Commit ea17556c authored by shunbo's avatar shunbo
Browse files

Initial commit

parents
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$(LIB_SRC)/transportModels/incompressible/singlePhaseTransportModel \
-I$(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
// Solve the Momentum equation
MRF.correctBoundaryVelocity(U);
tmp<fvVectorMatrix> tUEqn
(
fvm::ddt(U) + fvm::div(phi, U)
+ MRF.DDt(U)
+ turbulence->divDevReff(U)
==
fvOptions(U)
);
fvVectorMatrix& UEqn = tUEqn.ref();
UEqn.relax();
fvOptions.constrain(UEqn);
if (pimple.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;
}
// ************************************************************************* //
if (mesh.changing())
{
volVectorField::Boundary& bfld = U.boundaryFieldRef();
forAll(bfld, patchi)
{
if (bfld[patchi].fixesValue())
{
bfld[patchi].initEvaluate();
}
}
surfaceScalarField::Boundary& phiBfld = phi.boundaryFieldRef();
forAll(bfld, patchi)
{
if (bfld[patchi].fixesValue())
{
bfld[patchi].evaluate();
phiBfld[patchi] = bfld[patchi] & mesh.Sf().boundaryField()[patchi];
}
}
}
// Initialize BCs list for pcorr to zero-gradient
wordList pcorrTypes
(
p.boundaryField().size(),
zeroGradientFvPatchScalarField::typeName
);
// Set BCs of pcorr to fixed-value for patches at which p is fixed
forAll(p.boundaryField(), patchi)
{
if (p.boundaryField()[patchi].fixesValue())
{
pcorrTypes[patchi] = fixedValueFvPatchScalarField::typeName;
}
}
volScalarField pcorr
(
IOobject
(
"pcorr",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::NO_WRITE
),
mesh,
dimensionedScalar(p.dimensions(), Zero),
pcorrTypes
);
{
dimensionedScalar rAUf("rAUf", dimTime, 1.0);
const cellCellStencilObject& overlap = Stencil::New(mesh);
const labelList& cellTypes = overlap.cellTypes();
const labelIOList& zoneIDs = overlap.zoneID();
while (pimple.correctNonOrthogonal())
{
label nZones = gMax(zoneIDs)+1;
//label refCellI2 = -1;
labelList refCells(nZones, -1);
labelList refZones(nZones, -1);
forAll(zoneIDs, cellI)
{
label zoneId = zoneIDs[cellI];
if
(
refCells[zoneId] == -1
&& cellTypes[cellI] == cellCellStencil::CALCULATED
&& refZones[zoneId] == -1
)
{
refCells[zoneId] = cellI;
refZones[zoneId] = zoneId;
}
}
fvScalarMatrix pcorrEqn
(
fvm::laplacian(rAUf, pcorr) == fvc::div(phi)
);
// Only set reference for cells that are CALCULATED
{
DynamicList<label> validCells(refCells.size());
forAll(refCells, zoneId)
{
if (refCells[zoneId] != -1)
{
validCells.append(refCells[zoneId]);
}
}
pcorrEqn.setReferences
(
validCells,
scalar(0),
true
);
}
const dictionary& d = mesh.solver
(
pcorr.select
(
pimple.finalInnerIter()
)
);
//Bypass virtual layer
mesh.fvMesh::solve(pcorrEqn, d);
if (pimple.finalNonOrthogonalIter())
{
phi -= pcorrEqn.flux();
}
}
}
#include "createTimeControls.H"
bool correctPhi
(
pimple.dict().getOrDefault("correctPhi", false)
);
bool checkMeshCourantNo
(
pimple.dict().getOrDefault("checkMeshCourantNo", false)
);
bool massFluxInterpolation
(
pimple.dict().getOrDefault("massFluxInterpolation", false)
);
bool adjustFringe
(
pimple.dict().getOrDefault("oversetAdjustPhi", false)
);
bool ddtCorr
(
pimple.dict().getOrDefault("ddtCorr", true)
);
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, pimple.dict(), pRefCell, pRefValue);
mesh.setFluxRequired(p.name());
//- 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"
// Create bool field with interpolated cells
#include "createInterpolatedCells.H"
singlePhaseTransportModel laminarTransport(U, phi);
autoPtr<incompressible::turbulenceModel> turbulence
(
incompressible::turbulenceModel::New(U, phi, laminarTransport)
);
surfaceScalarField phiHbyA
(
IOobject
(
"phiHbyA",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::AUTO_WRITE
),
fvc::flux(U)
);
// Interpolation used
interpolationCellPoint<vector> UInterpolator(HbyA);
// Determine faces on outside of interpolated cells
bitSet isOwnerInterpolatedFace(mesh.nInternalFaces());
bitSet isNeiInterpolatedFace(mesh.nInternalFaces());
// Determine donor cells
labelListList donorCell(mesh.nInternalFaces());
scalarListList weightCellCells(mesh.nInternalFaces());
// Interpolated HbyA faces
vectorField UIntFaces(mesh.nInternalFaces(), Zero);
// Determine receptor neighbour cells
labelList receptorNeigCell(mesh.nInternalFaces(), -1);
{
const cellCellStencilObject& overlap = Stencil::New(mesh);
const labelList& cellTypes = overlap.cellTypes();
const labelIOList& zoneID = overlap.zoneID();
label nZones = gMax(zoneID)+1;
PtrList<fvMeshSubset> meshParts(nZones);
labelList nCellsPerZone(nZones, Zero);
// A mesh subset for each zone
forAll(meshParts, zonei)
{
meshParts.set
(
zonei,
// Select cells where the zoneID == zonei
new fvMeshSubset(mesh, zonei, zoneID)
);
}
for (label faceI = 0; faceI < mesh.nInternalFaces(); faceI++)
{
label ownType = cellTypes[mesh.faceOwner()[faceI]];
label neiType = cellTypes[mesh.faceNeighbour()[faceI]];
if
(
ownType == cellCellStencil::INTERPOLATED
&& neiType == cellCellStencil::CALCULATED
)
{
isOwnerInterpolatedFace.set(faceI);
const vector& fc = mesh.faceCentres()[faceI];
for (label zoneI = 0; zoneI < nZones; zoneI++)
{
if (zoneI != zoneID[mesh.faceOwner()[faceI]])
{
const fvMesh& partMesh = meshParts[zoneI].subMesh();
const labelList& cellMap = meshParts[zoneI].cellMap();
label cellI = partMesh.findCell(fc);
if (cellI != -1)
{
// Determine weights
labelList stencil(partMesh.cellCells()[cellI]);
stencil.append(cellI);
label st = stencil.size();
donorCell[faceI].setSize(st);
weightCellCells[faceI].setSize(st);
scalarField weights(st);
forAll(stencil, i)
{
scalar d = mag
(
partMesh.cellCentres()[stencil[i]]
- fc
);
weights[i] = 1.0/d;
donorCell[faceI][i] = cellMap[stencil[i]];
}
weights /= sum(weights);
weightCellCells[faceI] = weights;
forAll(stencil, i)
{
UIntFaces[faceI] +=
weightCellCells[faceI][i]
*UInterpolator.interpolate
(
fc,
donorCell[faceI][i]
);
}
break;
}
}
}
receptorNeigCell[faceI] = mesh.faceNeighbour()[faceI];
}
else if
(
ownType == cellCellStencil::CALCULATED
&& neiType == cellCellStencil::INTERPOLATED
)
{
isNeiInterpolatedFace.set(faceI);
const vector& fc = mesh.faceCentres()[faceI];
for (label zoneI = 0; zoneI < nZones; zoneI++)
{
if (zoneI != zoneID[mesh.faceNeighbour()[faceI]])
{
const fvMesh& partMesh = meshParts[zoneI].subMesh();
const labelList& cellMap = meshParts[zoneI].cellMap();
label cellI = partMesh.findCell(fc);
if (cellI != -1)
{
// Determine weights
labelList stencil(partMesh.cellCells()[cellI]);
stencil.append(cellI);
label st = stencil.size();
donorCell[faceI].setSize(st);
weightCellCells[faceI].setSize(st);
scalarField weights(st);
forAll(stencil, i)
{
scalar d = mag
(
partMesh.cellCentres()[stencil[i]]
- fc
);
weights[i] = 1.0/d;
donorCell[faceI][i] = cellMap[stencil[i]];
}
weights /= sum(weights);
weightCellCells[faceI] = weights;
forAll(stencil, i)
{
UIntFaces[faceI] +=
weightCellCells[faceI][i]
*UInterpolator.interpolate
(
fc,
donorCell[faceI][i]
);
}
break;
}
}
}
receptorNeigCell[faceI] = mesh.faceOwner()[faceI];
}
}
}
// contravariant U
vectorField U1Contrav(mesh.nInternalFaces(), Zero);
surfaceVectorField faceNormals(mesh.Sf()/mesh.magSf());
forAll(isNeiInterpolatedFace, faceI)
{
label cellId = -1;
if (isNeiInterpolatedFace.test(faceI))
{
cellId = mesh.faceNeighbour()[faceI];
}
else if (isOwnerInterpolatedFace.test(faceI))
{
cellId = mesh.faceOwner()[faceI];
}
if (cellId != -1)
{
const vector& n = faceNormals[faceI];
vector n1(Zero);
// 2-D cases
if (mesh.nSolutionD() == 2)
{
for (direction cmpt=0; cmpt<vector::nComponents; cmpt++)
{
if (mesh.geometricD()[cmpt] == -1)
{
switch (cmpt)
{
case vector::X:
{
n1 = vector(0, n.z(), -n.y());
break;
}
case vector::Y:
{
n1 = vector(n.z(), 0, -n.x());
break;
}
case vector::Z:
{
n1 = vector(n.y(), -n.x(), 0);
break;
}
}
}
}
}
else if (mesh.nSolutionD() == 3)
{
//Determine which is the primary direction
if (mag(n.x()) > mag(n.y()) && mag(n.x()) > mag(n.z()))
{
n1 = vector(n.y(), -n.x(), 0);
}
else if (mag(n.y()) > mag(n.z()))
{
n1 = vector(0, n.z(), -n.y());
}
else
{
n1 = vector(-n.z(), 0, n.x());
}
}
n1.normalise();
const vector n2 = normalised(n ^ n1);
tensor rot =
tensor
(
n.x() ,n.y(), n.z(),
n1.x() ,n1.y(), n1.z(),
n2.x() ,n2.y(), n2.z()
);
// tensor rot =
// tensor
// (
// n & x ,n & y, n & z,
// n1 & x ,n1 & y, n1 & z,
// n2 & x ,n2 & y, n2 & z
// );
U1Contrav[faceI].x() =
2*transform(rot, UIntFaces[faceI]).x()
- transform(rot, HbyA[receptorNeigCell[faceI]]).x();
U1Contrav[faceI].y() = transform(rot, HbyA[cellId]).y();
U1Contrav[faceI].z() = transform(rot, HbyA[cellId]).z();
HbyA[cellId] = transform(inv(rot), U1Contrav[faceI]);
}
}
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2016 OpenFOAM Foundation
Copyright (C) 2016-2018 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
overPimpleDyMFoam
Group
grpIncompressibleSolvers grpMovingMeshSolvers
Description
Transient solver for incompressible flow of Newtonian fluids
on a moving mesh using the PIMPLE (merged PISO-SIMPLE) algorithm.
Turbulence modelling is generic, i.e. laminar, RAS or LES may be selected.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "singlePhaseTransportModel.H"
#include "turbulentTransportModel.H"
#include "pimpleControl.H"
#include "fvOptions.H"
#include "cellCellStencilObject.H"
#include "zeroGradientFvPatchFields.H"
#include "localMin.H"
#include "interpolationCellPoint.H"
#include "transform.H"
#include "fvMeshSubset.H"
#include "oversetAdjustPhi.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
argList::addNote
(
"Transient solver for incompressible, turbulent flow"
" on a moving mesh."
);
#include "postProcess.H"
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createDynamicFvMesh.H"
#include "initContinuityErrs.H"
pimpleControl pimple(mesh);
#include "createFields.H"
#include "createUf.H"
#include "createMRF.H"
#include "createFvOptions.H"
#include "createControls.H"
#include "CourantNo.H"
#include "setInitialDeltaT.H"
turbulence->validate();
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while (runTime.run())
{
#include "readControls.H"
#include "CourantNo.H"
#include "setDeltaT.H"
++runTime;
Info<< "Time = " << runTime.timeName() << nl << endl;
bool changed = mesh.update();
if (changed)
{
#include "setCellMask.H"
#include "setInterpolatedCells.H"
surfaceScalarField faceMaskOld
(
localMin<scalar>(mesh).interpolate(cellMask.oldTime())
);
// Zero Uf on old faceMask (H-I)
Uf *= faceMaskOld;
// Update Uf and phi on new C-I faces
Uf += (1-faceMaskOld)*fvc::interpolate(U);
phi = mesh.Sf() & Uf;
// Zero phi on current H-I
surfaceScalarField faceMask
(
localMin<scalar>(mesh).interpolate(cellMask)
);
phi *= faceMask;
}
if (mesh.changing() && correctPhi)
{
// Calculate absolute flux from the mapped surface velocity
#include "correctPhi.H"
}
// Make the flux relative to the mesh motion
fvc::makeRelative(phi, U);
if (mesh.changing() && checkMeshCourantNo)
{
#include "meshCourantNo.H"
}
// --- Pressure-velocity PIMPLE corrector loop
while (pimple.loop())
{
#include "UEqn.H"
// --- Pressure corrector loop
while (pimple.correct())
{
#include "pEqn.H"
}
if (pimple.turbCorr())
{
laminarTransport.correct();
turbulence->correct();
}
}
runTime.write();
runTime.printExecutionTime(Info);
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //
// Option 1: interpolate rAU, do not block out rAU on blocked cells
volScalarField rAU("rAU", 1.0/UEqn.A());
mesh.interpolate(rAU);
// Option 2: do not interpolate rAU but block out rAU
//surfaceScalarField rAUf("rAUf", fvc::interpolate(blockedCells*rAU));
// Option 3: do not interpolate rAU but zero out rAUf on faces on holes
// But what about:
//
// H
// H I C C C C
// H
//
surfaceScalarField rAUf("rAUf", fvc::interpolate(rAU));
volVectorField H("H", UEqn.H());
volVectorField HbyA("HbyA", U);
HbyA = constrainHbyA(rAU*H, U, p);
if (massFluxInterpolation)
{
#include "interpolatedFaces.H"
}
if (runTime.outputTime())
{
H.write();
rAU.write();
HbyA.write();
}
if (pimple.nCorrPISO() <= 1)
{
tUEqn.clear();
}
phiHbyA = fvc::flux(HbyA);
if (ddtCorr)
{
surfaceScalarField faceMaskOld
(
localMin<scalar>(mesh).interpolate(cellMask.oldTime())
);
phiHbyA += rAUf*faceMaskOld*fvc::ddtCorr(U, Uf);
}
MRF.makeRelative(phiHbyA);
// WIP
if (p.needReference())
{
fvc::makeRelative(phiHbyA, U);
adjustPhi(phiHbyA, U, p);
fvc::makeAbsolute(phiHbyA, U);
}
if (adjustFringe)
{
fvc::makeRelative(phiHbyA, U);
oversetAdjustPhi(phiHbyA, U);
fvc::makeAbsolute(phiHbyA, U);
}
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::laplacian(rAUf, p) == fvc::div(phiHbyA)
);
pEqn.setReference(pRefCell, pRefValue);
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi = phiHbyA - pEqn.flux();
// option 2:
// rAUf*fvc::snGrad(p)*mesh.magSf();
}
}
#include "continuityErrs.H"
// Explicitly relax pressure for momentum corrector
p.relax();
volVectorField gradP(fvc::grad(p));
// Option 2: zero out velocity on blocked out cells
//U = HbyA - rAU*cellMask*gradP;
// Option 3: zero out velocity on blocked out cells
// This is needed for the scalar Eq (k,epsilon, etc)
// which can use U as source term
U = cellMask*(HbyA - rAU*gradP);
U.correctBoundaryConditions();
fvOptions.correct(U);
{
Uf = fvc::interpolate(U);
surfaceVectorField n(mesh.Sf()/mesh.magSf());
Uf += n*(phi/mesh.magSf() - (n & Uf));
}
// Make the fluxes relative to the mesh motion
fvc::makeRelative(phi, U);
surfaceScalarField faceMask
(
localMin<scalar>(mesh).interpolate(cellMask)
);
phi *= faceMask;
#include "readTimeControls.H"
correctPhi = pimple.dict().getOrDefault("correctPhi", false);
checkMeshCourantNo = pimple.dict().getOrDefault("checkMeshCourantNo", false);
massFluxInterpolation =
pimple.dict().getOrDefault("massFluxInterpolation", false);
ddtCorr = pimple.dict().getOrDefault("ddtCorr", true);
volScalarField rAU(1.0/UEqn.A());
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
surfaceScalarField phiHbyA("phiHbyA", fvc::flux(HbyA));
if (pimple.ddtCorr())
{
phiHbyA += MRF.zeroFilter(fvc::interpolate(rAU)*fvc::ddtCorr(U, phi, Uf));
}
MRF.makeRelative(phiHbyA);
if (p.needReference())
{
fvc::makeRelative(phiHbyA, U);
adjustPhi(phiHbyA, U, p);
fvc::makeAbsolute(phiHbyA, U);
}
tmp<volScalarField> rAtU(rAU);
if (pimple.consistent())
{
rAtU = 1.0/max(1.0/rAU - UEqn.H1(), 0.1/rAU);
phiHbyA +=
fvc::interpolate(rAtU() - rAU)*fvc::snGrad(p)*mesh.magSf();
HbyA -= (rAU - rAtU())*fvc::grad(p);
}
if (pimple.nCorrPISO() <= 1)
{
tUEqn.clear();
}
// Update the pressure BCs to ensure flux consistency
constrainPressure(p, U, phiHbyA, rAtU(), MRF);
// Non-orthogonal pressure corrector loop
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix pEqn
(
fvm::laplacian(rAtU(), p) == fvc::div(phiHbyA)
);
pEqn.setReference(pRefCell, pRefValue);
pEqn.solve(mesh.solver(p.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi = phiHbyA - pEqn.flux();
}
}
#include "continuityErrs.H"
// Explicitly relax pressure for momentum corrector
p.relax();
U = HbyA - rAtU*fvc::grad(p);
U.correctBoundaryConditions();
fvOptions.correct(U);
// Correct Uf if the mesh is moving
fvc::correctUf(Uf, U, phi);
// Make the fluxes relative to the mesh motion
fvc::makeRelative(phi, U);
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2017 OpenFOAM Foundation
Copyright (C) 2019 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
pimpleFoam.C
Group
grpIncompressibleSolvers
Description
Transient solver for incompressible, turbulent flow of Newtonian fluids
on a moving mesh.
\heading Solver details
The solver uses the PIMPLE (merged PISO-SIMPLE) algorithm to solve the
continuity equation:
\f[
\div \vec{U} = 0
\f]
and momentum equation:
\f[
\ddt{\vec{U}} + \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
Sub-models include:
- turbulence modelling, i.e. laminar, RAS or LES
- run-time selectable MRF and finite volume options, e.g. explicit porosity
\heading Required fields
\plaintable
U | Velocity [m/s]
p | Kinematic pressure, p/rho [m2/s2]
\<turbulence fields\> | As required by user selection
\endplaintable
Note
The motion frequency of this solver can be influenced by the presence
of "updateControl" and "updateInterval" in the dynamicMeshDict.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "dynamicFvMesh.H"
#include "singlePhaseTransportModel.H"
#include "turbulentTransportModel.H"
#include "pimpleControl.H"
#include "CorrectPhi.H"
#include "fvOptions.H"
#include "localEulerDdtScheme.H"
#include "fvcSmooth.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
argList::addNote
(
"Transient solver for incompressible, turbulent flow"
" of Newtonian fluids on a moving mesh."
);
#include "postProcess.H"
#include "addCheckCaseOptions.H"
#include "setRootCaseLists.H"
#include "createTime.H"
#include "createDynamicFvMesh.H"
#include "initContinuityErrs.H"
#include "createDyMControls.H"
#include "createFields.H"
#include "createUfIfPresent.H"
#include "CourantNo.H"
#include "setInitialDeltaT.H"
turbulence->validate();
if (!LTS)
{
#include "CourantNo.H"
#include "setInitialDeltaT.H"
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while (runTime.run())
{
#include "readDyMControls.H"
if (LTS)
{
#include "setRDeltaT.H"
}
else
{
#include "CourantNo.H"
#include "setDeltaT.H"
}
++runTime;
Info<< "Time = " << runTime.timeName() << nl << endl;
// --- Pressure-velocity PIMPLE corrector loop
while (pimple.loop())
{
if (pimple.firstIter() || moveMeshOuterCorrectors)
{
// Do any mesh changes
mesh.controlledUpdate();
if (mesh.changing())
{
MRF.update();
if (correctPhi)
{
// Calculate absolute flux
// from the mapped surface velocity
phi = mesh.Sf() & Uf();
#include "correctPhi.H"
// Make the flux relative to the mesh motion
fvc::makeRelative(phi, U);
}
if (checkMeshCourantNo)
{
#include "meshCourantNo.H"
}
}
}
#include "UEqn.H"
// --- Pressure corrector loop
while (pimple.correct())
{
#include "pEqn.H"
}
if (pimple.turbCorr())
{
laminarTransport.correct();
turbulence->correct();
}
}
runTime.write();
runTime.printExecutionTime(Info);
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //
{
volScalarField& rDeltaT = trDeltaT.ref();
const dictionary& pimpleDict = pimple.dict();
scalar maxCo
(
pimpleDict.getOrDefault<scalar>("maxCo", 0.8)
);
scalar rDeltaTSmoothingCoeff
(
pimpleDict.getOrDefault<scalar>("rDeltaTSmoothingCoeff", 0.02)
);
scalar rDeltaTDampingCoeff
(
pimpleDict.getOrDefault<scalar>("rDeltaTDampingCoeff", 1.0)
);
scalar maxDeltaT
(
pimpleDict.getOrDefault<scalar>("maxDeltaT", GREAT)
);
volScalarField rDeltaT0("rDeltaT0", rDeltaT);
// Set the reciprocal time-step from the local Courant number
rDeltaT.ref() = max
(
1/dimensionedScalar("maxDeltaT", dimTime, maxDeltaT),
fvc::surfaceSum(mag(phi))()()
/((2*maxCo)*mesh.V())
);
// Update the boundary values of the reciprocal time-step
rDeltaT.correctBoundaryConditions();
Info<< "Flow time scale min/max = "
<< gMin(1/rDeltaT.primitiveField())
<< ", " << gMax(1/rDeltaT.primitiveField()) << endl;
if (rDeltaTSmoothingCoeff < 1.0)
{
fvc::smooth(rDeltaT, rDeltaTSmoothingCoeff);
}
Info<< "Smoothed flow time scale min/max = "
<< gMin(1/rDeltaT.primitiveField())
<< ", " << gMax(1/rDeltaT.primitiveField()) << endl;
// Limit rate of change of time scale
// - reduce as much as required
// - only increase at a fraction of old time scale
if
(
rDeltaTDampingCoeff < 1.0
&& runTime.timeIndex() > runTime.startTimeIndex() + 1
)
{
rDeltaT =
rDeltaT0
*max(rDeltaT/rDeltaT0, scalar(1) - rDeltaTDampingCoeff);
Info<< "Damped flow time scale min/max = "
<< gMin(1/rDeltaT.primitiveField())
<< ", " << gMax(1/rDeltaT.primitiveField()) << endl;
}
}
pisoFoam.C
EXE = $(FOAM_APPBIN)/pisoFoam
EXE_INC = \
-I$(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
// Solve the Momentum equation
MRF.correctBoundaryVelocity(U);
fvVectorMatrix UEqn
(
fvm::ddt(U) + fvm::div(phi, U)
+ MRF.DDt(U)
+ turbulence->divDevReff(U)
==
fvOptions(U)
);
UEqn.relax();
fvOptions.constrain(UEqn);
if (piso.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, piso.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"
volScalarField rAU(1.0/UEqn.A());
volVectorField HbyA(constrainHbyA(rAU*UEqn.H(), U, p));
surfaceScalarField phiHbyA
(
"phiHbyA",
fvc::flux(HbyA)
+ MRF.zeroFilter(fvc::interpolate(rAU)*fvc::ddtCorr(U, phi))
);
MRF.makeRelative(phiHbyA);
adjustPhi(phiHbyA, U, p);
// Update the pressure BCs to ensure flux consistency
constrainPressure(p, U, phiHbyA, rAU, MRF);
// Non-orthogonal pressure corrector loop
while (piso.correctNonOrthogonal())
{
// Pressure corrector
fvScalarMatrix pEqn
(
fvm::laplacian(rAU, p) == fvc::div(phiHbyA)
);
pEqn.setReference(pRefCell, pRefValue);
pEqn.solve(mesh.solver(p.select(piso.finalInnerIter())));
if (piso.finalNonOrthogonalIter())
{
phi = phiHbyA - pEqn.flux();
}
}
#include "continuityErrs.H"
U = HbyA - rAU*fvc::grad(p);
U.correctBoundaryConditions();
fvOptions.correct(U);
/*---------------------------------------------------------------------------*\
========= |
\\ / 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
pisoFoam
Group
grpIncompressibleSolvers
Description
Transient solver for incompressible, turbulent flow, using the PISO
algorithm.
\heading Solver details
The solver uses the PISO algorithm to solve the continuity equation:
\f[
\div \vec{U} = 0
\f]
and momentum equation:
\f[
\ddt{\vec{U}} + \div \left( \vec{U} \vec{U} \right) - \div \gvec{R}
= - \grad p
\f]
Where:
\vartable
\vec{U} | Velocity
p | Pressure
\vec{R} | Stress tensor
\endvartable
Sub-models include:
- turbulence modelling, i.e. laminar, RAS or LES
- run-time selectable MRF and finite volume options, e.g. explicit porosity
\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 "pisoControl.H"
#include "fvOptions.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
argList::addNote
(
"Transient solver for incompressible, turbulent flow,"
" using the PISO algorithm."
);
#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 (runTime.loop())
{
Info<< "Time = " << runTime.timeName() << nl << endl;
#include "CourantNo.H"
// Pressure-velocity PISO corrector
{
#include "UEqn.H"
// --- PISO loop
while (piso.correct())
{
#include "pEqn.H"
}
}
laminarTransport.correct();
turbulence->correct();
runTime.write();
runTime.printExecutionTime(Info);
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | www.openfoam.com
\\/ M anipulation |
-------------------------------------------------------------------------------
Copyright (C) 2011-2016 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/>.
Global
CourantNo
Description
Calculates and outputs the maximum Courant Number.
\*---------------------------------------------------------------------------*/
scalar CoNum = 0.0;
scalar meanCoNum = 0.0;
scalar waveCoNum = 0.0;
if (mesh.nInternalFaces())
{
scalarField sumPhi
(
fvc::surfaceSum(mag(phi))().primitiveField()
/ h.primitiveField()
);
CoNum = 0.5*gMax(sumPhi/mesh.V().field())*runTime.deltaTValue();
meanCoNum =
0.5*(gSum(sumPhi)/gSum(mesh.V().field()))*runTime.deltaTValue();
// Gravity wave Courant number
waveCoNum = 0.25*gMax
(
fvc::surfaceSum
(
fvc::interpolate(sqrt(h))*mesh.magSf()
)().primitiveField()/mesh.V().field()
)*sqrt(magg).value()*runTime.deltaTValue();
}
Info<< "Courant number mean: " << meanCoNum
<< " max: " << CoNum << endl;
Info<< "Gravity wave Courant number max: " << waveCoNum
<< endl;
// ************************************************************************* //
Markdown is supported
0% or .
You are about to add 0 people to the discussion. Proceed with caution.
Finish editing this message first!
Please register or to comment