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C++ CConfig::GetObjFunc_Value_FileName方法代码示例

本文整理汇总了C++中CConfig::GetObjFunc_Value_FileName方法的典型用法代码示例。如果您正苦于以下问题：C++ CConfig::GetObjFunc_Value_FileName方法的具体用法？C++ CConfig::GetObjFunc_Value_FileName怎么用？C++ CConfig::GetObjFunc_Value_FileName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CConfig的用法示例。


在下文中一共展示了CConfig::GetObjFunc_Value_FileName方法的2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.........
        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;
        
      }
      
    }
    
    /*--- The value for Volume to the area of the first section
     in case this is a 2D calculation ---*/
    
    if (boundary->GetnDim() == 2) Volume = ObjectiveFunc[6];
    cout << "\nInternal volume: " << Volume << "." << endl;
    
    /*--- Write the objective function in a external file ---*/
		cstr = new char [config->GetObjFunc_Value_FileName().size()+1];
		strcpy (cstr, config->GetObjFunc_Value_FileName().c_str());
		ObjFunc_file.open(cstr, ios::out);
    ObjFunc_file << "TITLE = \"SU2_GEO Simulation\"" << endl;
    
    if (boundary->GetnDim() == 2) {
      ObjFunc_file << "VARIABLES = \"MAX_THICKNESS\",\"1/4_THICKNESS\",\"1/3_THICKNESS\",\"1/2_THICKNESS\",\"2/3_THICKNESS\",\"3/4_THICKNESS\",\"AREA\",\"AOA\",\"CHORD\",\"VOLUME\"" << endl;
    }
    else if (boundary->GetnDim() == 3) {
      ObjFunc_file << "VARIABLES = ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"MAX_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"1/4_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"1/3_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"1/2_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"2/3_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"3/4_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"AREA_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"AOA_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"CHORD_SEC"<< (iPlane+1) << "\", ";
      ObjFunc_file << "\"VOLUME\"" << endl;
    }
    
    ObjFunc_file << "ZONE T= \"Geometrical variables (value)\"" << endl;
    
    for (iPlane = 0; iPlane < nPlane*9; iPlane++)
      ObjFunc_file << ObjectiveFunc[iPlane] <<", ";
    ObjFunc_file << Volume << endl;

    ObjFunc_file.close();
    
	}
	
	if (config->GetGeometryMode() == GRADIENT) {
开发者ID:DulcetMech，项目名称:SU2，代码行数:67，代码来源:SU2_GEO.cpp

示例2: main


//.........这里部分代码省略.........
    
    /*--- 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, 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, 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, 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, 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, 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, Xcoord_Airfoil[iPlane], Ycoord_Airfoil[iPlane], Zcoord_Airfoil[iPlane], true);
        ObjectiveFunc[6*nPlane+iPlane]  = boundary->Compute_Area(Plane_P0[iPlane], Plane_Normal[iPlane], iPlane, 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;
        
      }
      
    }
    
    /*--- Write the objective function in a external file ---*/
		cstr = new char [config->GetObjFunc_Value_FileName().size()+1];
		strcpy (cstr, config->GetObjFunc_Value_FileName().c_str());
		ObjFunc_file.open(cstr, ios::out);
    ObjFunc_file << "TITLE = \"SU2_GDC Simulation\"" << endl;
    
    if (boundary->GetnDim() == 2) {
      ObjFunc_file << "VARIABLES = \"MAX_THICKNESS\",\"1/4_THICKNESS\",\"1/3_THICKNESS\",\"1/2_THICKNESS\",\"2/3_THICKNESS\",\"3/4_THICKNESS\",\"AREA\",\"AOA\",\"CHORD\"" << endl;
    }
    else if (boundary->GetnDim() == 3) {
      ObjFunc_file << "VARIABLES = ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"MAX_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"1/4_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"1/3_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"1/2_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"2/3_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"3/4_THICKNESS_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"AREA_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane; iPlane++) ObjFunc_file << "\"AOA_SEC"<< (iPlane+1) << "\", ";
      for (iPlane = 0; iPlane < nPlane-1; iPlane++) ObjFunc_file << "\"CHORD_SEC"<< (iPlane+1) << "\", ";
      ObjFunc_file << "\"CHORD_SEC"<< (nPlane) << "\"" << endl;
    }
    
    ObjFunc_file << "ZONE T= \"Geometrical variables (value)\"" << endl;
    
    for (iPlane = 0; iPlane < nPlane*9-1; iPlane++)
      ObjFunc_file << ObjectiveFunc[iPlane] <<", ";
    ObjFunc_file << ObjectiveFunc[nPlane*9-1] << endl;
    
    ObjFunc_file.close();
    
	}
	
	if (config->GetGeometryMode() == GRADIENT) {
开发者ID:dengxbskla，项目名称:SU2，代码行数:67，代码来源:SU2_GDC.cpp


注：本文中的CConfig::GetObjFunc_Value_FileName方法示例由纯净天空整理自Github/MSDocs等开源代码及文档管理平台，相关代码片段筛选自各路编程大神贡献的开源项目，源码版权归原作者所有，传播和使用请参考对应项目的License；未经允许，请勿转载。