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mfem/examples/advection.cpp
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// MFEM Advection Equation examples
//
// Compile with: make advection
//
// Sample runs:
//
// advection -p 1 -r 2 -o 1 -s 3
// advection -p 1 -r 1 -o 3 -s 4
// advection -p 1 -r 0 -o 5 -s 6
// advection -p 2 -r 1 -o 1 -s 3
// advection -p 2 -r 0 -o 3 -s 3
//
// Description: This example code solves the compressible Advection system of
// equations, a model nonlinear hyperbolic PDE, with a
// discontinuous Galerkin (DG) formulation.
//
// Specifically, it solves for an exact solution of the equations
// whereby a vortex is transported by a uniform flow. Since all
// boundaries are periodic here, the method's accuracy can be
// assessed by measuring the difference between the solution and
// the initial condition at a later time when the vortex returns
// to its initial location.
//
// Note that as the order of the spatial discretization increases,
// the timestep must become smaller. This example currently uses a
// simple estimate derived by Cockburn and Shu for the 1D RKDG
// method. An additional factor can be tuned by passing the --cfl
// (or -c shorter) flag.
//
// The example demonstrates user-defined bilinear and nonlinear
// form integrators for systems of equations that are defined with
// block vectors, and how these are used with an operator for
// explicit time integrators. In this case the system also
// involves an external approximate Riemann solver for the DG
// interface flux. It also demonstrates how to use GLVis for
// in-situ visualization of vector grid functions.
//
// We recommend viewing examples 9, 14 and 17 before viewing this
// example.
#include <fstream>
#include <iostream>
#include <sstream>
#include "mfem.hpp"
// Classes HyperbolicConservationLaws, NumericalFlux, and FaceIntegrator
// shared between the serial and parallel version of the example.
#include "hyperbolic_conservation_laws.hpp"
// Choice for the problem setup. See InitialCondition in ex18.hpp.
typedef std::__1::function<void(const Vector &, Vector &)> SpatialFunction;
void AdvectionMesh(const int problem, const char **mesh_file);
SpatialFunction AdvectionInitialCondition(const int problem);
SpatialFunction AdvectionVelocityVector(const int problem);
void UpdateSystem(FiniteElementSpace &fes,
DGHyperbolicConservationLaws &advection, GridFunction &sol,
ODESolver *ode_solver);
int main(int argc, char *argv[]) {
// 1. Parse command-line options.
int problem = 1;
const char *mesh_file = "";
int IntOrderOffset = 3;
int ref_levels = 4;
int order = 3;
int ode_solver_type = 4;
double t_final = 10.0;
double dt = -0.01;
double cfl = 0.3;
bool visualization = true;
int vis_steps = 50;
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(&ref_levels, "-r", "--refine",
"Number of times to refine the mesh uniformly.");
args.AddOption(&order, "-o", "--order",
"Order (degree) of the finite elements.");
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.");
args.AddOption(&t_final, "-tf", "--t-final", "Final time; start time is 0.");
args.AddOption(&dt, "-dt", "--time-step",
"Time step. Positive number skips CFL timestep calculation.");
args.AddOption(&cfl, "-c", "--cfl-number",
"CFL number for timestep calculation.");
args.AddOption(&visualization, "-vis", "--visualization", "-no-vis",
"--no-visualization",
"Enable or disable GLVis visualization.");
args.AddOption(&vis_steps, "-vs", "--visualization-steps",
"Visualize every n-th timestep.");
args.Parse();
if (!args.Good()) {
args.PrintUsage(cout);
return 1;
}
// When the user does not provide mesh file,
// use the default mesh file for the problem.
if ((mesh_file == NULL) || (mesh_file[0] == '\0')) { // if NULL or empty
AdvectionMesh(problem, &mesh_file); // get default mesh file name
}
args.PrintOptions(cout);
// 2. Read the mesh from the given mesh file.
Mesh mesh = Mesh(mesh_file);
const int dim = mesh.Dimension();
const int num_equations = 1;
// perform uniform refine
for (int lev = 0; lev < ref_levels; lev++) {
mesh.UniformRefinement();
}
if (dim > 1) mesh.EnsureNCMesh();
// 3. Define the ODE solver used for time integration. Several explicit
// Runge-Kutta methods are available.
ODESolver *ode_solver = NULL;
switch (ode_solver_type) {
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;
default:
cout << "Unknown ODE solver type: " << ode_solver_type << '\n';
return 3;
}
// 4. Define the discontinuous DG finite element space of the given
// polynomial order on the refined mesh.
DG_FECollection fec(order, dim);
// Finite element space for a scalar (thermodynamic quantity)
FiniteElementSpace fes(&mesh, &fec);
// This example depends on this ordering of the space.
MFEM_ASSERT(fes.GetOrdering() == Ordering::byNODES, "");
cout << "Number of unknowns: " << fes.GetVSize() << endl;
// 6. Define the initial conditions, save the corresponding mesh and grid
// functions to a file. This can be opened with GLVis with the -gc option.
// Initialize the state.
VectorFunctionCoefficient u0(num_equations,
AdvectionInitialCondition(problem));
VectorFunctionCoefficient b(dim, AdvectionVelocityVector(problem));
GridFunction sol(&fes);
sol.ProjectCoefficient(u0);
// Output the initial solution.
{
ofstream mesh_ofs("vortex.mesh");
mesh_ofs.precision(precision);
mesh_ofs << mesh;
for (int k = 0; k < num_equations; k++) {
GridFunction uk(&fes, sol.GetData() + fes.GetNDofs() * k);
ostringstream sol_name;
sol_name << "vortex-" << k << "-init.gf";
ofstream sol_ofs(sol_name.str().c_str());
sol_ofs.precision(precision);
sol_ofs << uk;
}
}
// 7. Set up the nonlinear form corresponding to the DG discretization of the
// flux divergence, and assemble the corresponding mass matrix.
AdvectionElementFormIntegrator *advectionElementFormIntegrator =
new AdvectionElementFormIntegrator(dim, b, IntOrderOffset);
NumericalFlux *numericalFlux = new RusanovFlux();
AdvectionFaceFormIntegrator *advectionFaceFormIntegrator =
new AdvectionFaceFormIntegrator(numericalFlux, dim, b, IntOrderOffset);
NonlinearForm nonlinForm(&fes);
// 8. 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).
DGHyperbolicConservationLaws advection(
&fes, &nonlinForm, *advectionElementFormIntegrator,
*advectionFaceFormIntegrator, num_equations);
// Visualize the density
socketstream sout;
if (visualization) {
char vishost[] = "localhost";
int visport = 19916;
sout.open(vishost, visport);
if (!sout) {
cout << "Unable to connect to GLVis server at " << vishost << ':'
<< visport << endl;
visualization = false;
cout << "GLVis visualization disabled.\n";
} else {
sout.precision(precision);
sout << "solution\n" << mesh << sol;
sout << "pause\n";
sout << flush;
cout << "GLVis visualization paused."
<< " Press space (in the GLVis window) to resume it.\n";
}
}
// Determine the minimum element size.
double hmin = 0.0;
if (cfl > 0) {
hmin = mesh.GetElementSize(0, 1);
for (int i = 1; i < mesh.GetNE(); i++) {
hmin = min(mesh.GetElementSize(i, 1), hmin);
}
}
// Start the timer.
tic_toc.Clear();
tic_toc.Start();
double t = 0.0;
advection.SetTime(t);
ode_solver->Init(advection);
if (cfl > 0) {
// Find a safe dt, using a temporary vector. Calling Mult() computes the
// maximum char speed at all quadrature points on all faces.
Vector z(sol.Size());
advection.Mult(sol, z);
// faceForm.Mult(sol, z);
dt = cfl * hmin / advection.getMaxCharSpeed() / (2 * order + 1);
}
// Integrate in time.
bool done = false;
for (int ti = 0; !done;) {
double dt_real = min(dt, t_final - t);
ode_solver->Step(sol, t, dt_real);
if (cfl > 0) {
dt = cfl * hmin / advection.getMaxCharSpeed() / (2 * order + 1);
}
ti++;
done = (t >= t_final - 1e-8 * dt);
if (done || ti % vis_steps == 0) {
cout << "time step: " << ti << ", time: " << t << endl;
if (visualization) {
sout << "solution\n" << mesh << sol << flush;
}
}
}
tic_toc.Stop();
cout << " done, " << tic_toc.RealTime() << "s." << endl;
// 9. Save the final solution. This output can be viewed later using GLVis:
// "glvis -m vortex.mesh -g vortex-1-final.gf".
for (int k = 0; k < num_equations; k++) {
GridFunction uk(&fes, sol.GetData() + fes.GetNDofs());
ostringstream sol_name;
sol_name << "vortex-" << k << "-final.gf";
ofstream sol_ofs(sol_name.str().c_str());
sol_ofs.precision(precision);
sol_ofs << uk;
}
// 10. Compute the L2 solution error summed for all components.
// if (t_final == 2.0) {
const double error = sol.ComputeLpError(2, u0);
cout << "Solution error: " << error << endl;
// }
// Free the used memory.
delete ode_solver;
return 0;
}
void UpdateSystem(FiniteElementSpace &fes,
DGHyperbolicConservationLaws &advection, GridFunction &sol,
ODESolver *ode_solver) {
fes.Update();
sol.Update();
advection.Update();
ode_solver->Init(advection);
fes.UpdatesFinished();
}
void AdvectionMesh(const int problem, const char **mesh_file) {
switch (problem) {
case 1:
*mesh_file = "../data/periodic-square-4x4.mesh";
break;
default:
throw invalid_argument("Default mesh is undefined");
}
}
// Initial condition
SpatialFunction AdvectionInitialCondition(const int problem) {
switch (problem) {
case 1:
return [](const Vector &x, Vector &y) {
MFEM_ASSERT(x.Size() == 2, "Dimension should be 2");
y(0) = __sinpi(x(0)) * __sinpi(x(1));
};
default:
throw invalid_argument("Problem Undefined");
}
}
// Initial condition
SpatialFunction AdvectionVelocityVector(const int problem) {
switch (problem) {
case 1:
return [](const Vector &x, Vector &y) {
const double d = max((x(0) + 1.) * (1. - x(0)), 0.) *
max((x(1) + 1.) * (1. - x(1)), 0.);
const double d2 = d * d;
y(0) = d2 * M_PI_2 * x(1);
y(1) = -d2 * M_PI_2 * x(0);
};
default:
throw invalid_argument("Problem Undefined");
}
}