(p_prev_time);
    }
  }

  // Wait for all views to be closed.
  View::wait();
  return 0;
}