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foam-extend4.1-coherent-io/applications/solvers/incompressible/boundaryFoam/boundaryFoam.C
2010-08-26 15:22:03 +01:00

150 lines
4.7 KiB
C

/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright held by original author
\\/ M anipulation |
-------------------------------------------------------------------------------
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 2 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, write to the Free Software Foundation,
Inc., 51 Franklin St, Fifth Floor, Boston, MA 02110-1301 USA
Application
boundaryFoam
Description
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"
#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;
while (runTime.loop())
{
Info<< "Time = " << runTime.timeName() << nl << endl;
fvVectorMatrix divR = turbulence->divDevReff(U);
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());
label id = y.size() - 1;
scalar wallShearStress =
flowDirection & turbulence->R()()[id] & wallNormal;
scalar yplusWall
// = 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;
return 0;
}
// ************************************************************************* //