The fix in example 9 uses the approach used in the regular example 9 to fix the same leak (see PR #816). Fix a memory leak in SUNDIALS example 9 using the same fix that was used
496 lines
15 KiB
C++
496 lines
15 KiB
C++
// MFEM Example 9
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// SUNDIALS Modification
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//
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// Compile with: make ex9
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//
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// Sample runs:
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// ex9 -m ../../data/periodic-segment.mesh -p 0 -r 2 -s 7 -dt 0.005
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// ex9 -m ../../data/periodic-square.mesh -p 1 -r 2 -s 8 -dt 0.005 -tf 9
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// ex9 -m ../../data/periodic-hexagon.mesh -p 0 -r 2 -s 7 -dt 0.0018 -vs 25
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// ex9 -m ../../data/periodic-hexagon.mesh -p 0 -r 2 -s 9 -dt 0.01 -vs 15
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// ex9 -m ../../data/amr-quad.mesh -p 1 -r 2 -s 9 -dt 0.002 -tf 9
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// ex9 -m ../../data/star-q3.mesh -p 1 -r 2 -s 9 -dt 0.005 -tf 9
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// ex9 -m ../../data/disc-nurbs.mesh -p 1 -r 3 -s 7 -dt 0.005 -tf 9
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// ex9 -m ../../data/periodic-cube.mesh -p 0 -r 2 -s 8 -dt 0.02 -tf 8 -o 2
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//
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// Description: This example code solves the time-dependent advection equation
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// du/dt + v.grad(u) = 0, where v is a given fluid velocity, and
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// u0(x)=u(0,x) is a given initial condition.
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//
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// The example demonstrates the use of Discontinuous Galerkin (DG)
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// bilinear forms in MFEM (face integrators), the use of explicit
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// ODE time integrators, the definition of periodic boundary
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// conditions through periodic meshes, as well as the use of GLVis
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// for persistent visualization of a time-evolving solution. The
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// saving of time-dependent data files for external visualization
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// with VisIt (visit.llnl.gov) is also illustrated.
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#include "mfem.hpp"
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#include <fstream>
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#include <iostream>
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#include <algorithm>
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#ifndef MFEM_USE_SUNDIALS
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#error This example requires that MFEM is built with MFEM_USE_SUNDIALS=YES
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#endif
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using namespace std;
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using namespace mfem;
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// Choice for the problem setup. The fluid velocity, initial condition and
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// inflow boundary condition are chosen based on this parameter.
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int problem;
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// Velocity coefficient
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void velocity_function(const Vector &x, Vector &v);
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// Initial condition
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double u0_function(const Vector &x);
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// Inflow boundary condition
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double inflow_function(const Vector &x);
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// Mesh bounding box
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Vector bb_min, bb_max;
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/** A time-dependent operator for the right-hand side of the ODE. The DG weak
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form of du/dt = -v.grad(u) is M du/dt = K u + b, where M and K are the mass
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and advection matrices, and b describes the flow on the boundary. This can
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be written as a general ODE, du/dt = M^{-1} (K u + b), and this class is
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used to evaluate the right-hand side. */
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class FE_Evolution : public TimeDependentOperator
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{
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private:
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SparseMatrix &M, &K;
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const Vector &b;
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DSmoother M_prec;
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CGSolver M_solver;
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mutable Vector z;
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public:
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FE_Evolution(SparseMatrix &_M, SparseMatrix &_K, const Vector &_b);
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virtual void Mult(const Vector &x, Vector &y) const;
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virtual ~FE_Evolution() { }
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};
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int main(int argc, char *argv[])
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{
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// 1. Parse command-line options.
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problem = 0;
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const char *mesh_file = "../../data/periodic-hexagon.mesh";
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int ref_levels = 2;
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int order = 3;
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int ode_solver_type = 4;
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double t_final = 10.0;
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double dt = 0.01;
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bool visualization = true;
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bool visit = false;
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bool binary = false;
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int vis_steps = 5;
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// Relative and absolute tolerances for CVODE and ARKODE.
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const double reltol = 1e-2, abstol = 1e-2;
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int precision = 8;
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cout.precision(precision);
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OptionsParser args(argc, argv);
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args.AddOption(&mesh_file, "-m", "--mesh",
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"Mesh file to use.");
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args.AddOption(&problem, "-p", "--problem",
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"Problem setup to use. See options in velocity_function().");
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args.AddOption(&ref_levels, "-r", "--refine",
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"Number of times to refine the mesh uniformly.");
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args.AddOption(&order, "-o", "--order",
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"Order (degree) of the finite elements.");
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args.AddOption(&ode_solver_type, "-s", "--ode-solver",
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"ODE solver:\n\t"
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"1 - Forward Euler,\n\t"
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"2 - RK2 SSP,\n\t"
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"3 - RK3 SSP,\n\t"
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"4 - RK4,\n\t"
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"6 - RK6,\n\t"
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"7 - CVODE (adaptive order implicit Adams),\n\t"
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"8 - ARKODE default (4th order) explicit,\n\t"
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"9 - ARKODE RK8.");
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args.AddOption(&t_final, "-tf", "--t-final",
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"Final time; start time is 0.");
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args.AddOption(&dt, "-dt", "--time-step",
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"Time step.");
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args.AddOption(&visualization, "-vis", "--visualization", "-no-vis",
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"--no-visualization",
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"Enable or disable GLVis visualization.");
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args.AddOption(&visit, "-visit", "--visit-datafiles", "-no-visit",
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"--no-visit-datafiles",
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"Save data files for VisIt (visit.llnl.gov) visualization.");
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args.AddOption(&binary, "-binary", "--binary-datafiles", "-ascii",
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"--ascii-datafiles",
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"Use binary (Sidre) or ascii format for VisIt data files.");
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args.AddOption(&vis_steps, "-vs", "--visualization-steps",
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"Visualize every n-th timestep.");
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args.Parse();
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if (!args.Good())
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{
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args.PrintUsage(cout);
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return 1;
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}
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// check for vaild ODE solver option
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if (ode_solver_type < 1 || ode_solver_type > 9)
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{
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cout << "Unknown ODE solver type: " << ode_solver_type << '\n';
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return 3;
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}
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args.PrintOptions(cout);
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// 2. Read the mesh from the given mesh file. We can handle geometrically
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// periodic meshes in this code.
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Mesh mesh(mesh_file, 1, 1);
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int dim = mesh.Dimension();
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// 3. Refine the mesh to increase the resolution. In this example we do
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// 'ref_levels' of uniform refinement, where 'ref_levels' is a
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// command-line parameter. If the mesh is of NURBS type, we convert it to
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// a (piecewise-polynomial) high-order mesh.
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for (int lev = 0; lev < ref_levels; lev++)
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{
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mesh.UniformRefinement();
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}
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if (mesh.NURBSext)
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{
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mesh.SetCurvature(max(order, 1));
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}
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mesh.GetBoundingBox(bb_min, bb_max, max(order, 1));
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// 4. Define the discontinuous DG finite element space of the given
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// polynomial order on the refined mesh.
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DG_FECollection fec(order, dim);
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FiniteElementSpace fes(&mesh, &fec);
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cout << "Number of unknowns: " << fes.GetVSize() << endl;
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// 5. Set up and assemble the bilinear and linear forms corresponding to the
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// DG discretization. The DGTraceIntegrator involves integrals over mesh
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// interior faces.
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VectorFunctionCoefficient velocity(dim, velocity_function);
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FunctionCoefficient inflow(inflow_function);
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FunctionCoefficient u0(u0_function);
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BilinearForm m(&fes);
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m.AddDomainIntegrator(new MassIntegrator);
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BilinearForm k(&fes);
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k.AddDomainIntegrator(new ConvectionIntegrator(velocity, -1.0));
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k.AddInteriorFaceIntegrator(
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new TransposeIntegrator(new DGTraceIntegrator(velocity, 1.0, -0.5)));
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k.AddBdrFaceIntegrator(
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new TransposeIntegrator(new DGTraceIntegrator(velocity, 1.0, -0.5)));
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LinearForm b(&fes);
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b.AddBdrFaceIntegrator(
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new BoundaryFlowIntegrator(inflow, velocity, -1.0, -0.5));
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m.Assemble();
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m.Finalize();
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int skip_zeros = 0;
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k.Assemble(skip_zeros);
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k.Finalize(skip_zeros);
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b.Assemble();
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// 6. Define the initial conditions, save the corresponding grid function to
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// a file and (optionally) save data in the VisIt format and initialize
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// GLVis visualization.
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GridFunction u(&fes);
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u.ProjectCoefficient(u0);
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{
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ofstream omesh("ex9.mesh");
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omesh.precision(precision);
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mesh.Print(omesh);
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ofstream osol("ex9-init.gf");
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osol.precision(precision);
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u.Save(osol);
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}
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// Create data collection for solution output: either VisItDataCollection for
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// ascii data files, or SidreDataCollection for binary data files.
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DataCollection *dc = NULL;
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if (visit)
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{
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if (binary)
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{
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#ifdef MFEM_USE_SIDRE
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dc = new SidreDataCollection("Example9", &mesh);
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#else
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MFEM_ABORT("Must build with MFEM_USE_SIDRE=YES for binary output.");
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#endif
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}
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else
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{
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dc = new VisItDataCollection("Example9", &mesh);
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dc->SetPrecision(precision);
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}
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dc->RegisterField("solution", &u);
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dc->SetCycle(0);
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dc->SetTime(0.0);
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dc->Save();
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}
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socketstream sout;
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if (visualization)
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{
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char vishost[] = "localhost";
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int visport = 19916;
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sout.open(vishost, visport);
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if (!sout)
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{
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cout << "Unable to connect to GLVis server at "
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<< vishost << ':' << visport << endl;
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visualization = false;
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cout << "GLVis visualization disabled.\n";
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}
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else
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{
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sout.precision(precision);
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sout << "solution\n" << mesh << u;
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sout << "pause\n";
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sout << flush;
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cout << "GLVis visualization paused."
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<< " Press space (in the GLVis window) to resume it.\n";
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}
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}
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// 7. Define the time-dependent evolution operator describing the ODE
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// right-hand side, and define the ODE solver used for time integration.
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FE_Evolution adv(m.SpMat(), k.SpMat(), b);
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double t = 0.0;
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adv.SetTime(t);
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// Create the time integrator
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ODESolver *ode_solver = NULL;
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CVODESolver *cvode = NULL;
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ARKStepSolver *arkode = NULL;
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switch (ode_solver_type)
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{
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case 1: ode_solver = new ForwardEulerSolver; break;
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case 2: ode_solver = new RK2Solver(1.0); break;
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case 3: ode_solver = new RK3SSPSolver; break;
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case 4: ode_solver = new RK4Solver; break;
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case 6: ode_solver = new RK6Solver; break;
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case 7:
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cvode = new CVODESolver(CV_ADAMS);
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cvode->Init(adv);
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cvode->SetSStolerances(reltol, abstol);
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cvode->SetMaxStep(dt);
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cvode->UseSundialsLinearSolver();
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ode_solver = cvode; break;
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case 8:
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case 9:
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arkode = new ARKStepSolver(ARKStepSolver::EXPLICIT);
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arkode->Init(adv);
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arkode->SetSStolerances(reltol, abstol);
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arkode->SetMaxStep(dt);
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if (ode_solver_type == 9) { arkode->SetERKTableNum(FEHLBERG_13_7_8); }
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ode_solver = arkode; break;
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}
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// Initialize MFEM integrators, SUNDIALS integrators are initialized above
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if (ode_solver_type < 7) { ode_solver->Init(adv); }
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// 8. Perform time-integration (looping over the time iterations, ti,
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// with a time-step dt).
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bool done = false;
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for (int ti = 0; !done; )
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{
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double dt_real = min(dt, t_final - t);
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ode_solver->Step(u, t, dt_real);
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ti++;
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done = (t >= t_final - 1e-8*dt);
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if (done || ti % vis_steps == 0)
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{
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cout << "time step: " << ti << ", time: " << t << endl;
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if (cvode) { cvode->PrintInfo(); }
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if (arkode) { arkode->PrintInfo(); }
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if (visualization)
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{
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sout << "solution\n" << mesh << u << flush;
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}
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if (visit)
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{
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dc->SetCycle(ti);
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dc->SetTime(t);
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dc->Save();
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}
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}
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}
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// 9. Save the final solution. This output can be viewed later using GLVis:
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// "glvis -m ex9.mesh -g ex9-final.gf".
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{
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ofstream osol("ex9-final.gf");
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osol.precision(precision);
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u.Save(osol);
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}
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// 10. Free the used memory.
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delete ode_solver;
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delete dc;
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return 0;
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}
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// Implementation of class FE_Evolution
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FE_Evolution::FE_Evolution(SparseMatrix &_M, SparseMatrix &_K, const Vector &_b)
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: TimeDependentOperator(_M.Size()), M(_M), K(_K), b(_b), z(_M.Size())
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{
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M_solver.SetPreconditioner(M_prec);
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M_solver.SetOperator(M);
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M_solver.iterative_mode = false;
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M_solver.SetRelTol(1e-9);
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M_solver.SetAbsTol(0.0);
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M_solver.SetMaxIter(100);
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M_solver.SetPrintLevel(0);
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}
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void FE_Evolution::Mult(const Vector &x, Vector &y) const
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{
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// y = M^{-1} (K x + b)
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K.Mult(x, z);
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z += b;
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M_solver.Mult(z, y);
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}
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// Velocity coefficient
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void velocity_function(const Vector &x, Vector &v)
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{
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int dim = x.Size();
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// map to the reference [-1,1] domain
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Vector X(dim);
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for (int i = 0; i < dim; i++)
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{
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double center = (bb_min[i] + bb_max[i]) * 0.5;
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X(i) = 2 * (x(i) - center) / (bb_max[i] - bb_min[i]);
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}
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switch (problem)
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{
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case 0:
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{
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// Translations in 1D, 2D, and 3D
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switch (dim)
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{
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case 1: v(0) = 1.0; break;
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case 2: v(0) = sqrt(2./3.); v(1) = sqrt(1./3.); break;
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case 3: v(0) = sqrt(3./6.); v(1) = sqrt(2./6.); v(2) = sqrt(1./6.);
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break;
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}
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break;
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}
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case 1:
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case 2:
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{
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// Clockwise rotation in 2D around the origin
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const double w = M_PI/2;
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switch (dim)
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{
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case 1: v(0) = 1.0; break;
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case 2: v(0) = w*X(1); v(1) = -w*X(0); break;
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case 3: v(0) = w*X(1); v(1) = -w*X(0); v(2) = 0.0; break;
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}
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break;
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}
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case 3:
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{
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// Clockwise twisting rotation in 2D around the origin
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const double w = M_PI/2;
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double d = max((X(0)+1.)*(1.-X(0)),0.) * max((X(1)+1.)*(1.-X(1)),0.);
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d = d*d;
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switch (dim)
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{
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case 1: v(0) = 1.0; break;
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case 2: v(0) = d*w*X(1); v(1) = -d*w*X(0); break;
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case 3: v(0) = d*w*X(1); v(1) = -d*w*X(0); v(2) = 0.0; break;
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}
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break;
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}
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}
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}
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// Initial condition
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double u0_function(const Vector &x)
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{
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int dim = x.Size();
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// map to the reference [-1,1] domain
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Vector X(dim);
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for (int i = 0; i < dim; i++)
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{
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double center = (bb_min[i] + bb_max[i]) * 0.5;
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X(i) = 2 * (x(i) - center) / (bb_max[i] - bb_min[i]);
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}
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switch (problem)
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{
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case 0:
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case 1:
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{
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switch (dim)
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{
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case 1:
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return exp(-40.*pow(X(0)-0.5,2));
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case 2:
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case 3:
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{
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double rx = 0.45, ry = 0.25, cx = 0., cy = -0.2, w = 10.;
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if (dim == 3)
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{
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const double s = (1. + 0.25*cos(2*M_PI*X(2)));
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rx *= s;
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ry *= s;
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}
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return ( erfc(w*(X(0)-cx-rx))*erfc(-w*(X(0)-cx+rx)) *
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erfc(w*(X(1)-cy-ry))*erfc(-w*(X(1)-cy+ry)) )/16;
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}
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}
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}
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case 2:
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{
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double x_ = X(0), y_ = X(1), rho, phi;
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rho = hypot(x_, y_);
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phi = atan2(y_, x_);
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return pow(sin(M_PI*rho),2)*sin(3*phi);
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}
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case 3:
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{
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const double f = M_PI;
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return sin(f*X(0))*sin(f*X(1));
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}
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}
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return 0.0;
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}
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// Inflow boundary condition (zero for the problems considered in this example)
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double inflow_function(const Vector &x)
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{
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switch (problem)
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{
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case 0:
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case 1:
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case 2:
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case 3: return 0.0;
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}
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return 0.0;
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}
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