C++ CGeometry::SetPsuP方法代码示例

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;
}

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:
//.........这里部分代码省略.........

int main(int argc, char *argv[]) {
  
  /*--- Local variables ---*/
  
	unsigned short iDV, nZone = 1, iFFDBox, iPlane, nPlane, iVar;
	double *ObjectiveFunc, *ObjectiveFunc_New, *Gradient, delta_eps, MinPlane, MaxPlane, MinXCoord, MaxXCoord,
  **Plane_P0, **Plane_Normal, Volume, Volume_New, Volume_Grad;
  vector<double> *Xcoord_Airfoil, *Ycoord_Airfoil, *Zcoord_Airfoil, *Variable_Airfoil;
  char grid_file[200], buffer_char[50], out_file[200];

 	char *cstr;
	ofstream Gradient_file, ObjFunc_file;
	int rank = MASTER_NODE;
  int size = SINGLE_NODE;
  
  /*--- MPI initialization ---*/

#ifndef NO_MPI
	MPI_Init(&argc,&argv);
	MPI_Comm_rank(MPI_COMM_WORLD,&rank);
  MPI_Comm_size(MPI_COMM_WORLD,&size);
#endif
	
	/*--- Pointer to different structures that will be used throughout the entire code ---*/
  
	CFreeFormDefBox** FFDBox = NULL;
	CConfig *config = NULL;
	CGeometry *boundary = NULL;
	CSurfaceMovement *surface_mov = NULL;
	
	/*--- Definition of the class for the definition of the problem ---*/
  
	if (argc == 2) config = new CConfig(argv[1], SU2_GDC, ZONE_0, nZone, 0, VERB_HIGH);
	else {
		strcpy (grid_file, "default.cfg");
		config = new CConfig(grid_file, SU2_GDC, ZONE_0, nZone, 0, VERB_HIGH);
	}
	
  /*--- Change the name of the input-output files for the parallel computation ---*/
  
#ifndef NO_MPI
	config->SetFileNameDomain(rank+1);
#endif
	
	/*--- Definition of the class for the boundary of the geometry ---*/
  
	boundary = new CBoundaryGeometry(config, config->GetMesh_FileName(), config->GetMesh_FileFormat());
  
  /*--- Set the number of sections, and allocate the memory ---*/
  
  if (boundary->GetnDim() == 2) nPlane = 1;
  else nPlane = config->GetnSections();

  Xcoord_Airfoil = new vector<double>[nPlane];
  Ycoord_Airfoil = new vector<double>[nPlane];
  Zcoord_Airfoil = new vector<double>[nPlane];
  Variable_Airfoil = new vector<double>[nPlane];

  Plane_P0 = new double*[nPlane];
  Plane_Normal = new double*[nPlane];
  for(iPlane = 0; iPlane < nPlane; iPlane++ ) {
    Plane_P0[iPlane] = new double[3];
    Plane_Normal[iPlane] = new double[3];
  }
  
  ObjectiveFunc = new double[nPlane*20];
  ObjectiveFunc_New = new double[nPlane*20];
  Gradient = new double[nPlane*20];

  for (iVar = 0; iVar < nPlane*20; iVar++) {
    ObjectiveFunc[iVar] = 0.0;
    ObjectiveFunc_New[iVar] = 0.0;
    Gradient[iVar] = 0.0;
  }
  
  /*--- Evaluation of the objective function ---*/
  
	if (rank == MASTER_NODE)
		cout << endl <<"----------------------- Preprocessing computations ----------------------" << endl;

  
  /*--- Boundary geometry preprocessing ---*/
  
	if (rank == MASTER_NODE) cout << "Identify vertices." <<endl;
	boundary->SetVertex();
  
  /*--- Compute elements surrounding points & points surrounding points ---*/
  
  if (rank == MASTER_NODE) cout << "Setting local point and element connectivity." << endl;
  boundary->SetEsuP();
	boundary->SetPsuP();
  boundary->SetEdges();

	/*--- Create the control volume structures ---*/
  
	if (rank == MASTER_NODE) cout << "Set boundary control volume structure." << endl;
	boundary->SetBoundControlVolume(config, ALLOCATE);
	
  /*--- Compute the surface curvature ---*/
  
//.........这里部分代码省略.........