149 lines
4.7 KiB
C
149 lines
4.7 KiB
C
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/*---------------------------------------------------------------------------*\
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========= |
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\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
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\\ / O peration |
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\\ / A nd | Copyright held by original author
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\\/ M anipulation |
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-------------------------------------------------------------------------------
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License
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This file is part of OpenFOAM.
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OpenFOAM 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 2 of the License, or (at your
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option) any later version.
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OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
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ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
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FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
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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 OpenFOAM; if not, write to the Free Software Foundation,
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Inc., 51 Franklin St, Fifth Floor, Boston, MA 02110-1301 USA
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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 "incompressible/singlePhaseTransportModel/singlePhaseTransportModel.H"
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#include "incompressible/RASModel/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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for (runTime++; !runTime.end(); runTime++)
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{
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Info<< "Time = " << runTime.timeName() << nl << endl;
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fvVectorMatrix divR = turbulence->divDevReff(U);
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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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scalar wallShearStress =
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flowDirection & turbulence->R()()[0] & wallNormal;
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scalar yplusWall
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= Foam::sqrt(mag(wallShearStress))*y[0]/laminarTransport.nu()[0];
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Info<< "Uncorrected Ubar = " << (flowDirection & UbarStar.value())<< tab
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<< "pressure gradient = " << (flowDirection & gradP.value()) << tab
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<< "min y+ = " << yplusWall << 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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const word& gFormat = runTime.graphFormat();
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makeGraph(y, flowDirection & U, "Uf", gFormat);
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makeGraph(y, laminarTransport.nu(), gFormat);
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makeGraph(y, turbulence->k(), gFormat);
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makeGraph(y, turbulence->epsilon(), gFormat);
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//makeGraph(y, flowDirection & R & flowDirection, "Rff", gFormat);
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//makeGraph(y, wallNormal & R & wallNormal, "Rww", gFormat);
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//makeGraph(y, flowDirection & R & wallNormal, "Rfw", gFormat);
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//makeGraph(y, sqrt(R.component(tensor::XX)), "u", gFormat);
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//makeGraph(y, sqrt(R.component(tensor::YY)), "v", gFormat);
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//makeGraph(y, sqrt(R.component(tensor::ZZ)), "w", gFormat);
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makeGraph(y, R.component(tensor::XY), "uv", gFormat);
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makeGraph(y, mag(fvc::grad(U)), "gammaDot", gFormat);
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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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