/*---------------------------------------------------------------------------*\ ========= | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox \\ / O peration | \\ / A nd | www.openfoam.com \\/ M anipulation | ------------------------------------------------------------------------------- Copyright (C) 2011-2017 OpenFOAM Foundation ------------------------------------------------------------------------------- License This file is part of OpenFOAM. OpenFOAM is free software: you can redistribute it and/or modify it under the terms of the GNU General Public License as published by the Free Software Foundation, either version 3 of the License, or (at your option) any later version. OpenFOAM is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License for more details. You should have received a copy of the GNU General Public License along with OpenFOAM. If not, see . Application boundaryFoam Group grpIncompressibleSolvers Description Steady-state solver for incompressible, 1D turbulent flow, typically to generate boundary layer conditions at an inlet. Boundary layer code to calculate the U, k and epsilon distributions. Used to create inlet boundary conditions for experimental comparisons for which U and k have not been measured. Turbulence model is runtime selectable. \*---------------------------------------------------------------------------*/ #include "fvCFD.H" #include "singlePhaseTransportModel.H" #include "turbulentTransportModel.H" #include "fvOptions.H" #include "wallFvPatch.H" #include "makeGraph.H" // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // int main(int argc, char *argv[]) { argList::addNote ( "Steady-state solver for incompressible, 1D turbulent flow," " typically to generate boundary layer conditions at an inlet." ); argList::noParallel(); #include "addCheckCaseOptions.H" #include "setRootCaseLists.H" #include "createTime.H" #include "createMesh.H" #include "createFields.H" #include "interrogateWallPatches.H" turbulence->validate(); // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // Info<< "\nStarting time loop\n" << endl; while (runTime.loop()) { Info<< "Time = " << runTime.timeName() << nl << endl; fvVectorMatrix divR(turbulence->divDevReff(U)); divR.source() = flowMask & divR.source(); fvVectorMatrix UEqn ( divR == gradP + fvOptions(U) ); UEqn.relax(); fvOptions.constrain(UEqn); UEqn.solve(); fvOptions.correct(U); // Correct driving force for a constant volume flow rate dimensionedVector UbarStar = flowMask & U.weightedAverage(mesh.V()); U += (Ubar - UbarStar); gradP += (Ubar - UbarStar)/(1.0/UEqn.A())().weightedAverage(mesh.V()); laminarTransport.correct(); turbulence->correct(); Info<< "Uncorrected Ubar = " << (flowDirection & UbarStar.value()) << ", pressure gradient = " << (flowDirection & gradP.value()) << endl; #include "evaluateNearWall.H" if (runTime.writeTime()) { #include "makeGraphs.H" } runTime.printExecutionTime(Info); } Info<< "End\n" << endl; return 0; } // ************************************************************************* //