Commit 649c29f9 authored by quant's avatar quant
Browse files

Initial commit

parent 89db0b5a
EXE_INC = \
-I.. \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \
-I$(LIB_SRC)/transportModels \
-I$(LIB_SRC)/transportModels/incompressible/singlePhaseTransportModel
EXE_LIBS = \
-lfiniteVolume \
-lfvOptions \
-lmeshTools \
-lsampling \
-lturbulenceModels \
-lincompressibleTurbulenceModels \
-lincompressibleTransportModels
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2017 OpenFOAM Foundation
-------------------------------------------------------------------------------
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 3 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, see <http://www.gnu.org/licenses/>.
Application
SRFSimpleFoam
Group
grpIncompressibleSolvers
Description
Steady-state solver for incompressible, turbulent flow of non-Newtonian
fluids in a single rotating frame.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "singlePhaseTransportModel.H"
#include "turbulentTransportModel.H"
#include "SRFModel.H"
#include "simpleControl.H"
#include "fvOptions.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
argList::addNote
(
"Steady-state solver for incompressible, turbulent flow"
" of non-Newtonian fluids in a single rotating frame."
);
#include "postProcess.H"
#include "addCheckCaseOptions.H"
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createMesh.H"
#include "createControl.H"
#include "createFields.H"
#include "initContinuityErrs.H"
turbulence->validate();
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while (simple.loop())
{
Info<< "Time = " << runTime.timeName() << nl << endl;
// --- Pressure-velocity SIMPLE corrector
{
#include "UrelEqn.H"
#include "pEqn.H"
}
U = Urel + SRF->U();
laminarTransport.correct();
turbulence->correct();
runTime.write();
runTime.printExecutionTime(Info);
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //
// Relative momentum predictor
tmp<fvVectorMatrix> tUrelEqn
(
fvm::div(phi, Urel)
+ turbulence->divDevReff(Urel)
+ SRF->Su()
==
fvOptions(Urel)
);
fvVectorMatrix& UrelEqn = tUrelEqn.ref();
UrelEqn.relax();
fvOptions.constrain(UrelEqn);
if (simple.momentumPredictor())
{
solve(UrelEqn == -fvc::grad(p));
fvOptions.correct(Urel);
}
Info<< "Reading field p\n" << endl;
volScalarField p
(
IOobject
(
"p",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
Info<< "Reading field Urel\n" << endl;
volVectorField Urel
(
IOobject
(
"Urel",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
Info<< "Reading/calculating face flux field phi\n" << endl;
surfaceScalarField phi
(
IOobject
(
"phi",
runTime.timeName(),
mesh,
IOobject::READ_IF_PRESENT,
IOobject::AUTO_WRITE
),
linearInterpolate(Urel) & mesh.Sf()
);
label pRefCell = 0;
scalar pRefValue = 0.0;
setRefCell(p, simple.dict(), pRefCell, pRefValue);
mesh.setFluxRequired(p.name());
Info<< "Creating SRF model\n" << endl;
autoPtr<SRF::SRFModel> SRF(SRF::SRFModel::New(Urel));
// Construct the absolute velocity
volVectorField U
(
IOobject
(
"U",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::AUTO_WRITE
),
Urel + SRF->U()
);
singlePhaseTransportModel laminarTransport(U, phi);
autoPtr<incompressible::turbulenceModel> turbulence
(
incompressible::turbulenceModel::New(U, phi, laminarTransport)
);
#include "createFvOptions.H"
{
volScalarField rAUrel(1.0/UrelEqn.A());
volVectorField HbyA("HbyA", Urel);
HbyA = rAUrel*UrelEqn.H();
surfaceScalarField phiHbyA("phiHbyA", fvc::flux(HbyA));
adjustPhi(phiHbyA, Urel, p);
tmp<volScalarField> rAtUrel(rAUrel);
if (simple.consistent())
{
rAtUrel = 1.0/(1.0/rAUrel - UrelEqn.H1());
phiHbyA +=
fvc::interpolate(rAtUrel() - rAUrel)*fvc::snGrad(p)*mesh.magSf();
HbyA -= (rAUrel - rAtUrel())*fvc::grad(p);
}
tUrelEqn.clear();
// Update the pressure BCs to ensure flux consistency
constrainPressure(p, Urel, phiHbyA, rAtUrel());
// Non-orthogonal pressure corrector loop
while (simple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::laplacian(rAtUrel(), p) == fvc::div(phiHbyA)
);
pEqn.setReference(pRefCell, pRefValue);
pEqn.solve();
if (simple.finalNonOrthogonalIter())
{
phi = phiHbyA - pEqn.flux();
}
}
#include "continuityErrs.H"
// Explicitly relax pressure for momentum corrector
p.relax();
// Momentum corrector
Urel = HbyA - rAtUrel()*fvc::grad(p);
Urel.correctBoundaryConditions();
fvOptions.correct(Urel);
}
// Momentum predictor
MRF.correctBoundaryVelocity(U);
tmp<fvVectorMatrix> tUEqn
(
fvm::div(phi, U)
+ MRF.DDt(U)
+ turbulence->divDevReff(U)
==
fvOptions(U)
);
fvVectorMatrix& UEqn = tUEqn.ref();
UEqn.relax();
fvOptions.constrain(UEqn);
if (simple.momentumPredictor())
{
solve(UEqn == -fvc::grad(p));
fvOptions.correct(U);
}
Info<< "Reading field p\n" << endl;
volScalarField p
(
IOobject
(
"p",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
Info<< "Reading field U\n" << endl;
volVectorField U
(
IOobject
(
"U",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
#include "createPhi.H"
label pRefCell = 0;
scalar pRefValue = 0.0;
setRefCell(p, simple.dict(), pRefCell, pRefValue);
mesh.setFluxRequired(p.name());
singlePhaseTransportModel laminarTransport(U, phi);
autoPtr<incompressible::turbulenceModel> turbulence
(
incompressible::turbulenceModel::New(U, phi, laminarTransport)
);
#include "createMRF.H"
#include "createFvOptions.H"
EXE_INC = \
-I$(FOAM_SOLVERS)/incompressible/pimpleFoam/overPimpleDyMFoam \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \
-I$(LIB_SRC)/transportModels \
-I$(LIB_SRC)/transportModels/incompressible/singlePhaseTransportModel \
-I$(LIB_SRC)/dynamicMesh/lnInclude \
-I$(LIB_SRC)/dynamicFvMesh/lnInclude \
-I$(LIB_SRC)/overset/lnInclude
EXE_LIBS = \
-lfiniteVolume \
-lfvOptions \
-lsampling \
-lturbulenceModels \
-lincompressibleTurbulenceModels \
-lincompressibleTransportModels \
-ldynamicMesh \
-ldynamicFvMesh \
-ltopoChangerFvMesh \
-loverset
// Momentum predictor
MRF.correctBoundaryVelocity(U);
tmp<fvVectorMatrix> tUEqn
(
fvm::div(phi, U)
+ MRF.DDt(U)
+ turbulence->divDevReff(U)
==
fvOptions(U)
);
fvVectorMatrix& UEqn = tUEqn.ref();
UEqn.relax();
fvOptions.constrain(UEqn);
if (simple.momentumPredictor())
{
solve(UEqn == -cellMask*fvc::grad(p));
}
fvOptions.correct(U);
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011 OpenFOAM Foundation
Copyright (C) 2016 OpenCFD Ltd.
-------------------------------------------------------------------------------
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 3 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, see <http://www.gnu.org/licenses/>.
Global
continuityErrs
Description
Calculates and prints the continuity errors.
\*---------------------------------------------------------------------------*/
{
volScalarField contErr(interpolatedCells*cellMask*fvc::div(phi));
scalar sumLocalContErr = runTime.deltaTValue()*
mag(contErr)().weightedAverage(mesh.V()).value();
scalar globalContErr = runTime.deltaTValue()*
contErr.weightedAverage(mesh.V()).value();
cumulativeContErr += globalContErr;
Info<< "time step continuity errors : sum local = " << sumLocalContErr
<< ", global = " << globalContErr
<< ", cumulative = " << cumulativeContErr
<< endl;
}
// ************************************************************************* //
Info<< "Reading field p\n" << endl;
volScalarField p
(
IOobject
(
"p",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
Info<< "Reading field U\n" << endl;
volVectorField U
(
IOobject
(
"U",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
#include "createPhi.H"
label pRefCell = 0;
scalar pRefValue = 0.0;
setRefCell(p, simple.dict(), pRefCell, pRefValue);
mesh.setFluxRequired(p.name());
singlePhaseTransportModel laminarTransport(U, phi);
autoPtr<incompressible::turbulenceModel> turbulence
(
incompressible::turbulenceModel::New(U, phi, laminarTransport)
);
#include "createMRF.H"
//- Overset specific
// Add solver-specific interpolations
{
wordHashSet& nonInt =
const_cast<wordHashSet&>(Stencil::New(mesh).nonInterpolatedFields());
nonInt.insert("HbyA");
nonInt.insert("grad(p)");
nonInt.insert("surfaceIntegrate(phi)");
nonInt.insert("surfaceIntegrate(phiHbyA)");
nonInt.insert("cellMask");
nonInt.insert("cellDisplacement");
nonInt.insert("interpolatedCells");
nonInt.insert("cellInterpolationWeight");
}
// Mask field for zeroing out contributions on hole cells
#include "createCellMask.H"
#include "createInterpolatedCells.H"
bool adjustFringe
(
simple.dict().getOrDefault("oversetAdjustPhi", false)
);
bool massFluxInterpolation
(
simple.dict().getOrDefault("massFluxInterpolation", false)
);
Info<< "Create dynamic mesh for time = "
<< runTime.timeName() << nl << endl;
autoPtr<dynamicFvMesh> meshPtr
(
dynamicFvMesh::New
(
IOobject
(
polyMesh::defaultRegion,
runTime.timeName(),
runTime,
IOobject::MUST_READ
)
)
);
dynamicFvMesh& mesh = meshPtr();
// Calculate initial mesh-to-mesh mapping. Note that this should be
// done under the hood, e.g. as a MeshObject
mesh.update();
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2014 OpenFOAM Foundation
Copyright (C) 2016-2017 OpenCFD Ltd.
-------------------------------------------------------------------------------
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 3 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, see <http://www.gnu.org/licenses/>.
Application
overSimpleFoam
Group
grpIncompressibleSolvers
Description
Steady-state solver for incompressible flows with turbulence modelling.
\heading Solver details
The solver uses the SIMPLE algorithm to solve the continuity equation:
\f[
\div \vec{U} = 0
\f]
and momentum equation:
\f[
\div \left( \vec{U} \vec{U} \right) - \div \gvec{R}
= - \grad p + \vec{S}_U
\f]
Where:
\vartable
\vec{U} | Velocity
p | Pressure
\vec{R} | Stress tensor
\vec{S}_U | Momentum source
\endvartable
\heading Required fields
\plaintable
U | Velocity [m/s]
p | Kinematic pressure, p/rho [m2/s2]
\<turbulence fields\> | As required by user selection
\endplaintable
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "singlePhaseTransportModel.H"
#include "turbulentTransportModel.H"
#include "simpleControl.H"
#include "fvOptions.H"
#include "dynamicFvMesh.H"
#include "cellCellStencilObject.H"
#include "localMin.H"
#include "interpolationCellPoint.H"
#include "fvMeshSubset.H"
#include "transform.H"
#include "oversetAdjustPhi.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
argList::addNote
(
"Steady-state solver for incompressible, turbulent flow"
);
#define CREATE_MESH createUpdatedDynamicFvMesh.H
#include "postProcess.H"
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createUpdatedDynamicFvMesh.H"
#include "createControl.H"
#include "createFields.H"
#include "createOversetFields.H"
#include "createFvOptions.H"
#include "initContinuityErrs.H"
turbulence->validate();
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while (simple.loop())
{
Info<< "Time = " << runTime.timeName() << nl << endl;
// --- Pressure-velocity SIMPLE corrector
{
#include "UEqn.H"
#include "pEqn.H"
}
laminarTransport.correct();
turbulence->correct();
runTime.write();
runTime.printExecutionTime(Info);
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //
{
surfaceScalarField faceMask(localMin<scalar>(mesh).interpolate(cellMask));
volScalarField rAU(1.0/UEqn.A());
surfaceScalarField rAUf("rAUf", faceMask*fvc::interpolate(rAU));
volVectorField HbyA("HbyA", U);
HbyA = constrainHbyA(cellMask*rAU*UEqn.H(), U, p);
//mesh.interpolate(HbyA);
if (massFluxInterpolation)
{
#include "interpolatedFaces.H"
}
tUEqn.clear();
surfaceScalarField phiHbyA("phiHbyA", fvc::flux(HbyA));
adjustPhi(phiHbyA, U, p);
if (adjustFringe)
{
oversetAdjustPhi(phiHbyA, U);
}
// Non-orthogonal pressure corrector loop
while (simple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::laplacian(rAUf, p) == fvc::div(phiHbyA)
);
pEqn.setReference(pRefCell, pRefValue);
pEqn.solve();
if (simple.finalNonOrthogonalIter())
{
phi = phiHbyA - pEqn.flux();
}
}
#include "continuityErrs.H"
// Explicitly relax pressure for momentum corrector
p.relax();
// Momentum corrector
volVectorField gradP(fvc::grad(p));
//mesh.interpolate(gradP);
U = HbyA - rAU*cellMask*gradP;
U.correctBoundaryConditions();
fvOptions.correct(U);
}
{
volScalarField rAU(1.0/UEqn.A());
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
surfaceScalarField phiHbyA("phiHbyA", fvc::flux(HbyA));
MRF.makeRelative(phiHbyA);
adjustPhi(phiHbyA, U, p);
tmp<volScalarField> rAtU(rAU);
if (simple.consistent())
{
rAtU = 1.0/(1.0/rAU - UEqn.H1());
phiHbyA +=
fvc::interpolate(rAtU() - rAU)*fvc::snGrad(p)*mesh.magSf();
HbyA -= (rAU - rAtU())*fvc::grad(p);
}
tUEqn.clear();
// Update the pressure BCs to ensure flux consistency
constrainPressure(p, U, phiHbyA, rAtU(), MRF);
// Non-orthogonal pressure corrector loop
while (simple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::laplacian(rAtU(), p) == fvc::div(phiHbyA)
);
pEqn.setReference(pRefCell, pRefValue);
pEqn.solve();
if (simple.finalNonOrthogonalIter())
{
phi = phiHbyA - pEqn.flux();
}
}
#include "continuityErrs.H"
// Explicitly relax pressure for momentum corrector
p.relax();
// Momentum corrector
U = HbyA - rAtU()*fvc::grad(p);
U.correctBoundaryConditions();
fvOptions.correct(U);
}
EXE_INC = \
-I.. \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
-I$(LIB_SRC)/TurbulenceModels/incompressible/lnInclude \
-I$(LIB_SRC)/transportModels \
-I$(LIB_SRC)/transportModels/incompressible/singlePhaseTransportModel
EXE_LIBS = \
-lfiniteVolume \
-lfvOptions \
-lmeshTools \
-lsampling \
-lturbulenceModels \
-lincompressibleTurbulenceModels \
-lincompressibleTransportModels
// Construct the Momentum equation
MRF.correctBoundaryVelocity(U);
tmp<fvVectorMatrix> tUEqn
(
fvm::div(phi, U)
+ MRF.DDt(U)
+ turbulence->divDevReff(U)
==
fvOptions(U)
);
fvVectorMatrix& UEqn = tUEqn.ref();
UEqn.relax();
// Include the porous media resistance and solve the momentum equation
// either implicit in the tensorial resistance or transport using by
// including the spherical part of the resistance in the momentum diagonal
tmp<volScalarField> trAU;
tmp<volTensorField> trTU;
if (pressureImplicitPorosity)
{
tmp<volTensorField> tTU = tensor(I)*UEqn.A();
pZones.addResistance(UEqn, tTU.ref());
trTU = inv(tTU());
trTU.ref().rename("rAU");
fvOptions.constrain(UEqn);
volVectorField gradp(fvc::grad(p));
for (int UCorr=0; UCorr<nUCorr; UCorr++)
{
U = trTU() & (UEqn.H() - gradp);
}
U.correctBoundaryConditions();
fvOptions.correct(U);
}
else
{
pZones.addResistance(UEqn);
fvOptions.constrain(UEqn);
solve(UEqn == -fvc::grad(p));
fvOptions.correct(U);
trAU = 1.0/UEqn.A();
trAU.ref().rename("rAU");
}
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