driftFluxFoam: New version of settlingFoam including MULES and MRF/fvOptions support

This commit is contained in:
Henry
2014-02-19 16:33:51 +00:00
committed by Andrew Heather
parent cecf40bc81
commit 9fbfc7da57
67 changed files with 4515 additions and 0 deletions

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driftFluxFoam.C
EXE = $(FOAM_APPBIN)/driftFluxFoam

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EXE_INC = \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/meshTools/lnInclude \
-I$(LIB_SRC)/sampling/lnInclude \
-I$(LIB_SRC)/fvOptions/lnInclude
EXE_LIBS = \
-lfiniteVolume \
-lmeshTools \
-lsampling \
-lfvOptions

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// Solve the Momentum equation
fvVectorMatrix UEqn
(
fvm::ddt(rho, U)
+ fvm::div(rhoPhi, U)
+ fvc::div
(
(alpha/(scalar(1.001) - alpha))*((rhoc*rhod)/rho)*Vdj*Vdj,
"div(phiVdj,Vdj)"
)
- fvm::laplacian(muEff, U)
- fvc::div(muEff*dev2(T(fvc::grad(U))))
==
fvOptions(rho, U)
);
UEqn.relax();
fvOptions.constrain(UEqn);
if (pimple.momentumPredictor())
{
solve
(
UEqn
==
fvc::reconstruct
(
(
- ghf*fvc::snGrad(rho)
- fvc::snGrad(p_rgh)
)*mesh.magSf()
)
);
fvOptions.correct(U);
}

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const dictionary& alphaControls = mesh.solverDict(alpha.name());
label nAlphaCorr(readLabel(alphaControls.lookup("nAlphaCorr")));
label nAlphaSubCycles(readLabel(alphaControls.lookup("nAlphaSubCycles")));

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{
word alphaScheme("div(phi,alpha)");
word alpharScheme("div(phirb,alpha)");
for (int aCorr=0; aCorr<nAlphaCorr; aCorr++)
{
phiAlpha =
(
fvc::flux
(
phi,
alpha,
alphaScheme
)
+ fvc::flux
(
phir,
alpha,
alpharScheme
)
);
MULES::explicitSolve(alpha, phi, phiAlpha, 1, 0);
}
Info<< "Phase-1 volume fraction = "
<< alpha.weightedAverage(mesh.Vsc()).value()
<< " Min(alpha) = " << min(alpha).value()
<< " Max(alpha) = " << max(alpha).value()
<< endl;
}

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{
surfaceScalarField phiAlpha
(
IOobject
(
"phiAlpha",
runTime.timeName(),
mesh
),
mesh,
dimensionedScalar("0", phi.dimensions(), 0)
);
surfaceScalarField phir
(
rhoc*(mesh.Sf() & fvc::interpolate(Vdj/rho))
);
if (nAlphaSubCycles > 1)
{
dimensionedScalar totalDeltaT = runTime.deltaT();
surfaceScalarField phiAlphaSum
(
IOobject
(
"phiAlphaSum",
runTime.timeName(),
mesh
),
mesh,
dimensionedScalar("0", phi.dimensions(), 0)
);
for
(
subCycle<volScalarField> alphaSubCycle(alpha, nAlphaSubCycles);
!(++alphaSubCycle).end();
)
{
#include "alphaEqn.H"
phiAlphaSum += (runTime.deltaT()/totalDeltaT)*phiAlpha;
}
phiAlpha = phiAlphaSum;
}
else
{
#include "alphaEqn.H"
}
// Apply the diffusion term separately to allow implicit solution
// and boundedness of the explicit advection
{
fvScalarMatrix alphaEqn
(
fvm::ddt(alpha) - fvc::ddt(alpha)
- fvm::laplacian(mut/rho, alpha)
);
alphaEqn.solve();
phiAlpha += alphaEqn.flux();
}
Info<< "Phase-1 volume fraction = "
<< alpha.weightedAverage(mesh.Vsc()).value()
<< " Min(alpha) = " << min(alpha).value()
<< " Max(alpha) = " << max(alpha).value()
<< endl;
rhoPhi = phiAlpha*(rhod - rhoc) + phi*rhoc;
rho == alpha*rhod + (scalar(1) - alpha)*rhoc;
}

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if (VdjModel == "general")
{
Vdj = V0*
(
exp(-a*max(alpha - alphaMin, scalar(0)))
- exp(-a1*max(alpha - alphaMin, scalar(0)))
);
}
else if (VdjModel == "simple")
{
Vdj = V0*pow(10.0, -a*max(alpha, scalar(0)));
}
else
{
FatalErrorIn(args.executable())
<< "Unknown VdjModel : " << VdjModel
<< abort(FatalError);
}
Vdj.correctBoundaryConditions();

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{
mul = muc +
plasticViscosity
(
plasticViscosityCoeff,
plasticViscosityExponent,
alpha
);
if (BinghamPlastic)
{
volScalarField tauy = yieldStress
(
yieldStressCoeff,
yieldStressExponent,
yieldStressOffset,
alpha
);
mul =
tauy/
(
mag(fvc::grad(U))
+ 1.0e-4*
(
tauy
+ dimensionedScalar
(
"deltaTauy",
tauy.dimensions(),
1.0e-15
)
)/mul
)
+ mul;
}
mul = min(mul, muMax);
}

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Info<< "Reading field p_rgh\n" << endl;
volScalarField p_rgh
(
IOobject
(
"p_rgh",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
Info<< "Reading field alpha\n" << endl;
volScalarField alpha
(
IOobject
(
"alpha",
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"
Info<< "Reading transportProperties\n" << endl;
IOdictionary transportProperties
(
IOobject
(
"transportProperties",
runTime.constant(),
mesh,
IOobject::MUST_READ_IF_MODIFIED,
IOobject::NO_WRITE
)
);
dimensionedScalar rhoc(transportProperties.lookup("rhoc"));
dimensionedScalar rhod(transportProperties.lookup("rhod"));
dimensionedScalar muc(transportProperties.lookup("muc"));
dimensionedScalar muMax(transportProperties.lookup("muMax"));
dimensionedScalar plasticViscosityCoeff
(
transportProperties.lookup("plasticViscosityCoeff")
);
dimensionedScalar plasticViscosityExponent
(
transportProperties.lookup("plasticViscosityExponent")
);
dimensionedScalar yieldStressCoeff
(
transportProperties.lookup("yieldStressCoeff")
);
dimensionedScalar yieldStressExponent
(
transportProperties.lookup("yieldStressExponent")
);
dimensionedScalar yieldStressOffset
(
transportProperties.lookup("yieldStressOffset")
);
Switch BinghamPlastic(transportProperties.lookup("BinghamPlastic"));
volScalarField rho
(
IOobject
(
"rho",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::NO_WRITE
),
alpha*rhod + (scalar(1) - alpha)*rhoc
);
rho.oldTime();
// Mass flux
surfaceScalarField rhoPhi
(
IOobject
(
"rhoPhi",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::NO_WRITE
),
fvc::interpolate(rho)*phi
);
Info<< "Calculating field mul\n" << endl;
volScalarField mul
(
IOobject
(
"mul",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::AUTO_WRITE
),
muc
+ plasticViscosity
(
plasticViscosityCoeff,
plasticViscosityExponent,
alpha
)
);
Info<< "Initialising field Vdj\n" << endl;
volVectorField Vdj
(
IOobject
(
"Vdj",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::AUTO_WRITE
),
mesh,
dimensionedVector("0.0", U.dimensions(), vector::zero),
U.boundaryField().types()
);
Info<< "Selecting Drift-Flux model " << endl;
const word VdjModel(transportProperties.lookup("VdjModel"));
Info<< tab << VdjModel << " selected\n" << endl;
const dictionary& VdjModelCoeffs
(
transportProperties.subDict(VdjModel + "Coeffs")
);
dimensionedVector V0(VdjModelCoeffs.lookup("V0"));
dimensionedScalar a(VdjModelCoeffs.lookup("a"));
dimensionedScalar a1(VdjModelCoeffs.lookup("a1"));
dimensionedScalar alphaMin(VdjModelCoeffs.lookup("alphaMin"));
IOdictionary RASProperties
(
IOobject
(
"RASProperties",
runTime.constant(),
mesh,
IOobject::MUST_READ_IF_MODIFIED,
IOobject::NO_WRITE
)
);
Switch turbulence(RASProperties.lookup("turbulence"));
dictionary kEpsilonDict(RASProperties.subDictPtr("kEpsilonCoeffs"));
dimensionedScalar Cmu
(
dimensionedScalar::lookupOrAddToDict
(
"Cmu",
kEpsilonDict,
0.09
)
);
dimensionedScalar C1
(
dimensionedScalar::lookupOrAddToDict
(
"C1",
kEpsilonDict,
1.44
)
);
dimensionedScalar C2
(
dimensionedScalar::lookupOrAddToDict
(
"C2",
kEpsilonDict,
1.92
)
);
dimensionedScalar C3
(
dimensionedScalar::lookupOrAddToDict
(
"C3",
kEpsilonDict,
0.85
)
);
dimensionedScalar sigmak
(
dimensionedScalar::lookupOrAddToDict
(
"sigmak",
kEpsilonDict,
1.0
)
);
dimensionedScalar sigmaEps
(
dimensionedScalar::lookupOrAddToDict
(
"sigmaEps",
kEpsilonDict,
1.3
)
);
dictionary wallFunctionDict(RASProperties.subDictPtr("wallFunctionCoeffs"));
dimensionedScalar kappa
(
dimensionedScalar::lookupOrAddToDict
(
"kappa",
wallFunctionDict,
0.41
)
);
dimensionedScalar E
(
dimensionedScalar::lookupOrAddToDict
(
"E",
wallFunctionDict,
9.8
)
);
if (RASProperties.lookupOrDefault("printCoeffs", false))
{
Info<< "kEpsilonCoeffs" << kEpsilonDict << nl
<< "wallFunctionCoeffs" << wallFunctionDict << endl;
}
nearWallDist y(mesh);
Info<< "Reading field k\n" << endl;
volScalarField k
(
IOobject
(
"k",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
Info<< "Reading field epsilon\n" << endl;
volScalarField epsilon
(
IOobject
(
"epsilon",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
Info<< "Calculating field mut\n" << endl;
volScalarField mut
(
IOobject
(
"mut",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::AUTO_WRITE
),
Cmu*rho*sqr(k)/epsilon
);
Info<< "Calculating field muEff\n" << endl;
volScalarField muEff
(
IOobject
(
"muEff",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::AUTO_WRITE
),
mut + mul
);
Info<< "Calculating field (g.h)f\n" << endl;
volScalarField gh("gh", g & mesh.C());
surfaceScalarField ghf("gh", g & mesh.Cf());
volScalarField p
(
IOobject
(
"p",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::AUTO_WRITE
),
p_rgh + rho*gh
);
label pRefCell = 0;
scalar pRefValue = 0.0;
setRefCell
(
p,
p_rgh,
mesh.solutionDict().subDict("PIMPLE"),
pRefCell,
pRefValue
);
if (p_rgh.needReference())
{
p += dimensionedScalar
(
"p",
p.dimensions(),
pRefValue - getRefCellValue(p, pRefCell)
);
p_rgh = p - rho*gh;
}

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/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2014 OpenFOAM Foundation
\\/ 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 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
driftFluxFoam
Description
Solver for 2 incompressible fluids using the mixture approach with the
drift-flux approximation for relative motion of the phases.
Used for simulating the settling of the dispersed phase and other similar
separation problems.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "CMULES.H"
#include "subCycle.H"
#include "nearWallDist.H"
#include "wallFvPatch.H"
#include "bound.H"
#include "Switch.H"
#include "plasticViscosity.H"
#include "yieldStress.H"
#include "pimpleControl.H"
#include "fvIOoptionList.H"
#include "fixedFluxPressureFvPatchScalarField.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
#include "setRootCase.H"
#include "createTime.H"
#include "createMesh.H"
#include "readGravitationalAcceleration.H"
#include "createFields.H"
#include "createFvOptions.H"
#include "initContinuityErrs.H"
pimpleControl pimple(mesh);
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while (runTime.run())
{
#include "readTimeControls.H"
#include "CourantNo.H"
#include "setDeltaT.H"
runTime++;
Info<< "Time = " << runTime.timeName() << nl << endl;
// --- Pressure-velocity PIMPLE corrector loop
while (pimple.loop())
{
#include "alphaControls.H"
#include "calcVdj.H"
#include "alphaEqnSubCycle.H"
#include "correctViscosity.H"
#include "UEqn.H"
// --- Pressure corrector loop
while (pimple.correct())
{
#include "pEqn.H"
}
if (pimple.turbCorr())
{
#include "kEpsilon.H"
}
}
runTime.write();
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< nl << endl;
}
Info<< "End\n" << endl;
return 0;
}
// ************************************************************************* //

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if (turbulence)
{
if (mesh.changing())
{
y.correct();
}
dimensionedScalar k0("k0", k.dimensions(), 0);
dimensionedScalar kMin("kMin", k.dimensions(), SMALL);
dimensionedScalar epsilon0("epsilon0", epsilon.dimensions(), 0);
dimensionedScalar epsilonMin("epsilonMin", epsilon.dimensions(), SMALL);
volScalarField divU(fvc::div(rhoPhi/fvc::interpolate(rho)));
tmp<volTensorField> tgradU = fvc::grad(U);
volScalarField G(mut*(tgradU() && dev(twoSymm(tgradU()))));
tgradU.clear();
volScalarField Gcoef
(
Cmu*k/sigmak*(g & fvc::grad(rho))/(epsilon + epsilonMin)
);
#include "wallFunctions.H"
// Dissipation equation
fvScalarMatrix epsEqn
(
fvm::ddt(rho, epsilon)
+ fvm::div(rhoPhi, epsilon)
- fvm::laplacian
(
mut/sigmaEps + muc, epsilon,
"laplacian(DepsilonEff,epsilon)"
)
==
C1*G*epsilon/(k + kMin)
- fvm::SuSp(C1*(1.0 - C3)*Gcoef + (2.0/3.0*C1)*rho*divU, epsilon)
- fvm::Sp(C2*rho*epsilon/(k + kMin), epsilon)
);
#include "wallDissipation.H"
epsEqn.relax();
epsEqn.solve();
bound(epsilon, epsilon0);
// Turbulent kinetic energy equation
fvScalarMatrix kEqn
(
fvm::ddt(rho, k)
+ fvm::div(rhoPhi, k)
- fvm::laplacian
(
mut/sigmak + muc, k,
"laplacian(DkEff,k)"
)
==
G
- fvm::SuSp(Gcoef + 2.0/3.0*rho*divU, k)
- fvm::Sp(rho*epsilon/(k + kMin), k)
);
kEqn.relax();
kEqn.solve();
bound(k, k0);
//- Re-calculate viscosity
mut = rho*Cmu*sqr(k)/(epsilon + epsilonMin);
#include "wallViscosity.H"
}
muEff = mut + mul;

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{
volScalarField rAU("rAU", 1.0/UEqn.A());
surfaceScalarField rAUf("rAUf", fvc::interpolate(rAU));
volVectorField HbyA("HbyA", U);
HbyA = rAU*UEqn.H();
surfaceScalarField phiHbyA
(
"phiHbyA",
(fvc::interpolate(HbyA) & mesh.Sf())
+ fvc::interpolate(rho*rAU)*fvc::ddtCorr(U, phi)
);
adjustPhi(phiHbyA, U, p_rgh);
fvOptions.makeRelative(phiHbyA);
surfaceScalarField phig
(
(
- ghf*fvc::snGrad(rho)
)*rAUf*mesh.magSf()
);
phiHbyA += phig;
// Update the fixedFluxPressure BCs to ensure flux consistency
setSnGrad<fixedFluxPressureFvPatchScalarField>
(
p_rgh.boundaryField(),
(
phiHbyA.boundaryField()
- fvOptions.relative(mesh.Sf().boundaryField() & U.boundaryField())
)/(mesh.magSf().boundaryField()*rAUf.boundaryField())
);
while (pimple.correctNonOrthogonal())
{
fvScalarMatrix p_rghEqn
(
fvm::laplacian(rAUf, p_rgh) == fvc::div(phiHbyA)
);
p_rghEqn.setReference(pRefCell, getRefCellValue(p_rgh, pRefCell));
p_rghEqn.solve(mesh.solver(p_rgh.select(pimple.finalInnerIter())));
if (pimple.finalNonOrthogonalIter())
{
phi = phiHbyA - p_rghEqn.flux();
p_rgh.relax();
U = HbyA + rAU*fvc::reconstruct((phig - p_rghEqn.flux())/rAUf);
U.correctBoundaryConditions();
fvOptions.correct(U);
}
}
#include "continuityErrs.H"
p == p_rgh + rho*gh;
if (p_rgh.needReference())
{
p += dimensionedScalar
(
"p",
p.dimensions(),
pRefValue - getRefCellValue(p, pRefCell)
);
p_rgh = p - rho*gh;
}
}

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volScalarField plasticViscosity
(
const dimensionedScalar& plasticViscosityCoeff,
const dimensionedScalar& plasticViscosityExponent,
const volScalarField& Alpha
)
{
tmp<volScalarField> tfld
(
plasticViscosityCoeff*
(
pow
(
10.0,
plasticViscosityExponent*Alpha + SMALL
) - scalar(1)
)
);
return tfld();
}

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/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 2011-2014 OpenFOAM Foundation
\\/ 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 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
wallDissipation
Description
Set wall dissipation in the epsilon matrix
\*---------------------------------------------------------------------------*/
{
const fvPatchList& patches = mesh.boundary();
forAll(patches, patchi)
{
const fvPatch& p = patches[patchi];
if (isA<wallFvPatch>(p))
{
epsEqn.setValues
(
p.faceCells(),
epsilon.boundaryField()[patchi].patchInternalField()
);
}
}
}
// ************************************************************************* //

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{
labelList cellBoundaryFaceCount(epsilon.size(), 0);
const scalar Cmu25 = ::pow(Cmu.value(), 0.25);
const scalar Cmu75 = ::pow(Cmu.value(), 0.75);
const scalar kappa_ = kappa.value();
const scalar muc_ = muc.value();
const fvPatchList& patches = mesh.boundary();
//- Initialise the near-wall P field to zero
forAll(patches, patchi)
{
const fvPatch& curPatch = patches[patchi];
if (isA<wallFvPatch>(curPatch))
{
forAll(curPatch, facei)
{
label faceCelli = curPatch.faceCells()[facei];
epsilon[faceCelli] = 0.0;
G[faceCelli] = 0.0;
}
}
}
//- Accumulate the wall face contributions to epsilon and G
// Increment cellBoundaryFaceCount for each face for averaging
forAll(patches, patchi)
{
const fvPatch& curPatch = patches[patchi];
if (isA<wallFvPatch>(curPatch))
{
const scalarField& mutw = mut.boundaryField()[patchi];
scalarField magFaceGradU
(
mag(U.boundaryField()[patchi].snGrad())
);
forAll(curPatch, facei)
{
label faceCelli = curPatch.faceCells()[facei];
// For corner cells (with two boundary or more faces),
// epsilon and G in the near-wall cell are calculated
// as an average
cellBoundaryFaceCount[faceCelli]++;
epsilon[faceCelli] +=
Cmu75*::pow(k[faceCelli], 1.5)
/(kappa_*y[patchi][facei]);
G[faceCelli] +=
(mutw[facei] + muc_)
*magFaceGradU[facei]
*Cmu25*::sqrt(k[faceCelli])
/(kappa_*y[patchi][facei]);
}
}
}
// perform the averaging
forAll(patches, patchi)
{
const fvPatch& curPatch = patches[patchi];
if (isA<wallFvPatch>(curPatch))
{
forAll(curPatch, facei)
{
label faceCelli = curPatch.faceCells()[facei];
epsilon[faceCelli] /= cellBoundaryFaceCount[faceCelli];
G[faceCelli] /= cellBoundaryFaceCount[faceCelli];
cellBoundaryFaceCount[faceCelli] = 1;
}
}
}
}

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{
const scalar Cmu25 = ::pow(Cmu.value(), 0.25);
const scalar kappa_ = kappa.value();
const scalar E_ = E.value();
const scalar muc_ = muc.value();
const scalar nuc_ = muc_/rhoc.value();
const fvPatchList& patches = mesh.boundary();
forAll(patches, patchi)
{
const fvPatch& curPatch = patches[patchi];
if (isA<wallFvPatch>(curPatch))
{
scalarField& mutw = mut.boundaryField()[patchi];
forAll(curPatch, facei)
{
label faceCelli = curPatch.faceCells()[facei];
scalar yPlus =
Cmu25*y[patchi][facei]*::sqrt(k[faceCelli])
/nuc_;
if (yPlus > 11.6)
{
mutw[facei] =
muc_*(yPlus*kappa_/::log(E_*yPlus) - 1);
}
else
{
mutw[facei] = 0.0;
}
}
}
}
}

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volScalarField yieldStress
(
const dimensionedScalar& yieldStressCoeff,
const dimensionedScalar& yieldStressExponent,
const dimensionedScalar& yieldStressOffset,
const volScalarField& alpha
)
{
tmp<volScalarField> tfld
(
yieldStressCoeff*
(
pow
(
10.0,
yieldStressExponent*(max(alpha, scalar(0)) + yieldStressOffset)
)
- pow
(
10.0,
yieldStressExponent*yieldStressOffset
)
)
);
return tfld();
}

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0.0191 0 0);
boundaryField
{
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type pressureInletOutletVelocity;
value uniform (0 0 0);
}
bottomWall
{
type fixedValue;
value uniform (0 0 0);
}
endWall
{
type fixedValue;
value uniform (0 0 0);
}
top
{
type slip;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,56 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object alpha;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0.001;
boundaryField
{
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
}
bottomWall
{
type zeroGradient;
}
endWall
{
type zeroGradient;
}
top
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,56 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 1.50919e-06;
boundaryField
{
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
}
bottomWall
{
type zeroGradient;
}
endWall
{
type zeroGradient;
}
top
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,56 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0.00015;
boundaryField
{
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
}
bottomWall
{
type zeroGradient;
}
endWall
{
type zeroGradient;
}
top
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,59 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p_rgh;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type fixedFluxPressure;
value uniform 0;
}
outlet
{
type fixedValue;
value uniform 0;
}
bottomWall
{
type fixedFluxPressure;
value uniform 0;
}
endWall
{
type fixedFluxPressure;
value uniform 0;
}
top
{
type fixedFluxPressure;
value uniform 0;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel kEpsilon;
turbulence on;
printCoeffs on;
// ************************************************************************* //

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@ -0,0 +1,22 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class uniformDimensionedVectorField;
location "constant";
object g;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -2 0 0 0 0];
value (0 -9.81 0);
// ************************************************************************* //

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@ -0,0 +1,105 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1;
vertices
(
(0 0 -0.1)
(8.65 0 -0.1)
(8.65 0.1 -0.1)
(0 0.1 -0.1)
(8.65 1 -0.1)
(0 1 -0.1)
(0 0 0.1)
(8.65 0 0.1)
(8.65 0.1 0.1)
(0 0.1 0.1)
(8.65 1 0.1)
(0 1 0.1)
);
blocks
(
hex (0 1 2 3 6 7 8 9) (200 4 1) simpleGrading (1 1 1)
hex (3 2 4 5 9 8 10 11) (200 36 1) simpleGrading (1 1 1)
);
edges
(
);
boundary
(
inlet
{
type patch;
faces
(
(0 6 9 3)
(3 9 11 5)
);
}
outlet
{
type patch;
faces
(
(1 2 8 7)
);
}
bottomWall
{
type wall;
faces
(
(0 1 7 6)
);
}
endWall
{
type wall;
faces
(
(2 4 10 8)
);
}
top
{
type patch;
faces
(
(5 11 10 4)
);
}
frontAndBack
{
type empty;
faces
(
(0 3 2 1)
(6 7 8 9)
(3 5 4 2)
(9 8 10 11)
);
}
);
mergePatchPairs
(
);
// ************************************************************************* //

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@ -0,0 +1,61 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format binary;
class polyBoundaryMesh;
location "constant/polyMesh";
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
6
(
inlet
{
type patch;
nFaces 40;
startFace 15760;
}
outlet
{
type patch;
nFaces 4;
startFace 15800;
}
bottomWall
{
type wall;
inGroups 1(wall);
nFaces 200;
startFace 15804;
}
endWall
{
type wall;
inGroups 1(wall);
nFaces 36;
startFace 16004;
}
top
{
type patch;
nFaces 200;
startFace 16040;
}
frontAndBack
{
type empty;
inGroups 1(empty);
nFaces 16000;
startFace 16240;
}
)
// ************************************************************************* //

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@ -0,0 +1,57 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
muc muc [ 1 -1 -1 0 0 0 0 ] 0.00178;
plasticViscosityCoeff plasticViscosityCoeff [ 1 -1 -1 0 0 0 0 ] 0.00023143;
plasticViscosityExponent plasticViscosityExponent [ 0 0 0 0 0 0 0 ] 179.26;
BinghamPlastic on;
yieldStressCoeff yieldStressCoeff [ 1 -1 -2 0 0 0 0 ] 0.00042189;
yieldStressExponent yieldStressExponent [ 0 0 0 0 0 0 0 ] 1050.8;
yieldStressOffset yieldStressOffset [ 0 0 0 0 0 0 0 ] 0;
muMax muMax [ 1 -1 -1 0 0 0 0 ] 10.0;
rhoc rhoc [ 1 -3 0 0 0 0 0 ] 996;
rhod rhod [ 1 -3 0 0 0 0 0 ] 1996;
VdjModel simple;
simpleCoeffs
{
V0 V0 [ 0 1 -1 0 0 0 0 ] ( 0 -0.002198 0 );
a a [ 0 0 0 0 0 0 0 ] 285.84;
a1 a1 [ 0 0 0 0 0 0 0 ] 0;
alphaMin alphaMin [ 0 0 0 0 0 0 0 ] 0;
}
generalCoeffs
{
V0 V0 [ 0 1 -1 0 0 0 0 ] ( 0 -0.0018 0 );
a a [ 0 0 0 0 0 0 0 ] 1e-05;
a1 a1 [ 0 0 0 0 0 0 0 ] 0.1;
alphaMin alphaMin [ 0 0 0 0 0 0 0 ] 2e-05;
}
// ************************************************************************* //

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@ -0,0 +1,54 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application driftFluxFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 6400;
deltaT 0.1;
writeControl adjustableRunTime;
writeInterval 50;
purgeWrite 0;
writeFormat binary;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep on;
maxCo 1;
maxDeltaT 1;
// ************************************************************************* //

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@ -0,0 +1,65 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(rhoPhi,U) Gauss linearUpwind grad(U);
div(phiVdj,Vdj) Gauss linear;
div(phi,alpha) Gauss vanLeer;
div(phirb,alpha) Gauss vanLeer;
div(rhoPhi,k) Gauss limitedLinear 1;
div(rhoPhi,epsilon) Gauss limitedLinear 1;
div((muEff*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p_rgh;
alpha;
}
// ************************************************************************* //

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@ -0,0 +1,86 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"alpha.*"
{
nAlphaCorr 1;
nAlphaSubCycles 4;
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-6;
relTol 0;
minIter 1;
}
p_rgh
{
solver GAMG;
tolerance 1e-7;
relTol 0.01;
smoother GaussSeidel;
cacheAgglomeration true;
nCellsInCoarsestLevel 20;
agglomerator faceAreaPair;
mergeLevels 1;
}
p_rghFinal
{
$p_rgh;
relTol 0;
}
"(U|k|epsilon)"
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-7;
relTol 0.1;
minIter 1;
}
"(U|k|epsilon)Final"
{
$k;
relTol 0;
}
}
PIMPLE
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
}
relaxationFactors
{
fields
{
}
equations
{
"U.*" 1;
"k.*" 1;
"epsilon.*" 1;
}
}
// ************************************************************************* //

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@ -0,0 +1,45 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
rotor
{
type fixedValue;
value uniform (0 0 0);
}
stator
{
type fixedValue;
value uniform (0 0 0);
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,44 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object alpha;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0.001;
boundaryField
{
rotor
{
type zeroGradient;
}
stator
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,44 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 7e-3;
boundaryField
{
rotor
{
type zeroGradient;
}
stator
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,44 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0.01;
boundaryField
{
rotor
{
type zeroGradient;
}
stator
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,44 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p_rgh;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
rotor
{
type zeroGradient;
}
stator
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,12 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
application=`getApplication`
runApplication ./makeMesh
runApplication $application
# ----------------------------------------------------------------- end-of-file

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@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel kEpsilon;
turbulence on;
printCoeffs on;
// ************************************************************************* //

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@ -0,0 +1,21 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class uniformDimensionedVectorField;
location "constant";
object g;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -2 0 0 0 0];
value (0 0 0);
// ************************************************************************* //

View File

@ -0,0 +1,818 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
`format' ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// General macros to create 2D/extruded-2D meshes
changecom(//)changequote([,])
define(calc, [esyscmd(perl -e 'print ($1)')])
define(VCOUNT, 0)
define(vlabel, [[// ]Vertex $1 = VCOUNT define($1, VCOUNT)define([VCOUNT], incr(VCOUNT))])
define(pi, 3.14159265)
define(hex2D, hex ($1b $2b $3b $4b $1t $2t $3t $4t))
define(quad2D, ($1b $2b $2t $1t))
define(frontQuad, ($1t $2t $3t $4t))
define(backQuad, ($1b $4b $3b $2b))
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.1;
// Hub radius
define(r, 0.2)
// Impeller-tip radius
define(rb, 0.5)
// Baffle-tip radius
define(Rb, 0.7)
// Tank radius
define(R, 1)
// MRF region radius
define(ri, calc(0.5*(rb + Rb)))
// Thickness of 2D slab
define(z, 0.1)
// Base z
define(Zb, 0)
// Top z
define(Zt, calc(Zb + z))
// Number of cells radially between hub and impeller tip
define(Nr, 12)
// Number of cells radially in each of the two regions between
// impeller and baffle tips
define(Ni, 4)
// Number of cells radially between baffle tip and tank
define(NR, 12)
// Number of cells azimuthally in each of the 8 blocks
define(Na, 12)
// Number of cells in the thickness of the slab
define(Nz, 1)
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
define(vert, (x$1$2 y$1$2 $3))
define(evert, (ex$1$2 ey$1$2 $3))
define(a0, 0)
define(a1, -45)
define(a2, -90)
define(a3, -135)
define(a4, 180)
define(a5, 135)
define(a6, 90)
define(a7, 45)
define(ea0, -22.5)
define(ea1, -67.5)
define(ea2, -112.5)
define(ea3, -157.5)
define(ea4, 157.5)
define(ea5, 112.5)
define(ea6, 67.5)
define(ea7, 22.5)
define(ca0, calc(cos((pi/180)*a0)))
define(ca1, calc(cos((pi/180)*a1)))
define(ca2, calc(cos((pi/180)*a2)))
define(ca3, calc(cos((pi/180)*a3)))
define(ca4, calc(cos((pi/180)*a4)))
define(ca5, calc(cos((pi/180)*a5)))
define(ca6, calc(cos((pi/180)*a6)))
define(ca7, calc(cos((pi/180)*a7)))
define(sa0, calc(sin((pi/180)*a0)))
define(sa1, calc(sin((pi/180)*a1)))
define(sa2, calc(sin((pi/180)*a2)))
define(sa3, calc(sin((pi/180)*a3)))
define(sa4, calc(sin((pi/180)*a4)))
define(sa5, calc(sin((pi/180)*a5)))
define(sa6, calc(sin((pi/180)*a6)))
define(sa7, calc(sin((pi/180)*a7)))
define(cea0, calc(cos((pi/180)*ea0)))
define(cea1, calc(cos((pi/180)*ea1)))
define(cea2, calc(cos((pi/180)*ea2)))
define(cea3, calc(cos((pi/180)*ea3)))
define(cea4, calc(cos((pi/180)*ea4)))
define(cea5, calc(cos((pi/180)*ea5)))
define(cea6, calc(cos((pi/180)*ea6)))
define(cea7, calc(cos((pi/180)*ea7)))
define(sea0, calc(sin((pi/180)*ea0)))
define(sea1, calc(sin((pi/180)*ea1)))
define(sea2, calc(sin((pi/180)*ea2)))
define(sea3, calc(sin((pi/180)*ea3)))
define(sea4, calc(sin((pi/180)*ea4)))
define(sea5, calc(sin((pi/180)*ea5)))
define(sea6, calc(sin((pi/180)*ea6)))
define(sea7, calc(sin((pi/180)*ea7)))
define(x00, calc(r*ca0))
define(x01, calc(r*ca1))
define(x02, calc(r*ca2))
define(x03, calc(r*ca3))
define(x04, calc(r*ca4))
define(x05, calc(r*ca5))
define(x06, calc(r*ca6))
define(x07, calc(r*ca7))
define(x10, calc(rb*ca0))
define(x11, calc(rb*ca1))
define(x12, calc(rb*ca2))
define(x13, calc(rb*ca3))
define(x14, calc(rb*ca4))
define(x15, calc(rb*ca5))
define(x16, calc(rb*ca6))
define(x17, calc(rb*ca7))
define(x20, calc(ri*ca0))
define(x21, calc(ri*ca1))
define(x22, calc(ri*ca2))
define(x23, calc(ri*ca3))
define(x24, calc(ri*ca4))
define(x25, calc(ri*ca5))
define(x26, calc(ri*ca6))
define(x27, calc(ri*ca7))
define(x30, calc(Rb*ca0))
define(x31, calc(Rb*ca1))
define(x32, calc(Rb*ca2))
define(x33, calc(Rb*ca3))
define(x34, calc(Rb*ca4))
define(x35, calc(Rb*ca5))
define(x36, calc(Rb*ca6))
define(x37, calc(Rb*ca7))
define(x40, calc(R*ca0))
define(x41, calc(R*ca1))
define(x42, calc(R*ca2))
define(x43, calc(R*ca3))
define(x44, calc(R*ca4))
define(x45, calc(R*ca5))
define(x46, calc(R*ca6))
define(x47, calc(R*ca7))
define(y00, calc(r*sa0))
define(y01, calc(r*sa1))
define(y02, calc(r*sa2))
define(y03, calc(r*sa3))
define(y04, calc(r*sa4))
define(y05, calc(r*sa5))
define(y06, calc(r*sa6))
define(y07, calc(r*sa7))
define(y10, calc(rb*sa0))
define(y11, calc(rb*sa1))
define(y12, calc(rb*sa2))
define(y13, calc(rb*sa3))
define(y14, calc(rb*sa4))
define(y15, calc(rb*sa5))
define(y16, calc(rb*sa6))
define(y17, calc(rb*sa7))
define(y20, calc(ri*sa0))
define(y21, calc(ri*sa1))
define(y22, calc(ri*sa2))
define(y23, calc(ri*sa3))
define(y24, calc(ri*sa4))
define(y25, calc(ri*sa5))
define(y26, calc(ri*sa6))
define(y27, calc(ri*sa7))
define(y30, calc(Rb*sa0))
define(y31, calc(Rb*sa1))
define(y32, calc(Rb*sa2))
define(y33, calc(Rb*sa3))
define(y34, calc(Rb*sa4))
define(y35, calc(Rb*sa5))
define(y36, calc(Rb*sa6))
define(y37, calc(Rb*sa7))
define(y40, calc(R*sa0))
define(y41, calc(R*sa1))
define(y42, calc(R*sa2))
define(y43, calc(R*sa3))
define(y44, calc(R*sa4))
define(y45, calc(R*sa5))
define(y46, calc(R*sa6))
define(y47, calc(R*sa7))
define(ex00, calc(r*cea0))
define(ex01, calc(r*cea1))
define(ex02, calc(r*cea2))
define(ex03, calc(r*cea3))
define(ex04, calc(r*cea4))
define(ex05, calc(r*cea5))
define(ex06, calc(r*cea6))
define(ex07, calc(r*cea7))
define(ex10, calc(rb*cea0))
define(ex11, calc(rb*cea1))
define(ex12, calc(rb*cea2))
define(ex13, calc(rb*cea3))
define(ex14, calc(rb*cea4))
define(ex15, calc(rb*cea5))
define(ex16, calc(rb*cea6))
define(ex17, calc(rb*cea7))
define(ex20, calc(ri*cea0))
define(ex21, calc(ri*cea1))
define(ex22, calc(ri*cea2))
define(ex23, calc(ri*cea3))
define(ex24, calc(ri*cea4))
define(ex25, calc(ri*cea5))
define(ex26, calc(ri*cea6))
define(ex27, calc(ri*cea7))
define(ex30, calc(Rb*cea0))
define(ex31, calc(Rb*cea1))
define(ex32, calc(Rb*cea2))
define(ex33, calc(Rb*cea3))
define(ex34, calc(Rb*cea4))
define(ex35, calc(Rb*cea5))
define(ex36, calc(Rb*cea6))
define(ex37, calc(Rb*cea7))
define(ex40, calc(R*cea0))
define(ex41, calc(R*cea1))
define(ex42, calc(R*cea2))
define(ex43, calc(R*cea3))
define(ex44, calc(R*cea4))
define(ex45, calc(R*cea5))
define(ex46, calc(R*cea6))
define(ex47, calc(R*cea7))
define(ey00, calc(r*sea0))
define(ey01, calc(r*sea1))
define(ey02, calc(r*sea2))
define(ey03, calc(r*sea3))
define(ey04, calc(r*sea4))
define(ey05, calc(r*sea5))
define(ey06, calc(r*sea6))
define(ey07, calc(r*sea7))
define(ey10, calc(rb*sea0))
define(ey11, calc(rb*sea1))
define(ey12, calc(rb*sea2))
define(ey13, calc(rb*sea3))
define(ey14, calc(rb*sea4))
define(ey15, calc(rb*sea5))
define(ey16, calc(rb*sea6))
define(ey17, calc(rb*sea7))
define(ey20, calc(ri*sea0))
define(ey21, calc(ri*sea1))
define(ey22, calc(ri*sea2))
define(ey23, calc(ri*sea3))
define(ey24, calc(ri*sea4))
define(ey25, calc(ri*sea5))
define(ey26, calc(ri*sea6))
define(ey27, calc(ri*sea7))
define(ey30, calc(Rb*sea0))
define(ey31, calc(Rb*sea1))
define(ey32, calc(Rb*sea2))
define(ey33, calc(Rb*sea3))
define(ey34, calc(Rb*sea4))
define(ey35, calc(Rb*sea5))
define(ey36, calc(Rb*sea6))
define(ey37, calc(Rb*sea7))
define(ey40, calc(R*sea0))
define(ey41, calc(R*sea1))
define(ey42, calc(R*sea2))
define(ey43, calc(R*sea3))
define(ey44, calc(R*sea4))
define(ey45, calc(R*sea5))
define(ey46, calc(R*sea6))
define(ey47, calc(R*sea7))
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
vertices
(
vert(0, 0, Zb) vlabel(r0b)
vert(0, 0, Zb) vlabel(r0sb)
vert(0, 1, Zb) vlabel(r1b)
vert(0, 2, Zb) vlabel(r2b)
vert(0, 2, Zb) vlabel(r2sb)
vert(0, 3, Zb) vlabel(r3b)
vert(0, 4, Zb) vlabel(r4b)
vert(0, 4, Zb) vlabel(r4sb)
vert(0, 5, Zb) vlabel(r5b)
vert(0, 6, Zb) vlabel(r6b)
vert(0, 6, Zb) vlabel(r6sb)
vert(0, 7, Zb) vlabel(r7b)
vert(1, 0, Zb) vlabel(rb0b)
vert(1, 1, Zb) vlabel(rb1b)
vert(1, 2, Zb) vlabel(rb2b)
vert(1, 3, Zb) vlabel(rb3b)
vert(1, 4, Zb) vlabel(rb4b)
vert(1, 5, Zb) vlabel(rb5b)
vert(1, 6, Zb) vlabel(rb6b)
vert(1, 7, Zb) vlabel(rb7b)
vert(2, 0, Zb) vlabel(ri0b)
vert(2, 1, Zb) vlabel(ri1b)
vert(2, 2, Zb) vlabel(ri2b)
vert(2, 3, Zb) vlabel(ri3b)
vert(2, 4, Zb) vlabel(ri4b)
vert(2, 5, Zb) vlabel(ri5b)
vert(2, 6, Zb) vlabel(ri6b)
vert(2, 7, Zb) vlabel(ri7b)
vert(3, 0, Zb) vlabel(Rb0b)
vert(3, 1, Zb) vlabel(Rb1b)
vert(3, 2, Zb) vlabel(Rb2b)
vert(3, 3, Zb) vlabel(Rb3b)
vert(3, 4, Zb) vlabel(Rb4b)
vert(3, 5, Zb) vlabel(Rb5b)
vert(3, 6, Zb) vlabel(Rb6b)
vert(3, 7, Zb) vlabel(Rb7b)
vert(4, 0, Zb) vlabel(R0b)
vert(4, 1, Zb) vlabel(R1b)
vert(4, 1, Zb) vlabel(R1sb)
vert(4, 2, Zb) vlabel(R2b)
vert(4, 3, Zb) vlabel(R3b)
vert(4, 3, Zb) vlabel(R3sb)
vert(4, 4, Zb) vlabel(R4b)
vert(4, 5, Zb) vlabel(R5b)
vert(4, 5, Zb) vlabel(R5sb)
vert(4, 6, Zb) vlabel(R6b)
vert(4, 7, Zb) vlabel(R7b)
vert(4, 7, Zb) vlabel(R7sb)
vert(0, 0, Zt) vlabel(r0t)
vert(0, 0, Zt) vlabel(r0st)
vert(0, 1, Zt) vlabel(r1t)
vert(0, 2, Zt) vlabel(r2t)
vert(0, 2, Zt) vlabel(r2st)
vert(0, 3, Zt) vlabel(r3t)
vert(0, 4, Zt) vlabel(r4t)
vert(0, 4, Zt) vlabel(r4st)
vert(0, 5, Zt) vlabel(r5t)
vert(0, 6, Zt) vlabel(r6t)
vert(0, 6, Zt) vlabel(r6st)
vert(0, 7, Zt) vlabel(r7t)
vert(1, 0, Zt) vlabel(rb0t)
vert(1, 1, Zt) vlabel(rb1t)
vert(1, 2, Zt) vlabel(rb2t)
vert(1, 3, Zt) vlabel(rb3t)
vert(1, 4, Zt) vlabel(rb4t)
vert(1, 5, Zt) vlabel(rb5t)
vert(1, 6, Zt) vlabel(rb6t)
vert(1, 7, Zt) vlabel(rb7t)
vert(2, 0, Zt) vlabel(ri0t)
vert(2, 1, Zt) vlabel(ri1t)
vert(2, 2, Zt) vlabel(ri2t)
vert(2, 3, Zt) vlabel(ri3t)
vert(2, 4, Zt) vlabel(ri4t)
vert(2, 5, Zt) vlabel(ri5t)
vert(2, 6, Zt) vlabel(ri6t)
vert(2, 7, Zt) vlabel(ri7t)
vert(3, 0, Zt) vlabel(Rb0t)
vert(3, 1, Zt) vlabel(Rb1t)
vert(3, 2, Zt) vlabel(Rb2t)
vert(3, 3, Zt) vlabel(Rb3t)
vert(3, 4, Zt) vlabel(Rb4t)
vert(3, 5, Zt) vlabel(Rb5t)
vert(3, 6, Zt) vlabel(Rb6t)
vert(3, 7, Zt) vlabel(Rb7t)
vert(4, 0, Zt) vlabel(R0t)
vert(4, 1, Zt) vlabel(R1t)
vert(4, 1, Zt) vlabel(R1st)
vert(4, 2, Zt) vlabel(R2t)
vert(4, 3, Zt) vlabel(R3t)
vert(4, 3, Zt) vlabel(R3st)
vert(4, 4, Zt) vlabel(R4t)
vert(4, 5, Zt) vlabel(R5t)
vert(4, 5, Zt) vlabel(R5st)
vert(4, 6, Zt) vlabel(R6t)
vert(4, 7, Zt) vlabel(R7t)
vert(4, 7, Zt) vlabel(R7st)
);
blocks
(
// block0
hex2D(r0, r1, rb1, rb0)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block1
hex2D(r1, r2s, rb2, rb1)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block2
hex2D(r2, r3, rb3, rb2)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block3
hex2D(r3, r4s, rb4, rb3)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block4
hex2D(r4, r5, rb5, rb4)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block5
hex2D(r5, r6s, rb6, rb5)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block6
hex2D(r6, r7, rb7, rb6)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block7
hex2D(r7, r0s, rb0, rb7)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block0
hex2D(rb0, rb1, ri1, ri0)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block1
hex2D(rb1, rb2, ri2, ri1)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block2
hex2D(rb2, rb3, ri3, ri2)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block3
hex2D(rb3, rb4, ri4, ri3)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block4
hex2D(rb4, rb5, ri5, ri4)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block5
hex2D(rb5, rb6, ri6, ri5)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block6
hex2D(rb6, rb7, ri7, ri6)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block7
hex2D(rb7, rb0, ri0, ri7)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block0
hex2D(ri0, ri1, Rb1, Rb0)
(Na Ni Nz)
simpleGrading (1 1 1)
// block1
hex2D(ri1, ri2, Rb2, Rb1)
(Na Ni Nz)
simpleGrading (1 1 1)
// block2
hex2D(ri2, ri3, Rb3, Rb2)
(Na Ni Nz)
simpleGrading (1 1 1)
// block3
hex2D(ri3, ri4, Rb4, Rb3)
(Na Ni Nz)
simpleGrading (1 1 1)
// block4
hex2D(ri4, ri5, Rb5, Rb4)
(Na Ni Nz)
simpleGrading (1 1 1)
// block5
hex2D(ri5, ri6, Rb6, Rb5)
(Na Ni Nz)
simpleGrading (1 1 1)
// block6
hex2D(ri6, ri7, Rb7, Rb6)
(Na Ni Nz)
simpleGrading (1 1 1)
// block7
hex2D(ri7, ri0, Rb0, Rb7)
(Na Ni Nz)
simpleGrading (1 1 1)
// block0
hex2D(Rb0, Rb1, R1s, R0)
(Na NR Nz)
simpleGrading (1 1 1)
// block1
hex2D(Rb1, Rb2, R2, R1)
(Na NR Nz)
simpleGrading (1 1 1)
// block2
hex2D(Rb2, Rb3, R3s, R2)
(Na NR Nz)
simpleGrading (1 1 1)
// block3
hex2D(Rb3, Rb4, R4, R3)
(Na NR Nz)
simpleGrading (1 1 1)
// block4
hex2D(Rb4, Rb5, R5s, R4)
(Na NR Nz)
simpleGrading (1 1 1)
// block5
hex2D(Rb5, Rb6, R6, R5)
(Na NR Nz)
simpleGrading (1 1 1)
// block6
hex2D(Rb6, Rb7, R7s, R6)
(Na NR Nz)
simpleGrading (1 1 1)
// block7
hex2D(Rb7, Rb0, R0, R7)
(Na NR Nz)
simpleGrading (1 1 1)
);
edges
(
arc r0b r1b evert(0, 0, Zb)
arc r1b r2sb evert(0, 1, Zb)
arc r2b r3b evert(0, 2, Zb)
arc r3b r4sb evert(0, 3, Zb)
arc r4b r5b evert(0, 4, Zb)
arc r5b r6sb evert(0, 5, Zb)
arc r6b r7b evert(0, 6, Zb)
arc r7b r0sb evert(0, 7, Zb)
arc rb0b rb1b evert(1, 0, Zb)
arc rb1b rb2b evert(1, 1, Zb)
arc rb2b rb3b evert(1, 2, Zb)
arc rb3b rb4b evert(1, 3, Zb)
arc rb4b rb5b evert(1, 4, Zb)
arc rb5b rb6b evert(1, 5, Zb)
arc rb6b rb7b evert(1, 6, Zb)
arc rb7b rb0b evert(1, 7, Zb)
arc ri0b ri1b evert(2, 0, Zb)
arc ri1b ri2b evert(2, 1, Zb)
arc ri2b ri3b evert(2, 2, Zb)
arc ri3b ri4b evert(2, 3, Zb)
arc ri4b ri5b evert(2, 4, Zb)
arc ri5b ri6b evert(2, 5, Zb)
arc ri6b ri7b evert(2, 6, Zb)
arc ri7b ri0b evert(2, 7, Zb)
arc Rb0b Rb1b evert(3, 0, Zb)
arc Rb1b Rb2b evert(3, 1, Zb)
arc Rb2b Rb3b evert(3, 2, Zb)
arc Rb3b Rb4b evert(3, 3, Zb)
arc Rb4b Rb5b evert(3, 4, Zb)
arc Rb5b Rb6b evert(3, 5, Zb)
arc Rb6b Rb7b evert(3, 6, Zb)
arc Rb7b Rb0b evert(3, 7, Zb)
arc R0b R1sb evert(4, 0, Zb)
arc R1b R2b evert(4, 1, Zb)
arc R2b R3sb evert(4, 2, Zb)
arc R3b R4b evert(4, 3, Zb)
arc R4b R5sb evert(4, 4, Zb)
arc R5b R6b evert(4, 5, Zb)
arc R6b R7sb evert(4, 6, Zb)
arc R7b R0b evert(4, 7, Zb)
arc r0t r1t evert(0, 0, Zt)
arc r1t r2st evert(0, 1, Zt)
arc r2t r3t evert(0, 2, Zt)
arc r3t r4st evert(0, 3, Zt)
arc r4t r5t evert(0, 4, Zt)
arc r5t r6st evert(0, 5, Zt)
arc r6t r7t evert(0, 6, Zt)
arc r7t r0st evert(0, 7, Zt)
arc rb0t rb1t evert(1, 0, Zt)
arc rb1t rb2t evert(1, 1, Zt)
arc rb2t rb3t evert(1, 2, Zt)
arc rb3t rb4t evert(1, 3, Zt)
arc rb4t rb5t evert(1, 4, Zt)
arc rb5t rb6t evert(1, 5, Zt)
arc rb6t rb7t evert(1, 6, Zt)
arc rb7t rb0t evert(1, 7, Zt)
arc ri0t ri1t evert(2, 0, Zt)
arc ri1t ri2t evert(2, 1, Zt)
arc ri2t ri3t evert(2, 2, Zt)
arc ri3t ri4t evert(2, 3, Zt)
arc ri4t ri5t evert(2, 4, Zt)
arc ri5t ri6t evert(2, 5, Zt)
arc ri6t ri7t evert(2, 6, Zt)
arc ri7t ri0t evert(2, 7, Zt)
arc Rb0t Rb1t evert(3, 0, Zt)
arc Rb1t Rb2t evert(3, 1, Zt)
arc Rb2t Rb3t evert(3, 2, Zt)
arc Rb3t Rb4t evert(3, 3, Zt)
arc Rb4t Rb5t evert(3, 4, Zt)
arc Rb5t Rb6t evert(3, 5, Zt)
arc Rb6t Rb7t evert(3, 6, Zt)
arc Rb7t Rb0t evert(3, 7, Zt)
arc R0t R1st evert(4, 0, Zt)
arc R1t R2t evert(4, 1, Zt)
arc R2t R3st evert(4, 2, Zt)
arc R3t R4t evert(4, 3, Zt)
arc R4t R5st evert(4, 4, Zt)
arc R5t R6t evert(4, 5, Zt)
arc R6t R7st evert(4, 6, Zt)
arc R7t R0t evert(4, 7, Zt)
);
patches
(
wall rotor
(
quad2D(r0, r1)
quad2D(r1, r2s)
quad2D(r2, r3)
quad2D(r3, r4s)
quad2D(r4, r5)
quad2D(r5, r6s)
quad2D(r6, r7)
quad2D(r7, r0s)
quad2D(r0, rb0)
quad2D(r0s, rb0)
quad2D(r2, rb2)
quad2D(r2s, rb2)
quad2D(r4, rb4)
quad2D(r4s, rb4)
quad2D(r6, rb6)
quad2D(r6s, rb6)
)
wall stator
(
quad2D(R0, R1s)
quad2D(R1, R2)
quad2D(R2, R3s)
quad2D(R3, R4)
quad2D(R4, R5s)
quad2D(R5, R6)
quad2D(R6, R7s)
quad2D(R7, R0)
quad2D(R1, Rb1)
quad2D(R1s, Rb1)
quad2D(R3, Rb3)
quad2D(R3s, Rb3)
quad2D(R5, Rb5)
quad2D(R5s, Rb5)
quad2D(R7, Rb7)
quad2D(R7s, Rb7)
)
empty front
(
frontQuad(r0, r1, rb1, rb0)
frontQuad(r1, r2s, rb2, rb1)
frontQuad(r2, r3, rb3, rb2)
frontQuad(r3, r4s, rb4, rb3)
frontQuad(r4, r5, rb5, rb4)
frontQuad(r5, r6s, rb6, rb5)
frontQuad(r6, r7, rb7, rb6)
frontQuad(r7, r0s, rb0, rb7)
frontQuad(rb0, rb1, ri1, ri0)
frontQuad(rb1, rb2, ri2, ri1)
frontQuad(rb2, rb3, ri3, ri2)
frontQuad(rb3, rb4, ri4, ri3)
frontQuad(rb4, rb5, ri5, ri4)
frontQuad(rb5, rb6, ri6, ri5)
frontQuad(rb6, rb7, ri7, ri6)
frontQuad(rb7, rb0, ri0, ri7)
frontQuad(ri0, ri1, Rb1, Rb0)
frontQuad(ri1, ri2, Rb2, Rb1)
frontQuad(ri2, ri3, Rb3, Rb2)
frontQuad(ri3, ri4, Rb4, Rb3)
frontQuad(ri4, ri5, Rb5, Rb4)
frontQuad(ri5, ri6, Rb6, Rb5)
frontQuad(ri6, ri7, Rb7, Rb6)
frontQuad(ri7, ri0, Rb0, Rb7)
frontQuad(Rb0, Rb1, R1s, R0)
frontQuad(Rb1, Rb2, R2, R1)
frontQuad(Rb2, Rb3, R3s, R2)
frontQuad(Rb3, Rb4, R4, R3)
frontQuad(Rb4, Rb5, R5s, R4)
frontQuad(Rb5, Rb6, R6, R5)
frontQuad(Rb6, Rb7, R7s, R6)
frontQuad(Rb7, Rb0, R0, R7)
)
empty back
(
backQuad(r0, r1, rb1, rb0)
backQuad(r1, r2s, rb2, rb1)
backQuad(r2, r3, rb3, rb2)
backQuad(r3, r4s, rb4, rb3)
backQuad(r4, r5, rb5, rb4)
backQuad(r5, r6s, rb6, rb5)
backQuad(r6, r7, rb7, rb6)
backQuad(r7, r0s, rb0, rb7)
backQuad(rb0, rb1, ri1, ri0)
backQuad(rb1, rb2, ri2, ri1)
backQuad(rb2, rb3, ri3, ri2)
backQuad(rb3, rb4, ri4, ri3)
backQuad(rb4, rb5, ri5, ri4)
backQuad(rb5, rb6, ri6, ri5)
backQuad(rb6, rb7, ri7, ri6)
backQuad(rb7, rb0, ri0, ri7)
backQuad(ri0, ri1, Rb1, Rb0)
backQuad(ri1, ri2, Rb2, Rb1)
backQuad(ri2, ri3, Rb3, Rb2)
backQuad(ri3, ri4, Rb4, Rb3)
backQuad(ri4, ri5, Rb5, Rb4)
backQuad(ri5, ri6, Rb6, Rb5)
backQuad(ri6, ri7, Rb7, Rb6)
backQuad(ri7, ri0, Rb0, Rb7)
backQuad(Rb0, Rb1, R1s, R0)
backQuad(Rb1, Rb2, R2, R1)
backQuad(Rb2, Rb3, R3s, R2)
backQuad(Rb3, Rb4, R4, R3)
backQuad(Rb4, Rb5, R5s, R4)
backQuad(Rb5, Rb6, R6, R5)
backQuad(Rb6, Rb7, R7s, R6)
backQuad(Rb7, Rb0, R0, R7)
)
);
// ************************************************************************* //

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@ -0,0 +1,50 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.x |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
location "constant/polyMesh";
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
4
(
rotor
{
type wall;
inGroups 1(wall);
nFaces 192;
startFace 5952;
}
stator
{
type wall;
inGroups 1(wall);
nFaces 192;
startFace 6144;
}
front
{
type empty;
inGroups 1(empty);
nFaces 3072;
startFace 6336;
}
back
{
type empty;
inGroups 1(empty);
nFaces 3072;
startFace 9408;
}
)
// ************************************************************************* //

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@ -0,0 +1,57 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
muc muc [ 1 -1 -1 0 0 0 0 ] 0.00178;
plasticViscosityCoeff plasticViscosityCoeff [ 1 -1 -1 0 0 0 0 ] 0.00023143;
plasticViscosityExponent plasticViscosityExponent [ 0 0 0 0 0 0 0 ] 179.26;
BinghamPlastic on;
yieldStressCoeff yieldStressCoeff [ 1 -1 -2 0 0 0 0 ] 0.00042189;
yieldStressExponent yieldStressExponent [ 0 0 0 0 0 0 0 ] 1050.8;
yieldStressOffset yieldStressOffset [ 0 0 0 0 0 0 0 ] 0;
muMax muMax [ 1 -1 -1 0 0 0 0 ] 10.0;
rhoc rhoc [ 1 -3 0 0 0 0 0 ] 996;
rhod rhod [ 1 -3 0 0 0 0 0 ] 1996;
VdjModel simple;
simpleCoeffs
{
V0 V0 [ 0 1 -1 0 0 0 0 ] ( 0 -0.002198 0 );
a a [ 0 0 0 0 0 0 0 ] 285.84;
a1 a1 [ 0 0 0 0 0 0 0 ] 0;
alphaMin alphaMin [ 0 0 0 0 0 0 0 ] 0;
}
generalCoeffs
{
V0 V0 [ 0 1 -1 0 0 0 0 ] ( 0 -0.0018 0 );
a a [ 0 0 0 0 0 0 0 ] 1e-05;
a1 a1 [ 0 0 0 0 0 0 0 ] 0.1;
alphaMin alphaMin [ 0 0 0 0 0 0 0 ] 2e-05;
}
// ************************************************************************* //

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@ -0,0 +1,6 @@
#!/bin/sh
m4 < constant/polyMesh/blockMeshDict.m4 > constant/polyMesh/blockMeshDict
blockMesh
topoSet
setsToZones -noFlipMap

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@ -0,0 +1,56 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application driftFluxFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 10;
deltaT 1e-3;
writeControl adjustableRunTime;
writeInterval 0.25;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep yes;
maxCo 0.5;
maxAlphaCo 0.5;
maxDeltaT 0.05;
// ************************************************************************* //

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@ -0,0 +1,37 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvOptions;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
MRF1
{
type MRFSource;
active yes;
selectionMode cellZone;
cellZone rotor;
MRFSourceCoeffs
{
// Fixed patches (by default they 'move' with the MRF zone)
nonRotatingPatches ();
origin (0 0 0);
axis (0 0 1);
omega constant 6.2831853;
}
}
// ************************************************************************* //

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@ -0,0 +1,65 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(rhoPhi,U) Gauss linearUpwind grad(U);
div(phiVdj,Vdj) Gauss linear;
div(phi,alpha) Gauss vanLeer;
div(phirb,alpha) Gauss vanLeer;
div(rhoPhi,k) Gauss limitedLinear 1;
div(rhoPhi,epsilon) Gauss limitedLinear 1;
div((muEff*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p_rgh ;
alpha ;
}
// ************************************************************************* //

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@ -0,0 +1,83 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"alpha.*"
{
nAlphaCorr 1;
nAlphaSubCycles 3;
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-6;
relTol 0;
}
"rho.*"
{
solver PCG;
preconditioner DIC;
tolerance 1e-8;
relTol 0;
}
p_rgh
{
solver GAMG;
tolerance 1e-6;
relTol 0.05;
smoother GaussSeidel;
cacheAgglomeration true;
nCellsInCoarsestLevel 20;
agglomerator faceAreaPair;
mergeLevels 1;
}
p_rghFinal
{
$p_rgh;
relTol 0;
}
"(U|k|epsilon)"
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-6;
relTol 0.1;
}
"(U|k|epsilon)Final"
{
$k;
relTol 0;
}
}
PIMPLE
{
momentumPredictor yes;
nCorrectors 3;
nNonOrthogonalCorrectors 0;
pRefCell 0;
pRefValue 0;
}
// ************************************************************************* //

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@ -0,0 +1,36 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object setFieldsDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
defaultFieldValues
(
volScalarFieldValue alpha.water 0
);
regions
(
boxToCell
{
box (0 0 -1) (1 1 1);
fieldValues
(
volScalarFieldValue alpha.water 1
);
}
);
// ************************************************************************* //

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@ -0,0 +1,32 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object topoSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
actions
(
{
name rotor;
type cellSet;
action new;
source zoneToCell;
sourceInfo
{
name rotor;
}
}
);
// ************************************************************************* //

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@ -0,0 +1,144 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
SYMP3
{
type slip;
}
INLE1
{
type fixedValue;
value uniform (0.1315 0 0);
}
OUTL9
{
type fixedValue;
value uniform (0 0.0177 0);
}
OUTL10
{
type fixedValue;
value uniform (0 0.0177 0);
}
OUTL11
{
type fixedValue;
value uniform (0 0.0177 0);
}
OUTL12
{
type fixedValue;
value uniform (0 0.0177 0);
}
WALL6
{
type translatingWallVelocity;
U (-0.003 0 0);
value uniform (-0.003 0 0);
}
WALL8
{
type fixedValue;
value uniform (0 0 0);
}
WALL61
{
type fixedValue;
value uniform (0 0 0);
}
WALL62
{
type fixedValue;
value uniform (0 0 0);
}
WALL63
{
type fixedValue;
value uniform (0 0 0);
}
WALL64
{
type fixedValue;
value uniform (0 0 0);
}
WALL65
{
type fixedValue;
value uniform (0 0 0);
}
WALL66
{
type fixedValue;
value uniform (0 0 0);
}
WALL67
{
type fixedValue;
value uniform (0 0 0);
}
WALL68
{
type fixedValue;
value uniform (0 0 0);
}
WALL69
{
type fixedValue;
value uniform (0 0 0);
}
WALL7
{
type fixedValue;
value uniform (0 0 0);
}
WALL70
{
type fixedValue;
value uniform (0 0 0);
}
OUTL15
{
type inletOutlet;
inletValue uniform (0 0 0);
}
}
// ************************************************************************* //

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@ -0,0 +1,126 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object alpha;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
SYMP3
{
type zeroGradient;
}
INLE1
{
type fixedValue;
value uniform 0.002;
}
OUTL9
{
type zeroGradient;
}
OUTL10
{
type zeroGradient;
}
OUTL11
{
type zeroGradient;
}
OUTL12
{
type zeroGradient;
}
WALL6
{
type zeroGradient;
}
WALL8
{
type zeroGradient;
}
WALL61
{
type zeroGradient;
}
WALL62
{
type zeroGradient;
}
WALL63
{
type zeroGradient;
}
WALL64
{
type zeroGradient;
}
WALL65
{
type zeroGradient;
}
WALL66
{
type zeroGradient;
}
WALL67
{
type zeroGradient;
}
WALL68
{
type zeroGradient;
}
WALL69
{
type zeroGradient;
}
WALL7
{
type zeroGradient;
}
WALL70
{
type zeroGradient;
}
OUTL15
{
type inletOutlet;
inletValue uniform 0;
}
}
// ************************************************************************* //

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@ -0,0 +1,126 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 1.973e-07;
boundaryField
{
SYMP3
{
type zeroGradient;
}
INLE1
{
type fixedValue;
value uniform 1.973e-07;
}
OUTL9
{
type zeroGradient;
}
OUTL10
{
type zeroGradient;
}
OUTL11
{
type zeroGradient;
}
OUTL12
{
type zeroGradient;
}
WALL6
{
type zeroGradient;
}
WALL8
{
type zeroGradient;
}
WALL61
{
type zeroGradient;
}
WALL62
{
type zeroGradient;
}
WALL63
{
type zeroGradient;
}
WALL64
{
type zeroGradient;
}
WALL65
{
type zeroGradient;
}
WALL66
{
type zeroGradient;
}
WALL67
{
type zeroGradient;
}
WALL68
{
type zeroGradient;
}
WALL69
{
type zeroGradient;
}
WALL7
{
type zeroGradient;
}
WALL70
{
type zeroGradient;
}
OUTL15
{
type inletOutlet;
inletValue uniform 1.973e-07;
}
}
// ************************************************************************* //

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@ -0,0 +1,126 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0.000259;
boundaryField
{
SYMP3
{
type zeroGradient;
}
INLE1
{
type fixedValue;
value uniform 0.000259;
}
OUTL9
{
type zeroGradient;
}
OUTL10
{
type zeroGradient;
}
OUTL11
{
type zeroGradient;
}
OUTL12
{
type zeroGradient;
}
WALL6
{
type zeroGradient;
}
WALL8
{
type zeroGradient;
}
WALL61
{
type zeroGradient;
}
WALL62
{
type zeroGradient;
}
WALL63
{
type zeroGradient;
}
WALL64
{
type zeroGradient;
}
WALL65
{
type zeroGradient;
}
WALL66
{
type zeroGradient;
}
WALL67
{
type zeroGradient;
}
WALL68
{
type zeroGradient;
}
WALL69
{
type zeroGradient;
}
WALL7
{
type zeroGradient;
}
WALL70
{
type zeroGradient;
}
OUTL15
{
type inletOutlet;
inletValue uniform 0.000259;
}
}
// ************************************************************************* //

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@ -0,0 +1,144 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p_rgh;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
SYMP3
{
type fixedFluxPressure;
value uniform 0;
}
INLE1
{
type fixedFluxPressure;
value uniform 0;
}
OUTL9
{
type fixedFluxPressure;
value uniform 0;
}
OUTL10
{
type fixedFluxPressure;
value uniform 0;
}
OUTL11
{
type fixedFluxPressure;
value uniform 0;
}
OUTL12
{
type fixedFluxPressure;
value uniform 0;
}
WALL6
{
type fixedFluxPressure;
value uniform 0;
}
WALL8
{
type fixedFluxPressure;
value uniform 0;
}
WALL61
{
type fixedFluxPressure;
value uniform 0;
}
WALL62
{
type fixedFluxPressure;
value uniform 0;
}
WALL63
{
type fixedFluxPressure;
value uniform 0;
}
WALL64
{
type fixedFluxPressure;
value uniform 0;
}
WALL65
{
type fixedFluxPressure;
value uniform 0;
}
WALL66
{
type fixedFluxPressure;
value uniform 0;
}
WALL67
{
type fixedFluxPressure;
value uniform 0;
}
WALL68
{
type fixedFluxPressure;
value uniform 0;
}
WALL69
{
type fixedFluxPressure;
value uniform 0;
}
WALL7
{
type fixedFluxPressure;
value uniform 0;
}
WALL70
{
type fixedFluxPressure;
value uniform 0;
}
OUTL15
{
type fixedValue;
value uniform 0;
}
}
// ************************************************************************* //

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@ -0,0 +1,9 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Clean time directories only
rm -rf *[1-9]*
rm -f log.* 2>/dev/null
# ----------------------------------------------------------------- end-of-file

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@ -0,0 +1,11 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
application=`getApplication`
runApplication $application
# ----------------------------------------------------------------- end-of-file

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@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel kEpsilon;
turbulence on;
printCoeffs on;
// ************************************************************************* //

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@ -0,0 +1,22 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class uniformDimensionedVectorField;
location "constant";
object g;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -2 0 0 0 0];
value ( 0 -9.81 0 );
// ************************************************************************* //

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@ -0,0 +1,160 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
(
SYMP3
{
type patch;
startFace 53708;
nFaces 3191;
}
INLE1
{
type patch;
startFace 56899;
nFaces 45;
}
OUTL9
{
type patch;
startFace 56944;
nFaces 11;
}
OUTL10
{
type patch;
startFace 56955;
nFaces 11;
}
OUTL11
{
type patch;
startFace 56966;
nFaces 11;
}
OUTL12
{
type patch;
startFace 56977;
nFaces 11;
}
WALL6
{
type wall;
startFace 56988;
nFaces 1474;
}
WALL8
{
type wall;
startFace 58462;
nFaces 1640;
}
WALL61
{
type wall;
startFace 60102;
nFaces 44;
}
WALL62
{
type wall;
startFace 60146;
nFaces 78;
}
WALL63
{
type wall;
startFace 60224;
nFaces 255;
}
WALL64
{
type wall;
startFace 60479;
nFaces 157;
}
WALL65
{
type wall;
startFace 60636;
nFaces 35;
}
WALL66
{
type wall;
startFace 60671;
nFaces 60;
}
WALL67
{
type wall;
startFace 60731;
nFaces 55;
}
WALL68
{
type wall;
startFace 60786;
nFaces 116;
}
WALL69
{
type wall;
startFace 60902;
nFaces 24;
}
WALL7
{
type wall;
startFace 60926;
nFaces 121;
}
WALL70
{
type wall;
startFace 61047;
nFaces 182;
}
OUTL15
{
type patch;
startFace 61229;
nFaces 14;
}
)
// ************************************************************************* //

View File

@ -0,0 +1,57 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
muc muc [ 1 -1 -1 0 0 0 0 ] 0.00178;
plasticViscosityCoeff plasticViscosityCoeff [ 1 -1 -1 0 0 0 0 ] 0.00023143;
plasticViscosityExponent plasticViscosityExponent [ 0 0 0 0 0 0 0 ] 0.17926;
BinghamPlastic on;
yieldStressCoeff yieldStressCoeff [ 1 -1 -2 0 0 0 0 ] 5.5469e-07;
yieldStressExponent yieldStressExponent [ 0 0 0 0 0 0 0 ] 95.25;
yieldStressOffset yieldStressOffset [ 0 0 0 0 0 0 0 ] 0;
muMax muMax [ 1 -1 -1 0 0 0 0 ] 10.0;
rhoc rhoc [ 1 -3 0 0 0 0 0 ] 1000;
rhod rhod [ 1 -3 0 0 0 0 0 ] 1042;
VdjModel simple;
simpleCoeffs
{
V0 V0 [ 0 1 -1 0 0 0 0 ] ( 0 -0.002198 0 );
a a [ 0 0 0 0 0 0 0 ] 8.84;
a1 a1 [ 0 0 0 0 0 0 0 ] 0;
alphaMin alphaMin [ 0 0 0 0 0 0 0 ] 0;
}
generalCoeffs
{
V0 V0 [ 0 1 -1 0 0 0 0 ] ( 0 -0.0018 0 );
a a [ 0 0 0 0 0 0 0 ] 1e-05;
a1 a1 [ 0 0 0 0 0 0 0 ] 0.1;
alphaMin alphaMin [ 0 0 0 0 0 0 0 ] 2e-05;
}
// ************************************************************************* //

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@ -0,0 +1,48 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application driftFluxFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 8000;
deltaT 0.1;
writeControl runTime;
writeInterval 50;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression compressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
// ************************************************************************* //

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@ -0,0 +1,65 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(rhoPhi,U) Gauss linearUpwind grad(U);
div(phiVdj,Vdj) Gauss linear;
div(phi,alpha) Gauss vanLeer;
div(phirb,alpha) Gauss vanLeer;
div(rhoPhi,k) Gauss limitedLinear 1;
div(rhoPhi,epsilon) Gauss limitedLinear 1;
div((muEff*dev2(T(grad(U))))) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p_rgh;
alpha;
}
// ************************************************************************* //

View File

@ -0,0 +1,84 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"alpha.*"
{
nAlphaCorr 1;
nAlphaSubCycles 4;
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-6;
relTol 0;
minIter 1;
}
p_rgh
{
solver GAMG;
tolerance 1e-7;
relTol 0.01;
smoother GaussSeidel;
cacheAgglomeration true;
nCellsInCoarsestLevel 20;
agglomerator faceAreaPair;
mergeLevels 1;
}
p_rghFinal
{
$p_rgh;
relTol 0;
}
"(U|k|epsilon)"
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-7;
relTol 0.1;
minIter 1;
}
"(U|k|epsilon)Final"
{
$k;
relTol 0;
}
}
PIMPLE
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
}
relaxationFactors
{
fields
{
}
equations
{
".*" 1;
}
}
// ************************************************************************* //