本文整理汇总了C++中CGeometry::ComputeSurf_Curvature方法的典型用法代码示例。如果您正苦于以下问题：C++ CGeometry::ComputeSurf_Curvature方法的具体用法？C++ CGeometry::ComputeSurf_Curvature怎么用？C++ CGeometry::ComputeSurf_Curvature使用的例子？那么, 这里精选的方法代码示例或许可以为您提供帮助。您也可以进一步了解该方法所在类CGeometry的用法示例。
在下文中一共展示了CGeometry::ComputeSurf_Curvature方法的1个代码示例，这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞，您的评价将有助于系统推荐出更棒的C++代码示例。
示例1: main
//.........这里部分代码省略.........
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->SetPoint_Connectivity();
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 ---*/
if (rank == MASTER_NODE) cout << "Compute the surface curvature." << endl;
boundary->ComputeSurf_Curvature(config);
if (rank == MASTER_NODE) cout << "Writing a Tecplot file of the surface curvature." << endl;
if (size > 1) sprintf (buffer_char, "_%d.plt", rank+1); else sprintf (buffer_char, ".plt");
strcpy (out_file, "Surface_Curvature"); strcat(out_file, buffer_char); boundary->SetBoundTecPlot(out_file, true, config);
/*--- Create plane structure ---*/
if (rank == MASTER_NODE) cout << "Set plane structure." << endl;
if (boundary->GetnDim() == 2) {
MinXCoord = -1E6; MaxXCoord = 1E6;
Plane_Normal[0][0] = 0.0; Plane_P0[0][0] = 0.0;
Plane_Normal[0][1] = 1.0; Plane_P0[0][1] = 0.0;
Plane_Normal[0][2] = 0.0; Plane_P0[0][2] = 0.0;
}
else if (boundary->GetnDim() == 3) {
MinPlane = config->GetSection_Location(0); MaxPlane = config->GetSection_Location(1);
MinXCoord = -1E6; MaxXCoord = 1E6;
for (iPlane = 0; iPlane < nPlane; iPlane++) {
Plane_Normal[iPlane][0] = 0.0; Plane_P0[iPlane][0] = 0.0;
Plane_Normal[iPlane][1] = 0.0; Plane_P0[iPlane][1] = 0.0;
Plane_Normal[iPlane][2] = 0.0; Plane_P0[iPlane][2] = 0.0;
Plane_Normal[iPlane][config->GetAxis_Orientation()] = 1.0;
Plane_P0[iPlane][config->GetAxis_Orientation()] = MinPlane + iPlane*(MaxPlane - MinPlane)/double(nPlane-1);
}
}
/*--- Create airfoil section structure ---*/
if (rank == MASTER_NODE) cout << "Set airfoil section structure." << endl;
for (iPlane = 0; iPlane < nPlane; iPlane++) {
boundary->ComputeAirfoil_Section(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, MinXCoord, MaxXCoord, NULL,
Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], Variable_Airfoil[iPlane], true, config);