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foam-extend4.1-coherent-io/applications/solvers/incompressible/boundaryFoam/boundaryFoam.C

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/*---------------------------------------------------------------------------*\
========= |
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\\ / F ield | foam-extend: Open Source CFD
\\ / O peration | Version: 3.2
\\ / A nd | Web: http://www.foam-extend.org
\\/ M anipulation | For copyright notice see file Copyright
-------------------------------------------------------------------------------
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
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
option) any later version.
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foam-extend 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
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along with foam-extend. If not, see <http://www.gnu.org/licenses/>.
Application
boundaryFoam
Description
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Steady-state solver for 1D turbulent flow, typically to generate boundary
layer conditions at an inlet, for use in a simulation.
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"
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#include "singlePhaseTransportModel.H"
#include "RASModel.H"
#include "wallFvPatch.H"
#include "makeGraph.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
# include "setRootCase.H"
# include "createTime.H"
# include "createMesh.H"
# include "createFields.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
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while (runTime.loop())
{
Info<< "Time = " << runTime.timeName() << nl << endl;
fvVectorMatrix divR = turbulence->divDevReff();
divR.source() = flowMask & divR.source();
fvVectorMatrix UEqn
(
divR == gradP
);
UEqn.relax();
UEqn.solve();
// Correct driving force for a constant mass flow rate
dimensionedVector UbarStar = flowMask & U.weightedAverage(mesh.V());
U += (Ubar - UbarStar);
gradP += (Ubar - UbarStar)/(1.0/UEqn.A())().weightedAverage(mesh.V());
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label id = y.size() - 1;
scalar wallShearStress =
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flowDirection & turbulence->R()()[id] & wallNormal;
scalar yplusWall
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// = Foam::sqrt(mag(wallShearStress))*y[id]/laminarTransport.nu()()[id];
= Foam::sqrt(mag(wallShearStress))*y[id]/turbulence->nuEff()()[id];
Info<< "Uncorrected Ubar = " << (flowDirection & UbarStar.value())<< tab
<< "pressure gradient = " << (flowDirection & gradP.value()) << tab
<< "min y+ = " << yplusWall << endl;
turbulence->correct();
if (runTime.outputTime())
{
volSymmTensorField R
(
IOobject
(
"R",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::AUTO_WRITE
),
turbulence->R()
);
runTime.write();
const word& gFormat = runTime.graphFormat();
makeGraph(y, flowDirection & U, "Uf", gFormat);
makeGraph(y, laminarTransport.nu(), gFormat);
makeGraph(y, turbulence->k(), gFormat);
makeGraph(y, turbulence->epsilon(), gFormat);
//makeGraph(y, flowDirection & R & flowDirection, "Rff", gFormat);
//makeGraph(y, wallNormal & R & wallNormal, "Rww", gFormat);
//makeGraph(y, flowDirection & R & wallNormal, "Rfw", gFormat);
//makeGraph(y, sqrt(R.component(tensor::XX)), "u", gFormat);
//makeGraph(y, sqrt(R.component(tensor::YY)), "v", gFormat);
//makeGraph(y, sqrt(R.component(tensor::ZZ)), "w", gFormat);
makeGraph(y, R.component(tensor::XY), "uv", gFormat);
makeGraph(y, mag(fvc::grad(U)), "gammaDot", gFormat);
}
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< nl << endl;
}
Info<< "End\n" << endl;
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return 0;
}
// ************************************************************************* //