本文整理汇总了C++中COutput::SetResult_Files方法的典型用法代码示例。如果您正苦于以下问题：C++ COutput::SetResult_Files方法的具体用法？C++ COutput::SetResult_Files怎么用？C++ COutput::SetResult_Files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COutput的用法示例。
在下文中一共展示了COutput::SetResult_Files方法的3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.........
case ADJ_EULER: case ADJ_NAVIER_STOKES: case ADJ_RANS:
StopCalc = integration_container[ZONE_0][ADJFLOW_SOL]->GetConvergence(); break;
case ADJ_TNE2_EULER: case ADJ_TNE2_NAVIER_STOKES:
StopCalc = integration_container[ZONE_0][ADJTNE2_SOL]->GetConvergence(); break;
}
/*--- Solution output. Determine whether a solution needs to be written
after the current iteration, and if so, execute the output file writing
routines. ---*/
if ((ExtIter+1 == config_container[ZONE_0]->GetnExtIter()) ||
((ExtIter % config_container[ZONE_0]->GetWrt_Sol_Freq() == 0) && (ExtIter != 0) &&
!((config_container[ZONE_0]->GetUnsteady_Simulation() == DT_STEPPING_1ST) ||
(config_container[ZONE_0]->GetUnsteady_Simulation() == DT_STEPPING_2ND))) ||
(StopCalc) ||
(((config_container[ZONE_0]->GetUnsteady_Simulation() == DT_STEPPING_1ST) ||
(config_container[ZONE_0]->GetUnsteady_Simulation() == DT_STEPPING_2ND)) &&
((ExtIter == 0) || (ExtIter % config_container[ZONE_0]->GetWrt_Sol_Freq_DualTime() == 0)))) {
/*--- Low-fidelity simulations (using a coarser multigrid level
approximation to the solution) require an interpolation back to the
finest grid. ---*/
if (config_container[ZONE_0]->GetLowFidelitySim()) {
integration_container[ZONE_0][FLOW_SOL]->SetProlongated_Solution(RUNTIME_FLOW_SYS, solver_container[ZONE_0][MESH_0], solver_container[ZONE_0][MESH_1], geometry_container[ZONE_0][MESH_0], geometry_container[ZONE_0][MESH_1], config_container[ZONE_0]);
integration_container[ZONE_0][FLOW_SOL]->Smooth_Solution(RUNTIME_FLOW_SYS, solver_container[ZONE_0][MESH_0], geometry_container[ZONE_0][MESH_0], 3, 1.25, config_container[ZONE_0]);
solver_container[ZONE_0][MESH_0][config_container[ZONE_0]->GetContainerPosition(RUNTIME_FLOW_SYS)]->Set_MPI_Solution(geometry_container[ZONE_0][MESH_0], config_container[ZONE_0]);
solver_container[ZONE_0][MESH_0][config_container[ZONE_0]->GetContainerPosition(RUNTIME_FLOW_SYS)]->Preprocessing(geometry_container[ZONE_0][MESH_0], solver_container[ZONE_0][MESH_0], config_container[ZONE_0], MESH_0, 0, RUNTIME_FLOW_SYS);
}
/*--- Execute the routine for writing restart, volume solution,
surface solution, and surface comma-separated value files. ---*/
output->SetResult_Files(solver_container, geometry_container, config_container, ExtIter, nZone);
}
/*--- If the convergence criteria has been met, terminate the simulation. ---*/
if (StopCalc) break;
ExtIter++;
}
/*--- Close the convergence history file. ---*/
if (rank == MASTER_NODE) {
ConvHist_file.close();
cout << endl <<"History file, closed." << endl;
}
/*
if (config->GetKind_Solver() == RANS){
if (config->GetKind_Turb_Model() == ML){
// Tell the ML code to stop running
string mlWriteFilename = config->GetML_Turb_Model_Write();
ofstream mlWrite;
mlWrite.open(mlWriteFilename.c_str());
mlWrite << int(-1) << flush;
mlWrite.close();
}
}
*/
/*--- Solver class deallocation ---*/
// for (iZone = 0; iZone < nZone; iZone++) {示例2: main
//.........这里部分代码省略.........
((config_container[ZONE_0]->GetUnsteady_Simulation() == DT_STEPPING_2ND) && (!fsi) &&
((ExtIter == 0) || ((ExtIter % config_container[ZONE_0]->GetWrt_Sol_Freq_DualTime() == 0) ||
((ExtIter-1) % config_container[ZONE_0]->GetWrt_Sol_Freq_DualTime() == 0))))
||
((config_container[ZONE_0]->GetUnsteady_Simulation() == DT_STEPPING_2ND) && (fsi) &&
((ExtIter == 0) || ((ExtIter % config_container[ZONE_0]->GetWrt_Sol_Freq_DualTime() == 0))))
||
(((config_container[ZONE_0]->GetDynamic_Analysis() == DYNAMIC) &&
((ExtIter == 0) || (ExtIter % config_container[ZONE_0]->GetWrt_Sol_Freq_DualTime() == 0))))){
/*--- Low-fidelity simulations (using a coarser multigrid level
approximation to the solution) require an interpolation back to the
finest grid. ---*/
if (config_container[ZONE_0]->GetLowFidelitySim()) {
integration_container[ZONE_0][FLOW_SOL]->SetProlongated_Solution(RUNTIME_FLOW_SYS, solver_container[ZONE_0][MESH_0][FLOW_SOL], solver_container[ZONE_0][MESH_1][FLOW_SOL], geometry_container[ZONE_0][MESH_0], geometry_container[ZONE_0][MESH_1], config_container[ZONE_0]);
integration_container[ZONE_0][FLOW_SOL]->Smooth_Solution(RUNTIME_FLOW_SYS, solver_container[ZONE_0][MESH_0][FLOW_SOL], geometry_container[ZONE_0][MESH_0], 3, 1.25, config_container[ZONE_0]);
solver_container[ZONE_0][MESH_0][config_container[ZONE_0]->GetContainerPosition(RUNTIME_FLOW_SYS)]->Set_MPI_Solution(geometry_container[ZONE_0][MESH_0], config_container[ZONE_0]);
solver_container[ZONE_0][MESH_0][config_container[ZONE_0]->GetContainerPosition(RUNTIME_FLOW_SYS)]->Preprocessing(geometry_container[ZONE_0][MESH_0], solver_container[ZONE_0][MESH_0], config_container[ZONE_0], MESH_0, 0, RUNTIME_FLOW_SYS, true);
}
if (rank == MASTER_NODE) cout << endl << "-------------------------- File Output Summary --------------------------";
/*--- Execute the routine for writing restart, volume solution,
surface solution, and surface comma-separated value files. ---*/
output->SetResult_Files(solver_container, geometry_container, config_container, ExtIter, nZone);
/*--- Output a file with the forces breakdown. ---*/
output->SetForces_Breakdown(geometry_container, solver_container,
config_container, integration_container, ZONE_0);
/*--- Compute the forces at different sections. ---*/
if (config_container[ZONE_0]->GetPlot_Section_Forces()) {
output->SetForceSections(solver_container[ZONE_0][MESH_0][FLOW_SOL],
geometry_container[ZONE_0][MESH_0], config_container[ZONE_0], ExtIter);
}
if (rank == MASTER_NODE) cout << "-------------------------------------------------------------------------" << endl << endl;
}
/*--- If the convergence criteria has been met, terminate the simulation. ---*/
if (StopCalc) break;
ExtIter++;
}
/*--- Output some information to the console. ---*/
if (rank == MASTER_NODE) {
/*--- Print out the number of non-physical points and reconstructions ---*/
if (config_container[ZONE_0]->GetNonphysical_Points() > 0)示例3: main
//.........这里部分代码省略.........
case ADJ_TNE2_EULER: case ADJ_TNE2_NAVIER_STOKES:
StopCalc = integration_container[ZONE_0][ADJTNE2_SOL]->GetConvergence(); break;
}
/*--- Solution output. Determine whether a solution needs to be written
after the current iteration, and if so, execute the output file writing
routines. ---*/
if ((ExtIter+1 >= config_container[ZONE_0]->GetnExtIter()) ||
((ExtIter % config_container[ZONE_0]->GetWrt_Sol_Freq() == 0) && (ExtIter != 0) &&
!((config_container[ZONE_0]->GetUnsteady_Simulation() == DT_STEPPING_1ST) ||
(config_container[ZONE_0]->GetUnsteady_Simulation() == DT_STEPPING_2ND))) ||
(StopCalc) ||
(((config_container[ZONE_0]->GetUnsteady_Simulation() == DT_STEPPING_1ST) ||
(config_container[ZONE_0]->GetUnsteady_Simulation() == DT_STEPPING_2ND)) &&
((ExtIter == 0) || (ExtIter % config_container[ZONE_0]->GetWrt_Sol_Freq_DualTime() == 0)))) {
/*--- Low-fidelity simulations (using a coarser multigrid level
approximation to the solution) require an interpolation back to the
finest grid. ---*/
if (config_container[ZONE_0]->GetLowFidelitySim()) {
integration_container[ZONE_0][FLOW_SOL]->SetProlongated_Solution(RUNTIME_FLOW_SYS, solver_container[ZONE_0][MESH_0][FLOW_SOL], solver_container[ZONE_0][MESH_1][FLOW_SOL], geometry_container[ZONE_0][MESH_0], geometry_container[ZONE_0][MESH_1], config_container[ZONE_0]);
integration_container[ZONE_0][FLOW_SOL]->Smooth_Solution(RUNTIME_FLOW_SYS, solver_container[ZONE_0][MESH_0][FLOW_SOL], geometry_container[ZONE_0][MESH_0], 3, 1.25, config_container[ZONE_0]);
solver_container[ZONE_0][MESH_0][config_container[ZONE_0]->GetContainerPosition(RUNTIME_FLOW_SYS)]->Set_MPI_Solution(geometry_container[ZONE_0][MESH_0], config_container[ZONE_0]);
solver_container[ZONE_0][MESH_0][config_container[ZONE_0]->GetContainerPosition(RUNTIME_FLOW_SYS)]->Preprocessing(geometry_container[ZONE_0][MESH_0], solver_container[ZONE_0][MESH_0], config_container[ZONE_0], MESH_0, 0, RUNTIME_FLOW_SYS, false);
}
if (rank == MASTER_NODE) cout << endl << "-------------------------- File Output Summary --------------------------";
/*--- Execute the routine for writing restart, volume solution,
surface solution, and surface comma-separated value files. ---*/
output->SetResult_Files(solver_container, geometry_container, config_container, ExtIter, nZone);
/*--- Output a file with the forces breakdown. ---*/
output->SetForces_Breakdown(geometry_container, solver_container,
config_container, integration_container, ZONE_0);
/*--- Compute the forces at different sections. ---*/
if (config_container[ZONE_0]->GetPlot_Section_Forces()) {
output->SetForceSections(solver_container[ZONE_0][MESH_0][FLOW_SOL],
geometry_container[ZONE_0][MESH_0], config_container[ZONE_0], ExtIter);
}
if (rank == MASTER_NODE) cout << "-------------------------------------------------------------------------" << endl << endl;
}
/*--- If the convergence criteria has been met, terminate the simulation. ---*/
if (StopCalc) break;
ExtIter++;
}
/*--- Output some information to the console. ---*/
if (rank == MASTER_NODE) {
/*--- Print out the number of non-physical points and reconstructions ---*/
if (config_container[ZONE_0]->GetNonphysical_Points() > 0)