118 lines
3.5 KiB
C++
118 lines
3.5 KiB
C++
/*---------------------------------------------------------------------------*\
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========= |
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\\ / F ield | foam-extend: Open Source CFD
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\\ / O peration | Version: 4.0
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\\ / A nd | Web: http://www.foam-extend.org
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\\/ M anipulation | For copyright notice see file Copyright
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-------------------------------------------------------------------------------
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License
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This file is part of foam-extend.
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foam-extend is free software: you can redistribute it and/or modify it
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under the terms of the GNU General Public License as published by the
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Free Software Foundation, either version 3 of the License, or (at your
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option) any later version.
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foam-extend is distributed in the hope that it will be useful, but
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WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU
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General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with foam-extend. If not, see <http://www.gnu.org/licenses/>.
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Application
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boundaryFoam
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Description
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Steady-state solver for 1D turbulent flow, typically to generate boundary
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layer conditions at an inlet, for use in a simulation.
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Boundary layer code to calculate the U, k and epsilon distributions.
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Used to create inlet boundary conditions for experimental comparisons
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for which U and k have not been measured.
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Turbulence model is runtime selectable.
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\*---------------------------------------------------------------------------*/
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#include "fvCFD.H"
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#include "singlePhaseTransportModel.H"
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#include "RASModel.H"
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#include "wallFvPatch.H"
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#include "makeGraph.H"
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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int main(int argc, char *argv[])
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{
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# include "setRootCase.H"
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# include "createTime.H"
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# include "createMesh.H"
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# include "createFields.H"
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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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Info<< "\nStarting time loop\n" << endl;
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while (runTime.loop())
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{
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Info<< "Time = " << runTime.timeName() << nl << endl;
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fvVectorMatrix divR = turbulence->divDevReff();
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divR.source() = flowMask & divR.source();
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fvVectorMatrix UEqn
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(
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divR == gradP
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);
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UEqn.relax();
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UEqn.solve();
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// Correct driving force for a constant mass flow rate
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dimensionedVector UbarStar = flowMask & U.weightedAverage(mesh.V());
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U += (Ubar - UbarStar);
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gradP += (Ubar - UbarStar)/(1.0/UEqn.A())().weightedAverage(mesh.V());
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Info<< "Uncorrected Ubar = " << (flowDirection & UbarStar.value())<< tab
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<< "pressure gradient = " << (flowDirection & gradP.value())
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<< endl;
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turbulence->correct();
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if (runTime.outputTime())
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{
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volSymmTensorField R
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(
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IOobject
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(
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"R",
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runTime.timeName(),
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mesh,
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IOobject::NO_READ,
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IOobject::AUTO_WRITE
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),
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turbulence->R()
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);
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runTime.write();
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}
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Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
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<< " ClockTime = " << runTime.elapsedClockTime() << " s"
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<< nl << endl;
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}
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Info<< "End\n" << endl;
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return 0;
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}
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// ************************************************************************* //
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