示例#1
0
文件: SU2_MAC.cpp 项目: shyang5/SU2
int main(int argc, char *argv[]) {
	
	/*--- Variable definitions ---*/
	char file_name[200];
  unsigned short nZone = 1;
  
#ifndef NO_MPI
#ifdef WINDOWS
	MPI_Init(&argc,&argv);
#else
	MPI::Init(argc, argv);
#endif
#endif
	
	/*--- Definition of the config problem ---*/
	CConfig *config;
	if (argc == 2) config = new CConfig(argv[1], SU2_MAC, ZONE_0, nZone, VERB_HIGH);
	else { strcpy (file_name, "default.cfg"); config = new CConfig(file_name, SU2_MAC, ZONE_0, nZone, VERB_HIGH); }
	
	/*--- Definition of the Class for the geometry ---*/
	CGeometry *geometry; geometry = new CGeometry;
	geometry = new CPhysicalGeometry(config, ZONE_0, nZone);
	
  /*--- Perform the non-dimensionalization, in case any values are needed ---*/
  config->SetNondimensionalization(geometry->GetnDim(), ZONE_0);
  
	cout << endl <<"----------------------- Preprocessing computations ----------------------" << endl;
	
	/*--- Compute elements surrounding points, points surrounding points, and elements surronding elements ---*/
	cout << "Setting local point and element connectivity." <<endl;
	geometry->SetEsuP(); geometry->SetPsuP(); geometry->SetEsuE();
	
	/*--- Check the orientation before computing geometrical quantities ---*/
	cout << "Check numerical grid orientation." <<endl;
	geometry->SetBoundVolume(); geometry->Check_Orientation(config);
	
	/*--- Create the edge structure ---*/
	cout << "Identify faces, edges and vertices." <<endl;
	geometry->SetFaces(); geometry->SetEdges(); geometry->SetVertex(config); geometry->SetCG();
	
	/*--- Create the control volume structures ---*/
	cout << "Set control volume structure." << endl;
	geometry->SetControlVolume(config, ALLOCATE); geometry->SetBoundControlVolume(config, ALLOCATE);
	
	/*--- Set the near-field and interface boundary conditions  ---*/
	geometry->MatchNearField(config);
	
	if (config->GetKind_Adaptation() != NONE) {
		
		cout << endl <<"--------------------- Start numerical grid adaptation -------------------" << endl;
		
		/*-- Definition of the Class for grid adaptation ---*/
		CGridAdaptation *grid_adaptation;
		grid_adaptation = new CGridAdaptation(geometry, config);
		
		/*--- Read the flow solution and/or the adjoint solution
		 and choose the elements to adapt ---*/
		if ((config->GetKind_Adaptation() != NONE) && (config->GetKind_Adaptation() != FULL)
				&& (config->GetKind_Adaptation() != WAKE) && (config->GetKind_Adaptation() != TWOPHASE)
				&& (config->GetKind_Adaptation() != SMOOTHING) && (config->GetKind_Adaptation() != SUPERSONIC_SHOCK))
			grid_adaptation->GetFlowSolution(geometry, config);
		
		switch (config->GetKind_Adaptation()) {
			case NONE:
				break;
			case SMOOTHING:
				config->SetSmoothNumGrid(true);
				grid_adaptation->SetNo_Refinement(geometry, 1);
				break;
			case FULL:
				grid_adaptation->SetComplete_Refinement(geometry, 1);
				break;
			case WAKE:
				grid_adaptation->SetWake_Refinement(geometry, 1);
				break;
			case TWOPHASE:
				grid_adaptation->SetTwoPhase_Refinement(geometry, 1);
				break;
			case SUPERSONIC_SHOCK:
				grid_adaptation->SetSupShock_Refinement(geometry, config);
				break;
			case FULL_FLOW:
				grid_adaptation->SetComplete_Refinement(geometry, 1);
				break;
			case FULL_ADJOINT:
				grid_adaptation->GetAdjSolution(geometry, config);
				grid_adaptation->SetComplete_Refinement(geometry, 1);
				break;
			case FULL_LINEAR:
				grid_adaptation->GetLinSolution(geometry, config);
				grid_adaptation->SetComplete_Refinement(geometry, 1);
				break;
			case GRAD_FLOW:
				grid_adaptation->SetIndicator_Flow(geometry, config, 1);
				break;
			case GRAD_ADJOINT:
				grid_adaptation->GetAdjSolution(geometry, config);
				grid_adaptation->SetIndicator_Adj(geometry, config, 1);
				break;
			case GRAD_FLOW_ADJ:
				grid_adaptation->GetAdjSolution(geometry, config);
				grid_adaptation->SetIndicator_FlowAdj(geometry, config);
				break;
			case COMPUTABLE:
				grid_adaptation->GetAdjSolution(geometry, config);
				grid_adaptation->GetFlowResidual(geometry, config);
				grid_adaptation->SetIndicator_Computable(geometry, config);
				break;
			case REMAINING:
				cout << "Adaptation method not implemented."<< endl;
				cout << "Press any key to exit..." << endl;
				cin.get();
				exit(1);
				break;
			case ROBUST:
				grid_adaptation->GetFlowResidual(geometry, config);
				grid_adaptation->GetAdjResidual(geometry, config);
				grid_adaptation->SetIndicator_Robust(geometry, config);
				break;
			case COMPUTABLE_ROBUST:
				grid_adaptation->GetAdjSolution(geometry, config);
				grid_adaptation->GetLinResidual(geometry, config);
				grid_adaptation->SetIndicator_Computable_Robust(geometry, config);
				break;
			default :
				cout << "The adaptation is not defined" << endl;
		}
		
		/*--- Perform an homothetic adaptation of the grid ---*/
		CPhysicalGeometry *geo_adapt; geo_adapt = new CPhysicalGeometry;
		
		cout << "Homothetic grid adaptation" << endl;
		if (geometry->GetnDim() == 2) grid_adaptation->SetHomothetic_Adaptation2D(geometry, geo_adapt, config);
		if (geometry->GetnDim() == 3) grid_adaptation->SetHomothetic_Adaptation3D(geometry, geo_adapt, config);
    
		/*--- Smooth the numerical grid coordinates ---*/
		if (config->GetSmoothNumGrid()) {
			cout << "Preprocessing for doing the implicit smoothing." << endl;
			geo_adapt->SetEsuP(); geo_adapt->SetPsuP(); geo_adapt->SetEsuE();
			geo_adapt->SetBoundVolume(); geo_adapt->Check_Orientation(config);
			geo_adapt->SetEdges(); geo_adapt->SetVertex(config);
			cout << "Implicit smoothing of the numerical grid coordinates." << endl;
			geo_adapt->SetCoord_Smoothing(5, 1.5, config);
		}
		
		/*--- Original and adapted grid ---*/
    strcpy (file_name, "original_grid.plt");
    geometry->SetTecPlot(file_name);
    
		/*--- Write the adaptation sensor ---*/
		grid_adaptation->WriteAdaptSensor(geometry, file_name);
		
    strcpy (file_name, "adapted_grid.plt");
    geo_adapt->SetTecPlot(file_name);
    strcpy (file_name, "adapted_surface.plt");
    geo_adapt->SetBoundTecPlot(config,file_name);
		
		/*--- Write the new adapted grid, including the modified boundaries surfaces ---*/
		geo_adapt->SetMeshFile(config, config->GetMesh_Out_FileName());
    
    
		/*--- Write the restart file ---*/
		if ((config->GetKind_Adaptation() != SMOOTHING) && (config->GetKind_Adaptation() != FULL) &&
				(config->GetKind_Adaptation() != WAKE) && (config->GetKind_Adaptation() != TWOPHASE) &&
				(config->GetKind_Adaptation() != SUPERSONIC_SHOCK))
			grid_adaptation->SetRestart_FlowSolution(config, geo_adapt, config->GetRestart_FlowFileName());
		
		if ((config->GetKind_Adaptation() == GRAD_FLOW_ADJ) || (config->GetKind_Adaptation() == GRAD_ADJOINT)
				|| (config->GetKind_Adaptation() == FULL_ADJOINT) || (config->GetKind_Adaptation() == ROBUST)
				|| (config->GetKind_Adaptation() == COMPUTABLE) || (config->GetKind_Adaptation() == COMPUTABLE_ROBUST) ||
				(config->GetKind_Adaptation() == REMAINING))
			grid_adaptation->SetRestart_AdjSolution(config, geo_adapt, config->GetRestart_AdjFileName());
		
		if ((config->GetKind_Adaptation() == FULL_LINEAR) || (config->GetKind_Adaptation() == COMPUTABLE_ROBUST)) {
			grid_adaptation->SetRestart_LinSolution(config, geo_adapt, config->GetRestart_LinFileName());
		}
	}
	else {
    strcpy (file_name, "original_grid.plt");
    geometry->SetTecPlot(file_name);
		geometry->SetMeshFile (config, config->GetMesh_Out_FileName());
	}
  
#ifndef NO_MPI
#ifdef WINDOWS
	MPI_Finalize();
#else
	MPI::Finalize();
#endif
#endif
	
	/*--- End solver ---*/
	cout << endl <<"------------------------- Exit Success (SU2_MAC) ------------------------" << endl << endl;
  
	return EXIT_SUCCESS;
}
示例#2
0
文件: SU2_PBC.cpp 项目: ZJLi2013/SU2
int main(int argc, char *argv[]) {
	
	char buffer_vtk[100], buffer_plt[100]; 
	string MeshFile;
	unsigned short nZone = 1;
    
#ifndef NO_MPI
#ifdef WINDOWS
	MPI_Init(&argc,&argv);
#else
    MPI::Init(argc, argv);
#endif
#endif
  
	/*--- Definition of the class for the definition of the problem ---*/
	CConfig *config;
	if (argc == 2) config = new CConfig(argv[1], SU2_PBC, ZONE_0, nZone, 0, VERB_HIGH);
	else {
		char grid_file[200];
		strcpy (grid_file, "default.cfg");
		config = new CConfig(grid_file, SU2_PBC, ZONE_0, nZone, 0, VERB_HIGH);
	}

	/*--- Definition of the class for the geometry ---*/
	CGeometry *geometry; geometry = new CGeometry;
	geometry = new CPhysicalGeometry(config, ZONE_0, nZone);
  
  /*--- Perform the non-dimensionalization, in case any values are needed ---*/
  config->SetNondimensionalization(geometry->GetnDim(), ZONE_0);
  
	cout << endl <<"----------------------- Preprocessing computations ----------------------" << endl;
	
	/*--- Compute elements surrounding points, points surrounding points, and elements surrounding elements ---*/
	cout << "Setting local point and element connectivity." <<endl; 
	geometry->SetEsuP(); geometry->SetPsuP(); geometry->SetEsuE();
	
	/*--- Check the orientation before computing geometrical quantities ---*/
	cout << "Checking the numerical grid orientation." <<endl;
	geometry->SetBoundVolume(); geometry->Check_Orientation(config);
	
	/*--- Create the edge structure ---*/
	cout << "Identifying edges and vertices." <<endl; 
	geometry->SetEdges(); geometry->SetVertex(config); 
	
	/*--- Compute center of gravity ---*/
	cout << "Computing centers of gravity." << endl;
	geometry->SetCG();
  
	/*--- Create the control volume structures ---*/
	cout << "Setting the control volume structure." << endl; 
	geometry->SetControlVolume(config, ALLOCATE);
	geometry->SetBoundControlVolume(config, ALLOCATE);
	
	cout << endl <<"-------------------- Setting the periodic boundaries --------------------" << endl;

	/*--- Set periodic boundary conditions ---*/
	geometry->SetPeriodicBoundary(config);
	
  /*--- Original grid for debugging purposes ---*/
  strcpy (buffer_plt, "periodic_original.plt"); geometry->SetTecPlot(buffer_plt);
 
	/*--- Create a new grid with the right periodic boundary ---*/
	CGeometry *periodic; periodic = new CPeriodicGeometry(geometry, config);
	periodic->SetPeriodicBoundary(geometry, config);
	periodic->SetMeshFile(geometry, config, config->GetMesh_Out_FileName());
	
	/*--- Output of the grid for debuging purposes ---*/
  strcpy (buffer_plt, "periodic_halo.plt"); periodic->SetTecPlot(buffer_plt);
	
#ifndef NO_MPI
#ifdef WINDOWS
	MPI_Finalize();
#else
	MPI::Finalize();
#endif
#endif
    
	/*--- End solver ---*/
	cout << endl <<"------------------------- Exit Success (SU2_PBC) ------------------------" << endl << endl;
	
	return EXIT_SUCCESS;
}