本文整理汇总了C++中CGeometry::Compute_Volume方法的典型用法代码示例。如果您正苦于以下问题：C++ CGeometry::Compute_Volume方法的具体用法？C++ CGeometry::Compute_Volume怎么用？C++ CGeometry::Compute_Volume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::Compute_Volume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.........
/*--- 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);
}
/*--- Compute the internal volume of a 3D body. ---*/
if (rank == MASTER_NODE) cout << "Computing the internal volume." << endl;
if (boundary->GetnDim() == 3) Volume = boundary->Compute_Volume(config, true);
if (rank == MASTER_NODE)
cout << endl <<"-------------------- Objective function evaluation ----------------------" << endl;
if (rank == MASTER_NODE) {
/*--- Evaluate objective function ---*/
for (iPlane = 0; iPlane < nPlane; iPlane++) {
if (Xcoord_Airfoil[iPlane].size() != 0) {
cout << "\nSection " << (iPlane+1) << ". Plane (yCoord): " << Plane_P0[iPlane][1] << "." << endl;
ObjectiveFunc[iPlane] = boundary->Compute_MaxThickness(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], true);
ObjectiveFunc[1*nPlane+iPlane] = boundary->Compute_Thickness(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, 0.250000, config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], true);
ObjectiveFunc[2*nPlane+iPlane] = boundary->Compute_Thickness(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, 0.333333, config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], true);
ObjectiveFunc[3*nPlane+iPlane] = boundary->Compute_Thickness(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, 0.500000, config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], true);
ObjectiveFunc[4*nPlane+iPlane] = boundary->Compute_Thickness(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, 0.666666, config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], true);
ObjectiveFunc[5*nPlane+iPlane] = boundary->Compute_Thickness(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, 0.750000, config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], true);
ObjectiveFunc[6*nPlane+iPlane] = boundary->Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, config, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], true);
ObjectiveFunc[7*nPlane+iPlane] = boundary->Compute_AoA(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], true);
ObjectiveFunc[8*nPlane+iPlane] = boundary->Compute_Chord(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], true);
cout << "Maximum thickness: " << ObjectiveFunc[iPlane] << "." << endl;
cout << "1/4 chord thickness: " << ObjectiveFunc[1*nPlane+iPlane] << "." << endl;
cout << "1/3 chord thickness: " << ObjectiveFunc[2*nPlane+iPlane] << "." << endl;
cout << "1/2 chord thickness: " << ObjectiveFunc[3*nPlane+iPlane] << "." << endl;
cout << "2/3 chord thickness: " << ObjectiveFunc[4*nPlane+iPlane] << "." << endl;
cout << "3/4 chord thickness: " << ObjectiveFunc[5*nPlane+iPlane] << "." << endl;
cout << "Area: " << ObjectiveFunc[6*nPlane+iPlane] << "." << endl;
cout << "Angle of attack: " << ObjectiveFunc[7*nPlane+iPlane] << "." << endl;
cout << "Chord: " << ObjectiveFunc[8*nPlane+iPlane] << "." << endl;