This tutorial program solves the Euler equations of fluid dynamics, using an explicit time integrator with the matrix-free framework applied to a high-order discontinuous Galerkin discretization in space. The numerical approach used here is identical to that used in step-67, however, we utilize different advanced MatrixFree techniques to reach even a higher throughput.
Further topics we discuss in this tutorial are the usage and benefits of the template argument VectorizedArrayType (instead of simply using VectorizedArray<Number>) as well as the possibility to pass lambdas to MatrixFree loops.
There exist many shared-memory libraries that are based on threads like TBB, OpenMP, or TaskFlow. Integrating such libraries into existing MPI programs allows one to use shared memory. However, these libraries come with an overhead for the programmer, since all parallelizable code sections have to be found and transformed according to the library used, including the difficulty when some third-party numerical library, like an iterative solver package, only relies on MPI.
Considering a purely MPI-parallelized FEM application, one can identify that the major time and memory benefit of using shared memory would come from accessing the part of the solution vector owned by the processes on the same compute node without the need to make explicit copies and buffering them. Fur this propose, MPI-3.0 provides shared-memory features based on so-called windows, where processes can directly access the data of the neighbors on the same shared-memory domain.
A few relevant MPI-3.0 commands are worth discussing in detail. A new MPI communicator comm_sm, which consists of processes from the communicator comm that have access to the same shared memory, can be created via:
The following code snippet shows the simplified allocation routines of shared memory for the value type T and the size local_size, as well as, how to query pointers to the data belonging to processes in the same shared-memory domain:
Once the data is not needed anymore, the window has to be freed, which also frees the locally-owned data:
For example, a vector can be set up with a partitioner (containing the global communicator) and a sub-communicator (containing the processes on the same compute node):
Locally owned values and ghost values can be processed as usual. However, now users also have read access to the values of the shared-memory neighbors via the function:
"Face-centric loops" (short FCL) visit cells and faces (inner and boundary ones) in separate loops. As a consequence, each entity is visited only once and fluxes between cells are evaluated only once. How to perform face-centric loops with the help of MatrixFree::loop() by providing three functions (one for the cell integrals, one for the inner, and one for the boundary faces) has been presented in step-59 and step-67.
"Cell-centric loops" (short CCL or ECL (for element-centric loops) in the hyper.deal release paper), in contrast, process a cell and in direct succession process all its faces (i.e., visit all faces twice). Their benefit has become clear for modern CPU processor architecture in the literature [154], although this kind of loop implies that fluxes have to be computed twice (for each side of an interior face). CCL has two primary advantages:
One should also note that although fluxes are computed twice in the case of CCL, this does not automatically translate into doubling of the computation, since values already interpolated to the cell quadrature points can be interpolated to a face with a simple 1D interpolation.
In particular, these flags enable that the internal data structures are set up for all faces of the cells.
Currently, cell-centric loops in deal.II only work for uniformly refined meshes and if no constraints are applied (which is the standard case DG is normally used).
The examples given above have already used lambdas, which have been provided to matrix-free loops. The following short examples present how to transform functions between a version where a class and a pointer to one of its methods are used and a variant where lambdas are utilized.
In the following code, a class and a pointer to one of its methods, which should be interpreted as cell integral, are passed to MatrixFree::loop():
However, it is also possible to pass an anonymous function via a lambda function with the same result:
This allows users to select the vector length/ISA and, as a consequence, the number of cells to be processed at once in matrix-free operator evaluations, possibly reducing the pressure on the caches, an severe issue for very high degrees (and dimensions).
A possible further reason to reduce the number of filled lanes is to simplify debugging: instead of having to look at, e.g., 8 cells, one can concentrate on a single cell.
This parameter specifies the size of the shared-memory group. Currently, only the values 1 and numbers::invalid_unsigned_int is possible, leading to the options that the memory features can be turned off or all processes having access to the same shared-memory domain are grouped together.
Here, the type of the data structure is chosen for vectorization. In the default case, VectorizedArray<Number> is used, i.e., the highest instruction-set-architecture extension available on the given hardware with the maximum number of vector lanes is used. However, one might reduce the number of filled lanes, e.g., by writing using VectorizedArrayType = VectorizedArray<Number, 4> to only process 4 cells.
Specify max number of time steps useful for performance studies.
Instance of SubCommunicatorWrapper containing the sub-communicator, which we need to pass to MatrixFree::reinit() to be able to exploit MPI-3.0 shared-memory capabilities:
New constructor, which creates a sub-communicator. The user can specify the size of the sub-communicator via the global parameter group_size. If the size is set to -1, all MPI processes of a shared-memory domain are combined to a group. The specified size is decisive for the benefit of the shared-memory capabilities of MatrixFree and, therefore, setting the size to -1 is a reasonable choice. By setting, the size to 1 users explicitly disable the MPI-3.0 shared-memory features of MatrixFree and rely completely on MPI-2.0 features, like MPI_Isend and MPI_Irecv.
New destructor responsible for freeing of the sub-communicator.
Categorize cells so that all lanes have the same boundary IDs for each face. This is strictly not necessary, however, allows to write simpler code in EulerOperator::perform_stage() without masking, since it is guaranteed that all cells grouped together (in a VectorizedArray) have to perform exactly the same operation also on the faces.
The following function does an entire stage of a Runge–Kutta update and is, alongside the slightly modified setup, the heart of this tutorial compared to step-67.
The following function contains to a large extent copies of the following functions from step-67 so that comments related the evaluation of the weak form are skipped here:
Buffer the computed values at the quadrature points, since these are overridden by FEEvaluation::submit_value() in the next step, however, are needed later on for the face integrals:
Test with the gradient of the test functions in the quadrature points. We skip the interpolation back to the support points of the element, since we first collect all contributions in the cell quadrature points and only perform the interpolation back as the final step.
Interpolate the values from the cell quadrature points to the quadrature points of the current face via a simple 1d interpolation:
Check if the face is an internal or a boundary face and select a different code path based on this information:
Process and internal face. The following lines of code are a copy of the function EulerDG::EulerOperator::local_apply_face from step-67:
Process a boundary face. These following lines of code are a copy of the function EulerDG::EulerOperator::local_apply_boundary_face from step-67:
Evaluate local integrals related to cell by quadrature and add into cell contribution via a simple 1d interpolation:
template <
int dim,
int degree,
int n_po
ints_1d>
void EulerOperator<dim, degree, n_points_1d>::initialize_vector(
data.initialize_dof_vector(vector);
template <
int dim,
int degree,
int n_po
ints_1d>
void EulerOperator<dim, degree, n_points_1d>::set_inflow_boundary(
{
AssertThrow(subsonic_outflow_boundaries.find(boundary_id) ==
subsonic_outflow_boundaries.end() &&
wall_boundaries.find(boundary_id) == wall_boundaries.end(),
ExcMessage(
"You already set the boundary with id " +
std::to_string(
static_cast<int>(boundary_id)) +
" to another type of boundary before now setting " +
ExcMessage(
"Expected function with dim+2 components"));
inflow_boundaries[boundary_id] = std::move(inflow_function);
template <
int dim,
int degree,
int n_po
ints_1d>
void EulerOperator<dim, degree, n_points_1d>::set_subsonic_outflow_boundary(
{
inflow_boundaries.end() &&
wall_boundaries.find(boundary_id) == wall_boundaries.end(),
ExcMessage(
"You already set the boundary with id " +
std::to_string(
static_cast<int>(boundary_id)) +
" to another type of boundary before now setting " +
"it as subsonic outflow"));
ExcMessage(
"Expected function with dim+2 components"));
subsonic_outflow_boundaries[
boundary_id] = std::move(outflow_function);
template <
int dim,
int degree,
int n_po
ints_1d>
void EulerOperator<dim, degree, n_points_1d>::set_wall_boundary(
{
inflow_boundaries.end() &&
subsonic_outflow_boundaries.find(boundary_id) ==
subsonic_outflow_boundaries.end(),
ExcMessage(
"You already set the boundary with id " +
std::to_string(
static_cast<int>(boundary_id)) +
" to another type of boundary before now setting " +
wall_boundaries.insert(boundary_id);
template <
int dim,
int degree,
int n_po
ints_1d>
void EulerOperator<dim, degree, n_points_1d>::set_body_force(
{
this->body_force = std::move(body_force);
template <
int dim,
int degree,
int n_po
ints_1d>
void EulerOperator<dim, degree, n_points_1d>::project(
solution.zero_out_ghost_values();
for (
unsigned int cell = 0; cell <
data.n_cell_batches(); ++cell)
for (
const unsigned int q : phi.quadrature_point_indices())
phi.submit_dof_value(evaluate_function(function,
phi.quadrature_point(q)),
inverse.transform_from_q_points_to_basis(dim + 2,
phi.set_dof_values(solution);
template <
int dim,
int degree,
int n_po
ints_1d>
std::array<double, 3> EulerOperator<dim, degree, n_points_1d>::compute_errors(
double errors_squared[3] = {};
for (
unsigned int cell = 0; cell <
data.n_cell_batches(); ++cell)
VectorizedArrayType local_errors_squared[3] = {};
for (
const unsigned int q : phi.quadrature_point_indices())
evaluate_function(function, phi.quadrature_point(q)) -
const auto JxW = phi.JxW(q);
local_errors_squared[0] += error[0] * error[0] * JxW;
for (
unsigned int d = 0;
d < dim; ++
d)
local_errors_squared[1] += (error[d + 1] * error[d + 1]) * JxW;
local_errors_squared[2] += (error[dim + 1] * error[dim + 1]) * JxW;
for (
unsigned int v = 0; v <
data.n_active_entries_per_cell_batch(cell);
for (
unsigned int d = 0;
d < 3; ++
d)
errors_squared[d] += local_errors_squared[d][v];
std::array<double, 3> errors;
for (
unsigned int d = 0;
d < 3; ++
d)
template <
int dim,
int degree,
int n_po
ints_1d>
double EulerOperator<dim, degree, n_points_1d>::compute_cell_transport_speed(
for (
unsigned int cell = 0; cell <
data.n_cell_batches(); ++cell)
VectorizedArrayType local_max = 0.;
for (
const unsigned int q : phi.quadrature_point_indices())
const auto velocity = euler_velocity<dim>(solution);
const auto pressure = euler_pressure<dim>(solution);
const auto inverse_jacobian = phi.inverse_jacobian(q);
const auto convective_speed = inverse_jacobian * velocity;
VectorizedArrayType convective_limit = 0.;
for (
unsigned int d = 0;
d < dim; ++
d)
const auto speed_of_sound =
std::sqrt(gamma * pressure * (1. / solution[0]));
for (
unsigned int d = 0;
d < dim; ++
d)
for (
unsigned int i = 0; i < 5; ++i)
(inverse_jacobian * eigenvector);
VectorizedArrayType eigenvector_norm = 0.;
for (
unsigned int d = 0;
d < dim; ++
d)
eigenvector /= eigenvector_norm;
const auto jac_times_ev = inverse_jacobian * eigenvector;
(jac_times_ev * jac_times_ev) / (eigenvector * eigenvector));
max_eigenvalue * speed_of_sound + convective_limit);
for (
unsigned int v = 0; v <
data.n_active_entries_per_cell_batch(cell);
max_transport =
std::max(max_transport, local_max[v]);
void make_grid_and_dofs();
void output_results(
const unsigned int result_number);
#ifdef DEAL_II_WITH_P4EST
EulerOperator<dim, fe_degree, n_q_points_1d> euler_operator;
virtual void evaluate_vector_field(
virtual std::vector<std::string> get_names()
const override;
get_data_component_interpretation()
const override;
virtual UpdateFlags get_needed_update_flags()
const override;
const bool do_schlieren_plot;
EulerProblem<dim>::Postprocessor::Postprocessor()
: do_schlieren_plot(dim == 2)
void EulerProblem<dim>::Postprocessor::evaluate_vector_field(
const unsigned int n_evaluation_points = inputs.solution_values.size();
if (do_schlieren_plot ==
true)
Assert(inputs.solution_gradients.size() == n_evaluation_points,
Assert(computed_quantities.size() == n_evaluation_points,
Assert(inputs.solution_values[0].size() == dim + 2, ExcInternalError());
dim + 2 + (do_schlieren_plot ==
true ? 1 : 0),
for (
unsigned int p = 0; p < n_evaluation_points; ++p)
for (
unsigned int d = 0;
d < dim + 2; ++
d)
solution[d] = inputs.solution_values[p](d);
const double density = solution[0];
const double pressure = euler_pressure<dim>(solution);
for (
unsigned int d = 0;
d < dim; ++
d)
computed_quantities[p](d) = velocity[
d];
computed_quantities[p](dim) = pressure;
computed_quantities[p](dim + 1) =
std::sqrt(gamma * pressure / density);
if (do_schlieren_plot ==
true)
computed_quantities[p](dim + 2) =
inputs.solution_gradients[p][0] * inputs.solution_gradients[p][0];
std::vector<std::string> EulerProblem<dim>::Postprocessor::get_names() const
std::vector<std::string> names;
for (
unsigned int d = 0;
d < dim; ++
d)
names.emplace_back(
"velocity");
names.emplace_back(
"pressure");
names.emplace_back(
"speed_of_sound");
if (do_schlieren_plot ==
true)
names.emplace_back(
"schlieren_plot");
std::vector<DataComponentInterpretation::DataComponentInterpretation>
EulerProblem<dim>::Postprocessor::get_data_component_interpretation() const
std::vector<DataComponentInterpretation::DataComponentInterpretation>
for (
unsigned int d = 0;
d < dim; ++
d)
interpretation.push_back(
if (do_schlieren_plot ==
true)
interpretation.push_back(
UpdateFlags EulerProblem<dim>::Postprocessor::get_needed_update_flags() const
if (do_schlieren_plot ==
true)
EulerProblem<dim>::EulerProblem()
#ifdef DEAL_II_WITH_P4EST
, triangulation(MPI_COMM_WORLD)
#endif
, dof_handler(triangulation)
void EulerProblem<dim>::make_grid_and_dofs()
for (
unsigned int d = 1;
d < dim; ++
d)
for (
unsigned int d = 1;
d < dim; ++
d)
triangulation.refine_global(2);
euler_operator.set_inflow_boundary(
0, std::make_unique<ExactSolution<dim>>(0));
triangulation, 0.03, 1, 0,
true);
euler_operator.set_inflow_boundary(
0, std::make_unique<ExactSolution<dim>>(0));
euler_operator.set_subsonic_outflow_boundary(
1, std::make_unique<ExactSolution<dim>>(0));
euler_operator.set_wall_boundary(2);
euler_operator.set_wall_boundary(3);
euler_operator.set_body_force(
std::vector<double>({0., 0., -0.2})));
triangulation.refine_global(n_global_refinements);
dof_handler.distribute_dofs(fe);
euler_operator.reinit(mapping, dof_handler);
euler_operator.initialize_vector(solution);
std::locale s = pcout.get_stream().getloc();
pcout.get_stream().imbue(std::locale(
""));
pcout <<
"Number of degrees of freedom: " << dof_handler.n_dofs()
<<
" ( = " << (dim + 2) <<
" [vars] x "
<< triangulation.n_global_active_cells() <<
" [cells] x "
pcout.get_stream().imbue(s);
void EulerProblem<dim>::output_results(
const unsigned int result_number)
{
const std::array<double, 3> errors =
euler_operator.compute_errors(ExactSolution<dim>(time), solution);
const std::string quantity_name = testcase == 0 ?
"error" :
"norm";
pcout <<
"Time:" << std::setw(8) << std::setprecision(3) << time
<<
", dt: " << std::setw(8) << std::setprecision(2) << time_step
<<
", " << quantity_name <<
" rho: " << std::setprecision(4)
<<
std::setw(10) << errors[0] << ", rho * u: " <<
std::setprecision(4)
<<
std::setw(10) << errors[1] << ", energy:" <<
std::setprecision(4)
<<
std::setw(10) << errors[2] <<
std::endl;
Postprocessor postprocessor;
data_out.set_flags(flags);
data_out.attach_dof_handler(dof_handler);
std::vector<std::string> names;
names.emplace_back(
"density");
for (
unsigned int d = 0;
d < dim; ++
d)
names.emplace_back(
"momentum");
names.emplace_back(
"energy");
std::vector<DataComponentInterpretation::DataComponentInterpretation>
interpretation.push_back(
for (
unsigned int d = 0;
d < dim; ++
d)
interpretation.push_back(
interpretation.push_back(
data_out.add_data_vector(dof_handler, solution, names, interpretation);
data_out.add_data_vector(solution, postprocessor);
if (testcase == 0 && dim == 2)
euler_operator.project(ExactSolution<dim>(time),
reference);
std::vector<std::string> names;
names.emplace_back(
"error_density");
for (
unsigned int d = 0;
d < dim; ++
d)
names.emplace_back(
"error_momentum");
names.emplace_back(
"error_energy");
std::vector<DataComponentInterpretation::DataComponentInterpretation>
interpretation.push_back(
for (
unsigned int d = 0;
d < dim; ++
d)
interpretation.push_back(
interpretation.push_back(
data_out.add_data_vector(dof_handler,
data_out.add_data_vector(mpi_owner,
"owner");
data_out.build_patches(mapping,
const std::string filename =
data_out.write_vtu_in_parallel(filename, MPI_COMM_WORLD);
void EulerProblem<dim>::run()
const unsigned int n_vect_number = VectorizedArrayType::size();
const unsigned int n_vect_bits = 8 *
sizeof(
Number) * n_vect_number;
<< " MPI processes" << std::endl;
pcout <<
"Vectorization over " << n_vect_number <<
' '
<< (std::is_same_v<Number, double> ?
"doubles" :
"floats") <<
" = "
<< n_vect_bits <<
" bits ("
const LowStorageRungeKuttaIntegrator integrator(lsrk_scheme);
rk_register_1.
reinit(solution);
rk_register_2.reinit(solution);
euler_operator.project(ExactSolution<dim>(time), solution);
double min_vertex_distance = std::numeric_limits<double>::max();
for (
const auto &cell : triangulation.active_cell_iterators())
if (cell->is_locally_owned())
std::
min(min_vertex_distance, cell->minimum_vertex_distance());
time_step = courant_number * integrator.n_stages() /
euler_operator.compute_cell_transport_speed(solution);
pcout <<
"Time step size: " << time_step
<<
", minimal h: " << min_vertex_distance
<<
", initial transport scaling: "
<< 1. / euler_operator.compute_cell_transport_speed(solution)
unsigned int timestep_number = 0;
while (time < final_time - 1e-12 && timestep_number < max_time_steps)
if (timestep_number % 5 == 0)
courant_number * integrator.n_stages() /
euler_operator.compute_cell_transport_speed(solution), 3);
integrator.perform_time_step(euler_operator,
if (
static_cast<int>(time / output_tick) !=
static_cast<int>((time - time_step) / output_tick) ||
time >= final_time - 1e-12)
static_cast<unsigned int>(std::round(time / output_tick)));
timer.print_wall_time_statistics(MPI_COMM_WORLD);
int main(
int argc,
char **argv)
{
using namespace Euler_DG;
EulerProblem<dimension> euler_problem;
catch (std::exception &exc)
<<
"----------------------------------------------------"
std::cerr <<
"Exception on processing: " << std::endl
<< exc.what() << std::endl
<<
"Aborting!" << std::endl
<<
"----------------------------------------------------"
<<
"----------------------------------------------------"
std::cerr <<
"Unknown exception!" << std::endl
<<
"Aborting!" << std::endl
<<
"----------------------------------------------------"
* * int main(int argc, char **argv)
void reinit(const size_type size, const bool omit_zeroing_entries=false)
DataComponentInterpretation
@ component_is_part_of_vector
void hyper_rectangle(Triangulation< dim, spacedim > &tria, const Point< dim > &p1, const Point< dim > &p2, const bool colorize=false)
void channel_with_cylinder(Triangulation< dim > &tria, const double shell_region_width=0.03, const unsigned int n_shells=2, const double skewness=2.0, const bool colorize=false)
* * if(update_pressure &update_flags) * compute_pressure(constitutive_request
* * * * ValueType TimeRateRequest< ValueType, dim, Number > get_value() const
* * * * std::vector< Number > ThermoPlasticMaterial< dim, ViscoplasticYieldLaw, Number >::get_state_parameters const
T sum(const T &t, const MPI_Comm mpi_communicator)
unsigned int n_mpi_processes(const MPI_Comm mpi_communicator)
T max(const T &t, const MPI_Comm mpi_communicator)
T min(const T &t, const MPI_Comm mpi_communicator)
std::string get_current_vectorization_level()
Number truncate_to_n_digits(const Number number, const unsigned int n_digits)
std::string int_to_string(const unsigned int value, const unsigned int digits=numbers::invalid_unsigned_int)
constexpr T pow(const T base, const int iexp)
void run(const Iterator &begin, const std_cxx20::type_identity_t< Iterator > &end, Worker worker, Copier copier, const ScratchData &sample_scratch_data, const CopyData &sample_copy_data, const unsigned int queue_length, const unsigned int chunk_size)
bool write_higher_order_cells
Running the program with the default settings on a machine with 24 processes in release mode and AVX2 vectorization produces the following output:
While the performance in this small test case is almost identical, the difference depends on the hardware and the dimension and size of the setup. In larger computations we have seen that the modifications shown in this tutorial were able to achieve a speedup of 27% for the Runge-Kutta stages.
The solver presented in this tutorial program can also be extended to the compressible Navier–Stokes equations by adding viscous terms, as also suggested in step-67. To keep as much of the performance obtained here despite the additional cost of elliptic terms, e.g. via an interior penalty method, that tutorial has proposed to switch the basis from FE_DGQ to FE_DGQHermite like in the step-59 tutorial program. The reasoning behind this switch is that in the case of FE_DGQ all values of neighboring cells (i.e., \(k+1\) layers) are needed, whilst in the case of FE_DGQHermite only 2 layers, making the latter significantly more suitable for higher degrees. The additional layers have to be, on the one hand, loaded from main memory during flux computation and, one the other hand, have to be communicated. Using the shared-memory capabilities introduced in this tutorial, the second point can be eliminated on a single compute node or its influence can be reduced in a hybrid context.
Cell-centric loops could be used to create block Gauss-Seidel preconditioners that are multiplicative within one process and additive over processes. These type of preconditioners use during flux computation, in contrast to Jacobi-type preconditioners, already updated values from neighboring cells. The following pseudo-code visualizes how this could in principal be achieved:
#include <fstream>
#include <iomanip>
#include <iostream>
namespace Euler_DG
{
constexpr unsigned int testcase = 1;
constexpr unsigned int dimension = 2;
constexpr unsigned int n_global_refinements = 2;
constexpr unsigned int fe_degree = 5;
constexpr unsigned int n_q_points_1d = fe_degree + 2;
using Number = double;
constexpr double gamma = 1.4;
constexpr double final_time = testcase == 0 ? 10 : 2.0;
constexpr double output_tick = testcase == 0 ? 1 : 0.05;
const double courant_number = 0.15 /
std::pow(fe_degree, 1.5);
enum LowStorageRungeKuttaScheme
{
stage_3_order_3,
stage_5_order_4,
stage_7_order_4,
stage_9_order_5,
};
constexpr LowStorageRungeKuttaScheme lsrk_scheme = stage_5_order_4;
class LowStorageRungeKuttaIntegrator
{
public:
LowStorageRungeKuttaIntegrator(const LowStorageRungeKuttaScheme scheme)
{
switch (scheme)
{
case stage_3_order_3:
break;
case stage_5_order_4:
break;
case stage_7_order_4:
break;
case stage_9_order_5:
break;
default:
}
rk_integrator(lsrk);
std::vector<double> ci;
rk_integrator.get_coefficients(ai, bi, ci);
}
unsigned int n_stages() const
{
return bi.size();
}
template <typename VectorType, typename Operator>
void perform_time_step(const Operator &pde_operator,
const double current_time,
const double time_step,
VectorType &solution,
VectorType &vec_ri,
VectorType &vec_ki) const
{
vec_ki.swap(solution);
double sum_previous_bi = 0;
for (unsigned int stage = 0; stage < bi.size(); ++stage)
{
const double c_i = stage == 0 ? 0 : sum_previous_bi + ai[stage - 1];
pde_operator.perform_stage(stage,
current_time + c_i * time_step,
bi[stage] * time_step,
(stage == bi.size() - 1 ?
0 :
ai[stage] * time_step),
(stage % 2 == 0 ? vec_ki : vec_ri),
(stage % 2 == 0 ? vec_ri : vec_ki),
solution);
if (stage > 0)
sum_previous_bi += bi[stage - 1];
}
}
private:
std::vector<double> bi;
std::vector<double> ai;
};
enum EulerNumericalFlux
{
lax_friedrichs_modified,
harten_lax_vanleer,
};
constexpr EulerNumericalFlux numerical_flux_type = lax_friedrichs_modified;
template <int dim>
class ExactSolution :
public Function<dim>
{
public:
ExactSolution(const double time)
{}
const unsigned int component = 0) const override;
};
template <int dim>
double ExactSolution<dim>::value(
const Point<dim> &x,
const unsigned int component) const
{
switch (testcase)
{
case 0:
{
Assert(dim == 2, ExcNotImplemented());
const double beta = 5;
x0[0] = 5.;
const double radius_sqr =
(x - x0).norm_square() - 2. * (x[0] - x0[0]) * t + t * t;
const double factor =
const double density_log = std::log2(
std::abs(1. - (gamma - 1.) / gamma * 0.25 * factor * factor));
const double density = std::exp2(density_log * (1. / (gamma - 1.)));
const double u = 1. - factor * (x[1] - x0[1]);
const double v = factor * (x[0] - t - x0[0]);
if (component == 0)
return density;
else if (component == 1)
return density * u;
else if (component == 2)
return density * v;
else
{
const double pressure =
std::exp2(density_log * (gamma / (gamma - 1.)));
return pressure / (
gamma - 1.) +
0.5 * (density * u * u + density * v * v);
}
}
case 1:
{
if (component == 0)
return 1.;
else if (component == 1)
return 0.4;
else if (component == dim + 1)
return 3.097857142857143;
else
return 0.;
}
default:
return 0.;
}
}
template <int dim, typename Number>
{
const Number inverse_density =
Number(1.) / conserved_variables[0];
for (
unsigned int d = 0;
d < dim; ++
d)
velocity[d] = conserved_variables[1 + d] * inverse_density;
return velocity;
}
template <int dim, typename Number>
{
euler_velocity<dim>(conserved_variables);
Number rho_u_dot_u = conserved_variables[1] * velocity[0];
for (
unsigned int d = 1;
d < dim; ++
d)
rho_u_dot_u += conserved_variables[1 + d] * velocity[d];
return (gamma - 1.) * (conserved_variables[dim + 1] - 0.5 * rho_u_dot_u);
}
template <int dim, typename Number>
{
euler_velocity<dim>(conserved_variables);
const Number pressure = euler_pressure<dim>(conserved_variables);
for (
unsigned int d = 0;
d < dim; ++
d)
{
flux[0][
d] = conserved_variables[1 +
d];
for (
unsigned int e = 0;
e < dim; ++
e)
flux[e + 1][d] = conserved_variables[e + 1] * velocity[d];
flux[
d + 1][
d] += pressure;
velocity[
d] * (conserved_variables[dim + 1] + pressure);
}
return flux;
}
template <int n_components, int dim, typename Number>
{
for (
unsigned int d = 0;
d < n_components; ++
d)
result[d] = matrix[d] * vector;
return result;
}
template <int dim, typename Number>
{
const auto velocity_m = euler_velocity<dim>(u_m);
const auto velocity_p = euler_velocity<dim>(u_p);
const auto pressure_m = euler_pressure<dim>(u_m);
const auto pressure_p = euler_pressure<dim>(u_p);
const auto flux_m = euler_flux<dim>(u_m);
const auto flux_p = euler_flux<dim>(u_p);
switch (numerical_flux_type)
{
case lax_friedrichs_modified:
{
gamma * pressure_p * (1. / u_p[0]),
velocity_m.norm_square() +
gamma * pressure_m * (1. / u_m[0])));
return 0.5 * (flux_m * normal + flux_p * normal) +
0.5 * lambda * (u_m - u_p);
}
case harten_lax_vanleer:
{
const auto avg_velocity_normal =
0.5 * ((velocity_m + velocity_p) * normal);
0.5 * gamma *
(pressure_p * (1. / u_p[0]) + pressure_m * (1. / u_m[0]))));
return inverse_s *
((s_pos * (flux_m * normal) - s_neg * (flux_p * normal)) -
s_pos * s_neg * (u_m - u_p));
}
default:
{
return {};
}
}
}
template <int dim, typename VectorizedArrayType>
VectorizedArrayType
const unsigned int component)
{
VectorizedArrayType result;
for (unsigned int v = 0; v < VectorizedArrayType::size(); ++v)
{
for (
unsigned int d = 0;
d < dim; ++
d)
p[d] = p_vectorized[d][v];
result[v] = function.
value(p, component);
}
return result;
}
template <int dim, typename VectorizedArrayType, int n_components = dim + 2>
{
for (unsigned int v = 0; v < VectorizedArrayType::size(); ++v)
{
for (
unsigned int d = 0;
d < dim; ++
d)
p[d] = p_vectorized[d][v];
for (
unsigned int d = 0;
d < n_components; ++
d)
result[d][v] = function.
value(p, d);
}
return result;
}
template <int dim, int degree, int n_points_1d>
class EulerOperator
{
public:
static constexpr unsigned int n_quadrature_points_1d = n_points_1d;
~EulerOperator();
void set_subsonic_outflow_boundary(
void
perform_stage(const unsigned int stage,
const Number cur_time,
const Number bi,
const Number ai,
std::array<double, 3> compute_errors(
double compute_cell_transport_speed(
void
private:
std::map<types::boundary_id, std::unique_ptr<Function<dim>>>
inflow_boundaries;
std::map<types::boundary_id, std::unique_ptr<Function<dim>>>
subsonic_outflow_boundaries;
std::set<types::boundary_id> wall_boundaries;
std::unique_ptr<Function<dim>> body_force;
};
template <int dim, int degree, int n_points_1d>
EulerOperator<dim, degree, n_points_1d>::EulerOperator(
TimerOutput &timer)
: timer(timer)
{
#ifdef DEAL_II_WITH_MPI
if (group_size == 1)
{
this->subcommunicator = MPI_COMM_SELF;
}
{
MPI_Comm_split_type(MPI_COMM_WORLD,
MPI_COMM_TYPE_SHARED,
rank,
MPI_INFO_NULL,
&subcommunicator);
}
else
{
}
#else
(void)subcommunicator;
(void)group_size;
this->subcommunicator = MPI_COMM_SELF;
#endif
}
template <int dim, int degree, int n_points_1d>
EulerOperator<dim, degree, n_points_1d>::~EulerOperator()
{
#ifdef DEAL_II_WITH_MPI
if (this->subcommunicator != MPI_COMM_SELF)
MPI_Comm_free(&subcommunicator);
#endif
}
template <int dim, int degree, int n_points_1d>
void EulerOperator<dim, degree, n_points_1d>::reinit(
{
const std::vector<const DoFHandler<dim> *> dof_handlers = {&dof_handler};
const std::vector<const AffineConstraints<double> *> constraints = {&dummy};
const std::vector<Quadrature<1>> quadratures = {
QGauss<1>(n_q_points_1d),
additional_data;
additional_data);
mapping, dof_handlers, constraints, quadratures, additional_data);
}
template <int dim, int degree, int n_points_1d>
void EulerOperator<dim, degree, n_points_1d>::perform_stage(
const unsigned int stage,
const Number current_time,
const Number bi,
const Number ai,
{
for (auto &i : inflow_boundaries)
i.
second->set_time(current_time);
for (auto &i : subsonic_outflow_boundaries)
i.
second->set_time(current_time);
data.template loop_cell_centric<LinearAlgebra::distributed::Vector<Number>,
[&](
const auto &
data,
auto &dst,
const auto &src,
const auto cell_range) {
degree,
n_points_1d,
dim + 2,
VectorizedArrayType>;
degree,
n_points_1d,
dim + 2,
VectorizedArrayType>;
FECellIntegral phi(
data);
FECellIntegral phi_temp(
data);
FEFaceIntegral phi_m(
data,
true);
FEFaceIntegral phi_p(
data,
false);
if (constant_function)
constant_body_force =
evaluate_function<dim, VectorizedArrayType, dim>(
dim,
n_points_1d,
n_points_1d,
VectorizedArrayType,
eval({},
data.get_shape_info().
data[0].shape_gradients_collocation_eo,
{});
phi.n_components);
for (unsigned int cell = cell_range.first; cell < cell_range.second;
++cell)
{
phi.reinit(cell);
phi_temp.reinit(cell);
if (ai !=
Number() && stage == 0)
{
phi.read_dof_values(src);
for (unsigned int i = 0;
i < phi.static_dofs_per_component * (dim + 2);
++i)
phi_temp.begin_dof_values()[i] = phi.begin_dof_values()[i];
}
else
{
}
for (unsigned int i = 0; i < phi.static_n_q_points * (dim + 2); ++i)
buffer[i] = phi.begin_values()[i];
for (const unsigned int q : phi.quadrature_point_indices())
{
const auto w_q = phi.get_value(q);
phi.submit_gradient(euler_flux<dim>(w_q), q);
if (body_force.get() != nullptr)
{
constant_function ?
constant_body_force :
evaluate_function<dim, VectorizedArrayType, dim>(
*body_force, phi.quadrature_point(q));
for (
unsigned int d = 0;
d < dim; ++
d)
forcing[d + 1] = w_q[0] * force[d];
for (
unsigned int d = 0;
d < dim; ++
d)
forcing[dim + 1] += force[d] * w_q[d + 1];
phi.submit_value(forcing, q);
}
}
{
auto *values_ptr = phi.begin_values();
auto *gradient_ptr = phi.begin_gradients();
for (unsigned int c = 0; c < dim + 2; ++c)
{
if (dim >= 1 && body_force.get() == nullptr)
eval.template gradients<0, false, false, dim>(gradient_ptr,
values_ptr);
else if (dim >= 1)
eval.template gradients<0, false, true, dim>(gradient_ptr,
values_ptr);
if (dim >= 2)
eval.template gradients<1, false, true, dim>(gradient_ptr +
1,
values_ptr);
if (dim >= 3)
eval.template gradients<2, false, true, dim>(gradient_ptr +
2,
values_ptr);
values_ptr += phi.static_n_q_points;
gradient_ptr += phi.static_n_q_points * dim;
}
}
for (unsigned int face = 0;
face < GeometryInfo<dim>::faces_per_cell;
++face)
{
const auto boundary_ids =
data.get_faces_by_cells_boundary_id(cell, face);
Assert(std::equal(boundary_ids.begin(),
boundary_ids.begin() +
data.n_active_entries_per_cell_batch(cell),
boundary_ids.begin()),
ExcMessage("Boundary IDs of lanes differ."));
phi_m.reinit(cell, face);
n_points_1d - 1,
VectorizedArrayType>::
template interpolate_quadrature<true, false>(
dim + 2,
buffer.data(),
phi_m.begin_values(),
face);
{
phi_p.reinit(cell, face);
for (const unsigned int q :
phi_m.quadrature_point_indices())
{
const auto numerical_flux =
euler_numerical_flux<dim>(phi_m.get_value(q),
phi_p.get_value(q),
phi_m.normal_vector(q));
phi_m.submit_value(-numerical_flux, q);
}
}
else
{
for (const unsigned int q :
phi_m.quadrature_point_indices())
{
const auto w_m = phi_m.get_value(q);
const auto normal = phi_m.normal_vector(q);
auto rho_u_dot_n = w_m[1] * normal[0];
for (
unsigned int d = 1;
d < dim; ++
d)
rho_u_dot_n += w_m[1 + d] * normal[d];
bool at_outflow = false;
if (wall_boundaries.find(boundary_id) !=
wall_boundaries.end())
{
w_p[0] = w_m[0];
for (
unsigned int d = 0;
d < dim; ++
d)
w_p[d + 1] =
w_m[d + 1] - 2. * rho_u_dot_n * normal[d];
w_p[dim + 1] = w_m[dim + 1];
}
else if (inflow_boundaries.find(boundary_id) !=
inflow_boundaries.end())
w_p = evaluate_function(
*inflow_boundaries.find(boundary_id)->second,
phi_m.quadrature_point(q));
else if (subsonic_outflow_boundaries.find(
boundary_id) !=
subsonic_outflow_boundaries.end())
{
w_p = w_m;
w_p[dim + 1] =
evaluate_function(*subsonic_outflow_boundaries
.find(boundary_id)
phi_m.quadrature_point(q),
dim + 1);
at_outflow = true;
}
else
ExcMessage(
"Unknown boundary id, did "
"you set a boundary condition for "
"this part of the domain boundary?"));
auto flux = euler_numerical_flux<dim>(w_m, w_p, normal);
if (at_outflow)
for (unsigned int v = 0;
v < VectorizedArrayType::size();
++v)
{
if (rho_u_dot_n[v] < -1e-12)
for (
unsigned int d = 0;
d < dim; ++
d)
flux[d + 1][v] = 0.;
}
phi_m.submit_value(-flux, q);
}
}
n_points_1d - 1,
VectorizedArrayType>::
template interpolate_quadrature<false, true>(
dim + 2,
phi_m.begin_values(),
phi.begin_values(),
face);
}
for (unsigned int q = 0; q < phi.static_n_q_points; ++q)
{
const auto factor = VectorizedArrayType(1.0) / phi.JxW(q);
for (unsigned int c = 0; c < dim + 2; ++c)
phi.begin_values()[c * phi.static_n_q_points + q] =
phi.begin_values()[c * phi.static_n_q_points + q] * factor;
}
dim,
degree + 1,
n_points_1d>::do_backward(dim + 2,
.data[0]
.inverse_shape_values_eo,
false,
phi.begin_values(),
phi.begin_dof_values());
{
for (unsigned int q = 0; q < phi.static_dofs_per_cell; ++q)
phi.begin_dof_values()[q] = bi * phi.begin_dof_values()[q];
phi.distribute_local_to_global(solution);
}
else
{
if (stage != 0)
phi_temp.read_dof_values(solution);
for (unsigned int q = 0; q < phi.static_dofs_per_cell; ++q)
{
const auto K_i = phi.begin_dof_values()[q];
phi.begin_dof_values()[q] =
phi_temp.begin_dof_values()[q] + (ai * K_i);
phi_temp.begin_dof_values()[q] += bi * K_i;
}
phi.set_dof_values(dst);
phi_temp.set_dof_values(solution);
}
}
},
vec_ki,
current_ri,
true,
}
template <int dim, int degree, int n_points_1d>
void EulerOperator<dim, degree, n_points_1d>::initialize_vector(
{
data.initialize_dof_vector(vector);
}
template <int dim, int degree, int n_points_1d>
void EulerOperator<dim, degree, n_points_1d>::set_inflow_boundary(
{
AssertThrow(subsonic_outflow_boundaries.find(boundary_id) ==
subsonic_outflow_boundaries.end() &&
wall_boundaries.find(boundary_id) == wall_boundaries.end(),
ExcMessage("You already set the boundary with id " +
std::to_string(static_cast<int>(boundary_id)) +
" to another type of boundary before now setting " +
"it as inflow"));
ExcMessage("Expected function with dim+2 components"));
inflow_boundaries[
boundary_id] = std::move(inflow_function);
}
template <int dim, int degree, int n_points_1d>
void EulerOperator<dim, degree, n_points_1d>::set_subsonic_outflow_boundary(
{
inflow_boundaries.end() &&
wall_boundaries.find(boundary_id) == wall_boundaries.end(),
ExcMessage("You already set the boundary with id " +
std::to_string(static_cast<int>(boundary_id)) +
" to another type of boundary before now setting " +
"it as subsonic outflow"));
ExcMessage("Expected function with dim+2 components"));
subsonic_outflow_boundaries[
boundary_id] = std::move(outflow_function);
}
template <int dim, int degree, int n_points_1d>
void EulerOperator<dim, degree, n_points_1d>::set_wall_boundary(
{
inflow_boundaries.end() &&
subsonic_outflow_boundaries.find(boundary_id) ==
subsonic_outflow_boundaries.end(),
ExcMessage("You already set the boundary with id " +
std::to_string(static_cast<int>(boundary_id)) +
" to another type of boundary before now setting " +
"it as wall boundary"));
wall_boundaries.insert(boundary_id);
}
template <int dim, int degree, int n_points_1d>
void EulerOperator<dim, degree, n_points_1d>::set_body_force(
{
this->body_force = std::move(body_force);
}
template <int dim, int degree, int n_points_1d>
void EulerOperator<dim, degree, n_points_1d>::project(
{
degree,
dim + 2,
VectorizedArrayType>
inverse(phi);
for (
unsigned int cell = 0; cell <
data.n_cell_batches(); ++cell)
{
phi.reinit(cell);
for (const unsigned int q : phi.quadrature_point_indices())
phi.submit_dof_value(evaluate_function(function,
phi.quadrature_point(q)),
q);
inverse.transform_from_q_points_to_basis(dim + 2,
phi.begin_dof_values(),
phi.begin_dof_values());
phi.set_dof_values(solution);
}
}
template <int dim, int degree, int n_points_1d>
std::array<double, 3> EulerOperator<dim, degree, n_points_1d>::compute_errors(
{
double errors_squared[3] = {};
for (
unsigned int cell = 0; cell <
data.n_cell_batches(); ++cell)
{
phi.reinit(cell);
VectorizedArrayType local_errors_squared[3] = {};
for (const unsigned int q : phi.quadrature_point_indices())
{
const auto error =
evaluate_function(function, phi.quadrature_point(q)) -
phi.get_value(q);
const auto JxW = phi.JxW(q);
local_errors_squared[0] += error[0] * error[0] * JxW;
for (
unsigned int d = 0;
d < dim; ++
d)
local_errors_squared[1] += (error[d + 1] * error[d + 1]) * JxW;
local_errors_squared[2] += (error[dim + 1] * error[dim + 1]) * JxW;
}
for (
unsigned int v = 0; v <
data.n_active_entries_per_cell_batch(cell);
++v)
for (
unsigned int d = 0;
d < 3; ++
d)
errors_squared[d] += local_errors_squared[d][v];
}
std::array<double, 3> errors;
for (
unsigned int d = 0;
d < 3; ++
d)
return errors;
}
template <int dim, int degree, int n_points_1d>
double EulerOperator<dim, degree, n_points_1d>::compute_cell_transport_speed(
{
for (
unsigned int cell = 0; cell <
data.n_cell_batches(); ++cell)
{
phi.reinit(cell);
VectorizedArrayType local_max = 0.;
for (const unsigned int q : phi.quadrature_point_indices())
{
const auto solution = phi.get_value(q);
const auto velocity = euler_velocity<dim>(solution);
const auto pressure = euler_pressure<dim>(solution);
const auto inverse_jacobian = phi.inverse_jacobian(q);
const auto convective_speed = inverse_jacobian * velocity;
VectorizedArrayType convective_limit = 0.;
for (
unsigned int d = 0;
d < dim; ++
d)
convective_limit =
const auto speed_of_sound =
std::sqrt(gamma * pressure * (1. / solution[0]));
for (
unsigned int d = 0;
d < dim; ++
d)
eigenvector[d] = 1.;
for (unsigned int i = 0; i < 5; ++i)
{
(inverse_jacobian * eigenvector);
VectorizedArrayType eigenvector_norm = 0.;
for (
unsigned int d = 0;
d < dim; ++
d)
eigenvector_norm =
eigenvector /= eigenvector_norm;
}
const auto jac_times_ev = inverse_jacobian * eigenvector;
(jac_times_ev * jac_times_ev) / (eigenvector * eigenvector));
local_max =
max_eigenvalue * speed_of_sound + convective_limit);
}
for (
unsigned int v = 0; v <
data.n_active_entries_per_cell_batch(cell);
++v)
max_transport =
std::max(max_transport, local_max[v]);
}
return max_transport;
}
template <int dim>
class EulerProblem
{
public:
EulerProblem();
private:
void make_grid_and_dofs();
void output_results(const unsigned int result_number);
#ifdef DEAL_II_WITH_P4EST
#else
#endif
EulerOperator<dim, fe_degree, n_q_points_1d> euler_operator;
double time, time_step;
{
public:
Postprocessor();
virtual void evaluate_vector_field(
virtual std::vector<std::string> get_names() const override;
virtual std::vector<
get_data_component_interpretation() const override;
virtual UpdateFlags get_needed_update_flags()
const override;
private:
const bool do_schlieren_plot;
};
};
template <int dim>
EulerProblem<dim>::Postprocessor::Postprocessor()
: do_schlieren_plot(dim == 2)
{}
template <int dim>
void EulerProblem<dim>::Postprocessor::evaluate_vector_field(
{
if (do_schlieren_plot == true)
ExcInternalError());
Assert(computed_quantities.size() == n_evaluation_points,
ExcInternalError());
dim + 2 + (do_schlieren_plot == true ? 1 : 0),
ExcInternalError());
for (unsigned int p = 0; p < n_evaluation_points; ++p)
{
for (
unsigned int d = 0;
d < dim + 2; ++
d)
const double density = solution[0];
const double pressure = euler_pressure<dim>(solution);
for (
unsigned int d = 0;
d < dim; ++
d)
computed_quantities[p](d) = velocity[
d];
computed_quantities[p](dim) = pressure;
computed_quantities[p](dim + 1) =
std::sqrt(gamma * pressure / density);
if (do_schlieren_plot == true)
computed_quantities[p](dim + 2) =
}
}
template <int dim>
std::vector<std::string> EulerProblem<dim>::Postprocessor::get_names() const
{
std::vector<std::string> names;
for (
unsigned int d = 0;
d < dim; ++
d)
names.emplace_back("velocity");
names.emplace_back("pressure");
names.emplace_back("speed_of_sound");
if (do_schlieren_plot == true)
names.emplace_back("schlieren_plot");
return names;
}
template <int dim>
std::vector<DataComponentInterpretation::DataComponentInterpretation>
EulerProblem<dim>::Postprocessor::get_data_component_interpretation() const
{
std::vector<DataComponentInterpretation::DataComponentInterpretation>
interpretation;
for (
unsigned int d = 0;
d < dim; ++
d)
interpretation.push_back(
if (do_schlieren_plot == true)
interpretation.push_back(
return interpretation;
}
template <int dim>
UpdateFlags EulerProblem<dim>::Postprocessor::get_needed_update_flags()
const
{
if (do_schlieren_plot == true)
else
}
template <int dim>
EulerProblem<dim>::EulerProblem()
#ifdef DEAL_II_WITH_P4EST
, triangulation(MPI_COMM_WORLD)
#endif
, fe(
FE_DGQ<dim>(fe_degree), dim + 2)
, mapping(fe_degree)
, dof_handler(triangulation)
, euler_operator(timer)
, time(0)
, time_step(0)
{}
template <int dim>
void EulerProblem<dim>::make_grid_and_dofs()
{
switch (testcase)
{
case 0:
{
for (
unsigned int d = 1;
d < dim; ++
d)
lower_left[d] = -5;
upper_right[0] = 10;
for (
unsigned int d = 1;
d < dim; ++
d)
upper_right[d] = 5;
lower_left,
upper_right);
triangulation.refine_global(2);
euler_operator.set_inflow_boundary(
0, std::make_unique<ExactSolution<dim>>(0));
break;
}
case 1:
{
triangulation, 0.03, 1, 0, true);
euler_operator.set_inflow_boundary(
0, std::make_unique<ExactSolution<dim>>(0));
euler_operator.set_subsonic_outflow_boundary(
1, std::make_unique<ExactSolution<dim>>(0));
euler_operator.set_wall_boundary(2);
euler_operator.set_wall_boundary(3);
if (dim == 3)
euler_operator.set_body_force(
std::vector<double>({0., 0., -0.2})));
break;
}
default:
}
triangulation.refine_global(n_global_refinements);
euler_operator.reinit(mapping, dof_handler);
euler_operator.initialize_vector(solution);
std::locale s = pcout.get_stream().getloc();
pcout.get_stream().imbue(std::locale(""));
pcout <<
"Number of degrees of freedom: " << dof_handler.
n_dofs()
<< " ( = " << (dim + 2) << " [vars] x "
<< triangulation.n_global_active_cells() << " [cells] x "
<< std::endl;
pcout.get_stream().imbue(s);
}
template <int dim>
void EulerProblem<dim>::output_results(const unsigned int result_number)
{
const std::array<double, 3> errors =
euler_operator.compute_errors(ExactSolution<dim>(time), solution);
const std::string quantity_name = testcase == 0 ? "error" : "norm";
pcout << "Time:" << std::setw(8) << std::setprecision(3) << time
<< ", dt: " << std::setw(8) << std::setprecision(2) << time_step
<< ", " << quantity_name << " rho: " << std::setprecision(4)
<< std::setw(10) << errors[0] << ", rho * u: " << std::setprecision(4)
<< std::setw(10) << errors[1] << ", energy:" << std::setprecision(4)
<< std::setw(10) << errors[2] << std::endl;
{
Postprocessor postprocessor;
{
std::vector<std::string> names;
names.emplace_back("density");
for (
unsigned int d = 0;
d < dim; ++
d)
names.emplace_back("momentum");
names.emplace_back("energy");
std::vector<DataComponentInterpretation::DataComponentInterpretation>
interpretation;
interpretation.push_back(
for (
unsigned int d = 0;
d < dim; ++
d)
interpretation.push_back(
interpretation.push_back(
}
if (testcase == 0 && dim == 2)
{
euler_operator.project(ExactSolution<dim>(time),
reference);
std::vector<std::string> names;
names.emplace_back("error_density");
for (
unsigned int d = 0;
d < dim; ++
d)
names.emplace_back("error_momentum");
names.emplace_back("error_energy");
std::vector<DataComponentInterpretation::DataComponentInterpretation>
interpretation;
interpretation.push_back(
for (
unsigned int d = 0;
d < dim; ++
d)
interpretation.push_back(
interpretation.push_back(
names,
interpretation);
}
fe.degree,
const std::string filename =
}
}
template <int dim>
void EulerProblem<dim>::run()
{
{
const unsigned int n_vect_number = VectorizedArrayType::size();
const unsigned int n_vect_bits = 8 *
sizeof(
Number) * n_vect_number;
pcout << "Running with "
<< " MPI processes" << std::endl;
pcout << "Vectorization over " << n_vect_number << ' '
<< (std::is_same_v<Number, double> ? "doubles" : "floats") << " = "
<< n_vect_bits << " bits ("
<< std::endl;
}
make_grid_and_dofs();
const LowStorageRungeKuttaIntegrator integrator(lsrk_scheme);
rk_register_1.
reinit(solution);
rk_register_2.
reinit(solution);
euler_operator.project(ExactSolution<dim>(time), solution);
double min_vertex_distance = std::numeric_limits<double>::max();
for (const auto &cell : triangulation.active_cell_iterators())
if (cell->is_locally_owned())
min_vertex_distance =
std::
min(min_vertex_distance, cell->minimum_vertex_distance());
min_vertex_distance =
time_step = courant_number * integrator.n_stages() /
euler_operator.compute_cell_transport_speed(solution);
pcout << "Time step size: " << time_step
<< ", minimal h: " << min_vertex_distance
<< ", initial transport scaling: "
<< 1. / euler_operator.compute_cell_transport_speed(solution)
<< std::endl
<< std::endl;
output_results(0);
unsigned int timestep_number = 0;
while (time < final_time - 1e-12 && timestep_number < max_time_steps)
{
++timestep_number;
if (timestep_number % 5 == 0)
time_step =
courant_number * integrator.n_stages() /
euler_operator.compute_cell_transport_speed(solution), 3);
{
integrator.perform_time_step(euler_operator,
time,
time_step,
solution,
rk_register_1,
rk_register_2);
}
time += time_step;
if (static_cast<int>(time / output_tick) !=
static_cast<int>((time - time_step) / output_tick) ||
time >= final_time - 1e-12)
output_results(
static_cast<unsigned int>(std::round(time / output_tick)));
}
pcout << std::endl;
}
}
int main(
int argc,
char **argv)
{
using namespace Euler_DG;
try
{
EulerProblem<dimension> euler_problem;
euler_problem.run();
}
catch (std::exception &exc)
{
std::cerr << std::endl
<< std::endl
<< "----------------------------------------------------"
<< std::endl;
std::cerr << "Exception on processing: " << std::endl
<< exc.what() << std::endl
<< "Aborting!" << std::endl
<< "----------------------------------------------------"
<< std::endl;
return 1;
}
catch (...)
{
std::cerr << std::endl
<< std::endl
<< "----------------------------------------------------"
<< std::endl;
std::cerr << "Unknown exception!" << std::endl
<< "Aborting!" << std::endl
<< "----------------------------------------------------"
<< std::endl;
return 1;
}
return 0;
}
void write_vtu_in_parallel(const std::string &filename, const MPI_Comm comm) const
void set_flags(const FlagType &flags)
void attach_dof_handler(const DoFHandler< dim, spacedim > &)
void add_data_vector(const VectorType &data, const std::vector< std::string > &names, const DataVectorType type=type_automatic, const std::vector< DataComponentInterpretation::DataComponentInterpretation > &data_component_interpretation={})
virtual void build_patches(const unsigned int n_subdivisions=0)
void distribute_dofs(const FiniteElement< dim, spacedim > &fe)
const Triangulation< dim, spacedim > & get_triangulation() const
types::global_dof_index n_dofs() const
void zero_out_ghost_values() const
void print_wall_time_statistics(const MPI_Comm mpi_communicator_statistics, const double print_quantile=0.) const
void reinit(MatrixBlock< MatrixType > &v, const BlockSparsityPattern &p)
std::vector<::Vector< double > > solution_values
std::vector< std::vector< Tensor< 1, spacedim > > > solution_gradients
TasksParallelScheme tasks_parallel_scheme