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new solver
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buoyantBoussinesqFoam.C
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EXE = $(FOAM_APPBIN)/buoyantBoussinesqFoam
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EXE_INC = \
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-I$(LIB_SRC)/finiteVolume/lnInclude \
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-I$(LIB_SRC)/turbulenceModels \
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-I$(LIB_SRC)/turbulenceModels/incompressible/RAS/lnInclude \
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-I$(LIB_SRC)/transportModels \
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-I$(LIB_SRC)/transportModels/incompressible/singlePhaseTransportModel
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EXE_LIBS = \
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-lfiniteVolume \
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-lmeshTools \
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-lincompressibleRASModels \
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-lincompressibleTransportModels
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{
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volScalarField kappaEff
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(
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"kappaEff",
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turbulence->nu() + turbulence->nut()/Prt
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);
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fvScalarMatrix TEqn
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(
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fvm::ddt(T)
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+ fvm::div(phi, T)
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- fvm::laplacian(kappaEff, T)
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);
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TEqn.relax();
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TEqn.solve();
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}
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// Solve the momentum equation
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tmp<fvVectorMatrix> UEqn
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(
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fvm::ddt(U)
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+ fvm::div(phi, U)
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+ turbulence->divDevReff(U)
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);
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UEqn().relax();
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solve
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(
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UEqn()
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==
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-fvc::reconstruct
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(
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(
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fvc::snGrad(pd)
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- betaghf*fvc::snGrad(T)
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) * mesh.magSf()
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)
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);
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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 (C) 1991-2009 OpenCFD Ltd.
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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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buoyantBoussinesqSimpleFoam
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Description
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Steady-state solver for buoyant, turbulent flow of incompressible fluids
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Uses the Boussinesq approximation:
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\f[
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rho_{eff} = 1 - beta(T - T_{ref})
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\f]
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where:
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\f$ rho_{eff} \f$ = the effective (driving) density
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beta = thermal expansion coefficient [1/K]
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T = temperature [K]
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\f$ T_{ref} \f$ = reference temperature [K]
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Valid when:
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\f[
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rho_{eff} << 1
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\f]
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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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// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
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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 "readEnvironmentalProperties.H"
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# include "createFields.H"
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# include "initContinuityErrs.H"
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# include "readTimeControls.H"
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# include "CourantNo.H"
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# include "setInitialDeltaT.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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# include "readTimeControls.H"
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# include "readPISOControls.H"
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# include "CourantNo.H"
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# include "setDeltaT.H"
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# include "UEqn.H"
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// --- PISO loop
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for (int corr=0; corr<nCorr; corr++)
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{
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# include "TEqn.H"
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# include "pdEqn.H"
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}
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turbulence->correct();
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if (runTime.write())
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{
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# include "writeAdditionalFields.H"
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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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Info<< "Reading thermophysical properties\n" << endl;
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Info<< "Reading field T\n" << endl;
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volScalarField T
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(
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IOobject
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(
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"T",
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runTime.timeName(),
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mesh,
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IOobject::MUST_READ,
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IOobject::AUTO_WRITE
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),
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mesh
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);
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// kinematic pd
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Info<< "Reading field pd\n" << endl;
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volScalarField pd
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(
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IOobject
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(
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"pd",
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runTime.timeName(),
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mesh,
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IOobject::MUST_READ,
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IOobject::AUTO_WRITE
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),
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mesh
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);
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Info<< "Reading field U\n" << endl;
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volVectorField U
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(
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IOobject
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(
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"U",
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runTime.timeName(),
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mesh,
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IOobject::MUST_READ,
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IOobject::AUTO_WRITE
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),
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mesh
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);
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# include "createPhi.H"
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# include "readTransportProperties.H"
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Info<< "Creating turbulence model\n" << endl;
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autoPtr<incompressible::RASModel> turbulence
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(
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incompressible::RASModel::New(U, phi, laminarTransport)
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);
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Info<< "Calculating field beta*(g.h)\n" << endl;
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surfaceScalarField betaghf("betagh", beta*(g & mesh.Cf()));
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label pdRefCell = 0;
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scalar pdRefValue = 0.0;
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setRefCell
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(
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pd,
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mesh.solutionDict().subDict("SIMPLE"),
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pdRefCell,
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pdRefValue
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);
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{
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volScalarField rUA("rUA", 1.0/UEqn().A());
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surfaceScalarField rUAf("(1|A(U))", fvc::interpolate(rUA));
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U = rUA*UEqn().H();
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UEqn.clear();
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phi =
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(fvc::interpolate(U) & mesh.Sf())
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+ fvc::ddtPhiCorr(rUA, U, phi)
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+ betaghf*fvc::snGrad(T)*rUAf*mesh.magSf();
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for (int nonOrth=0; nonOrth<=nNonOrthCorr; nonOrth++)
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{
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fvScalarMatrix pdEqn
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(
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fvm::laplacian(rUAf, pd) == fvc::div(phi)
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);
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// retain the residual from the first iteration
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if (nonOrth == 0)
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{
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pdEqn.solve(mesh.solver(pd.name() + "Final"));
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}
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else
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{
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pdEqn.solve(mesh.solver(pd.name()));
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}
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if (nonOrth == nNonOrthCorr)
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{
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// Calculate the conservative fluxes
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phi -= pdEqn.flux();
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// Correct the momentum source with the pressure gradient flux
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// calculated from the relaxed pressure
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U -=
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rUA
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*fvc::reconstruct((pdEqn.flux() - betaghf*fvc::snGrad(T))/rUAf);
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U.correctBoundaryConditions();
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}
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}
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#include "continuityErrs.H"
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}
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@ -0,0 +1,13 @@
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singlePhaseTransportModel laminarTransport(U, phi);
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// thermal expansion coefficient [1/K]
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dimensionedScalar beta(laminarTransport.lookup("beta"));
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// reference temperature [K]
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dimensionedScalar TRef(laminarTransport.lookup("TRef"));
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// reference kinematic pressure [m2/s2]
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dimensionedScalar pRef(laminarTransport.lookup("pRef"));
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// turbulent Prandtl number
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dimensionedScalar Prt(laminarTransport.lookup("Prt"));
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@ -0,0 +1,29 @@
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{
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volScalarField rhoEff
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(
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IOobject
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(
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"rhoEff",
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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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1.0 - beta*(T - TRef)
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);
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rhoEff.write();
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volScalarField p
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(
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IOobject
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(
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"p",
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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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pd + rhoEff*(g & mesh.C()) + pRef
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);
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p.write();
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}
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