Merge branch 'master' of /home/dm4/OpenFOAM/OpenFOAM-dev

This commit is contained in:
mattijs
2012-01-03 11:08:31 +00:00
60 changed files with 2764 additions and 1417 deletions

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@ -109,6 +109,9 @@ int main(int argc, char *argv[])
surfaceScalarField phiv_pos(U_pos & mesh.Sf());
surfaceScalarField phiv_neg(U_neg & mesh.Sf());
fvc::makeRelative(phiv_pos, U);
fvc::makeRelative(phiv_neg, U);
volScalarField c(sqrt(thermo.Cp()/thermo.Cv()*rPsi));
surfaceScalarField cSf_pos
(
@ -161,17 +164,9 @@ int main(int argc, char *argv[])
Info<< "Time = " << runTime.timeName() << nl << endl;
mesh.movePoints(motionPtr->newPoints());
phiv_pos = U_pos & mesh.Sf();
phiv_neg = U_neg & mesh.Sf();
fvc::makeRelative(phiv_pos, U);
fvc::makeRelative(phiv_neg, U);
phiv_neg -= mesh.phi();
phiv_pos *= a_pos;
phiv_neg *= a_neg;
aphiv_pos = phiv_pos - aSf;
aphiv_neg = phiv_neg + aSf;
surfaceScalarField phi("phi", aphiv_pos*rho_pos + aphiv_neg*rho_neg);
phi = aphiv_pos*rho_pos + aphiv_neg*rho_neg;
Info<< phi.boundaryField()[0] << endl;
surfaceVectorField phiUp
(
@ -183,6 +178,7 @@ int main(int argc, char *argv[])
(
aphiv_pos*(rho_pos*(e_pos + 0.5*magSqr(U_pos)) + p_pos)
+ aphiv_neg*(rho_neg*(e_neg + 0.5*magSqr(U_neg)) + p_neg)
+ mesh.phi()*(a_pos*p_pos + a_neg*p_neg)
+ aSf*p_pos - aSf*p_neg
);

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@ -0,0 +1,12 @@
{
solve
(
fvm::ddt(rho, e)
+ fvm::div(phi, e)
- fvm::laplacian(turbulence->alphaEff(), e)
==
- p*fvc::div(phi/fvc::interpolate(rho) + mesh.phi())
);
thermo.correct();
}

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@ -76,34 +76,23 @@ Foam::tmp<Foam::volScalarField> Foam::dragModels::GidaspowErgunWenYu::K
volScalarField bp(pow(beta, -2.65));
volScalarField Re(max(Ur*d/phase2_.nu(), scalar(1.0e-3)));
volScalarField Cds(24.0*(1.0 + 0.15*pow(Re, 0.687))/Re);
forAll(Re, celli)
{
if (Re[celli] > 1000.0)
{
Cds[celli] = 0.44;
}
}
volScalarField Cds
(
neg(Re - 1000)*(24.0*(1.0 + 0.15*pow(Re, 0.687))/Re)
+ pos(Re - 1000)*0.44
);
// Wen and Yu (1966)
tmp<volScalarField> tKWenYu(0.75*Cds*phase2_.rho()*Ur*bp/d);
volScalarField& KWenYu = tKWenYu();
// Ergun
forAll (beta, cellj)
{
if (beta[cellj] <= 0.8)
{
KWenYu[cellj] =
150.0*alpha_[cellj]*phase2_.nu().value()*phase2_.rho().value()
/sqr(beta[cellj]*d[cellj])
+ 1.75*phase2_.rho().value()*Ur[cellj]
/(beta[cellj]*d[cellj]);
}
}
return tKWenYu;
return
(
pos(beta - 0.8)
*(0.75*Cds*phase2_.rho()*Ur*bp/d)
+ neg(beta - 0.8)
*(
150.0*alpha_*phase2_.nu()*phase2_.rho()/(sqr(beta*d))
+ 1.75*phase2_.rho()*Ur/(beta*d)
)
);
}

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@ -75,15 +75,11 @@ Foam::tmp<Foam::volScalarField> Foam::dragModels::GidaspowSchillerNaumann::K
volScalarField bp(pow(beta, -2.65));
volScalarField Re(max(beta*Ur*phase1_.d()/phase2_.nu(), scalar(1.0e-3)));
volScalarField Cds(24.0*(scalar(1) + 0.15*pow(Re, 0.687))/Re);
forAll(Re, celli)
{
if (Re[celli] > 1000.0)
{
Cds[celli] = 0.44;
}
}
volScalarField Cds
(
neg(Re - 1000)*(24.0*(1.0 + 0.15*pow(Re, 0.687))/Re)
+ pos(Re - 1000)*0.44
);
return 0.75*Cds*phase2_.rho()*Ur*bp/phase1_.d();
}

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@ -72,15 +72,11 @@ Foam::tmp<Foam::volScalarField> Foam::dragModels::SchillerNaumann::K
) const
{
volScalarField Re(max(Ur*phase1_.d()/phase2_.nu(), scalar(1.0e-3)));
volScalarField Cds(24.0*(scalar(1) + 0.15*pow(Re, 0.687))/Re);
forAll(Re, celli)
{
if (Re[celli] > 1000.0)
{
Cds[celli] = 0.44;
}
}
volScalarField Cds
(
neg(Re - 1000)*(24.0*(1.0 + 0.15*pow(Re, 0.687))/Re)
+ pos(Re - 1000)*0.44
);
return 0.75*Cds*phase2_.rho()*Ur/phase1_.d();
}

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@ -73,15 +73,11 @@ Foam::tmp<Foam::volScalarField> Foam::dragModels::SyamlalOBrien::K
{
volScalarField beta(max(scalar(1) - alpha_, scalar(1.0e-6)));
volScalarField A(pow(beta, 4.14));
volScalarField B(0.8*pow(beta, 1.28));
forAll (beta, celli)
{
if (beta[celli] > 0.85)
{
B[celli] = pow(beta[celli], 2.65);
}
}
volScalarField B
(
neg(beta - 0.85)*(0.8*pow(beta, 1.28))
+ pos(beta - 0.85)*(pow(beta, 2.65))
);
volScalarField Re(max(Ur*phase1_.d()/phase2_.nu(), scalar(1.0e-3)));

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@ -75,15 +75,11 @@ Foam::tmp<Foam::volScalarField> Foam::dragModels::WenYu::K
volScalarField bp(pow(beta, -2.65));
volScalarField Re(max(Ur*phase1_.d()/phase2_.nu(), scalar(1.0e-3)));
volScalarField Cds(24.0*(scalar(1) + 0.15*pow(Re, 0.687))/Re);
forAll(Re, celli)
{
if (Re[celli] > 1000.0)
{
Cds[celli] = 0.44;
}
}
volScalarField Cds
(
neg(Re - 1000)*(24.0*(1.0 + 0.15*pow(Re, 0.687))/Re)
+ pos(Re - 1000)*0.44
);
return 0.75*Cds*phase2_.rho()*Ur*bp/phase1_.d();
}

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@ -149,6 +149,8 @@ Foam::kineticTheoryModels::frictionalStressModels::Schaeffer::muf
}
}
muff.correctBoundaryConditions();
return tmuf;
}

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@ -21,16 +21,27 @@ forAllIter(PtrDictionary<phaseModel>, fluid.phases(), iter)
+ fvm::div(phase.phiAlpha(), U)
- fvm::Sp(fvc::ddt(alpha) + fvc::div(phase.phiAlpha()), U)
)
- fvm::laplacian(alpha*nuEff, U)
- fvc::div
(
alpha*(nuEff*dev(T(fvc::grad(U))) /*- ((2.0/3.0)*I)*k*/),
"div(Rc)"
)
==
- fvm::Sp(fluid.dragCoeff(phase, dragCoeffs())/phase.rho(), U)
//- (alpha*phase.rho())*fluid.lift(phase)
+ (alpha/phase.rho())*fluid.Svm(phase)
- fvm::laplacian(alpha*nuEff, U)
- fvc::div
(
alpha*(nuEff*dev(T(fvc::grad(U))) /*- ((2.0/3.0)*I)*k*/),
"div(Rc)"
)
==
- fvm::Sp(fluid.dragCoeff(phase, dragCoeffs())/phase.rho(), U)
//- (alpha*phase.rho())*fluid.lift(phase)
+ (alpha/phase.rho())*fluid.Svm(phase)
- fvm::Sp
(
slamDampCoeff
*max
(
mag(U.dimensionedInternalField()) - maxSlamVelocity,
dimensionedScalar("U0", dimVelocity, 0)
)
/pow(mesh.V(), 1.0/3.0),
U
)
)
);
mrfZones.addCoriolis(alpha, UEqns[phasei]);

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@ -53,6 +53,18 @@
phi += fvc::interpolate(alpha)*phase.phi();
}
scalar slamDampCoeff
(
fluid.lookupOrDefault<scalar>("slamDampCoeff", 1)
);
dimensionedScalar maxSlamVelocity
(
"maxSlamVelocity",
dimVelocity,
fluid.lookupOrDefault<scalar>("maxSlamVelocity", GREAT)
);
// dimensionedScalar pMin
// (
// "pMin",

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@ -1,80 +0,0 @@
volScalarField dragCoeff
(
IOobject
(
"dragCoeff",
runTime.timeName(),
mesh
),
mesh,
dimensionedScalar("dragCoeff", dimensionSet(1, -3, -1, 0, 0), 0)
);
volVectorField liftForce
(
IOobject
(
"liftForce",
runTime.timeName(),
mesh
),
mesh,
dimensionedVector("liftForce", dimensionSet(1, -2, -2, 0, 0), vector::zero)
);
volScalarField heatTransferCoeff
(
IOobject
(
"heatTransferCoeff",
runTime.timeName(),
mesh
),
mesh,
dimensionedScalar("heatTransferCoeff", dimensionSet(1, -1, -3, -1, 0), 0)
);
{
volVectorField Ur = U1 - U2;
volScalarField magUr = mag(Ur);
if (dispersedPhase == "1")
{
dragCoeff = drag1->K(magUr);
heatTransferCoeff = heatTransfer1->K(magUr);
}
else if (dispersedPhase == "2")
{
dragCoeff = drag2->K(magUr);
heatTransferCoeff = heatTransfer2->K(magUr);
}
else if (dispersedPhase == "both")
{
dragCoeff =
(
alpha2*drag1->K(magUr)
+ alpha1*drag2->K(magUr)
);
heatTransferCoeff =
(
alpha2*heatTransfer1->K(magUr)
+ alpha1*heatTransfer2->K(magUr)
);
}
else
{
FatalErrorIn(args.executable())
<< "dispersedPhase: " << dispersedPhase << " is incorrect"
<< exit(FatalError);
}
volScalarField alphaCoeff
(
(alpha1 + minInterfaceAlpha)*(alpha2 + minInterfaceAlpha)
);
dragCoeff *= alphaCoeff;
heatTransferCoeff *= alphaCoeff;
liftForce = Cl*(alpha1*rho1 + alpha2*rho2)*(Ur ^ fvc::curl(U));
}

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@ -75,34 +75,23 @@ Foam::tmp<Foam::volScalarField> Foam::dragModels::GidaspowErgunWenYu::K
volScalarField bp(pow(beta, -2.65));
volScalarField Re(max(Ur*d/phase2_.nu(), scalar(1.0e-3)));
volScalarField Cds(24.0*(1.0 + 0.15*pow(Re, 0.687))/Re);
forAll(Re, celli)
{
if (Re[celli] > 1000.0)
{
Cds[celli] = 0.44;
}
}
volScalarField Cds
(
neg(Re - 1000)*(24.0*(1.0 + 0.15*pow(Re, 0.687))/Re)
+ pos(Re - 1000)*0.44
);
// Wen and Yu (1966)
tmp<volScalarField> tKWenYu = 0.75*Cds*phase2_.rho()*Ur*bp/d;
volScalarField& KWenYu = tKWenYu();
// Ergun
forAll (beta, cellj)
{
if (beta[cellj] <= 0.8)
{
KWenYu[cellj] =
150.0*phase1_[cellj]*phase2_.nu().value()*phase2_.rho().value()
/sqr(beta[cellj]*d[cellj])
+ 1.75*phase2_.rho().value()*Ur[cellj]
/(beta[cellj]*d[cellj]);
}
}
return tKWenYu;
return
(
pos(beta - 0.8)
*(0.75*Cds*phase2_.rho()*Ur*bp/d)
+ neg(beta - 0.8)
*(
150.0*phase1_*phase2_.nu()*phase2_.rho()/(sqr(beta*d))
+ 1.75*phase2_.rho()*Ur/(beta*d)
)
);
}

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@ -74,15 +74,11 @@ Foam::tmp<Foam::volScalarField> Foam::dragModels::GidaspowSchillerNaumann::K
volScalarField bp(pow(beta, -2.65));
volScalarField Re(max(beta*Ur*phase1_.d()/phase2_.nu(), scalar(1.0e-3)));
volScalarField Cds(24.0*(scalar(1) + 0.15*pow(Re, 0.687))/Re);
forAll(Re, celli)
{
if (Re[celli] > 1000.0)
{
Cds[celli] = 0.44;
}
}
volScalarField Cds
(
neg(Re - 1000)*(24.0*(1.0 + 0.15*pow(Re, 0.687))/Re)
+ pos(Re - 1000)*0.44
);
return 0.75*Cds*phase2_.rho()*Ur*bp/phase1_.d();
}

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@ -71,15 +71,11 @@ Foam::tmp<Foam::volScalarField> Foam::dragModels::SchillerNaumann::K
) const
{
volScalarField Re(max(Ur*phase1_.d()/phase2_.nu(), scalar(1.0e-3)));
volScalarField Cds(24.0*(scalar(1) + 0.15*pow(Re, 0.687))/Re);
forAll(Re, celli)
{
if (Re[celli] > 1000.0)
{
Cds[celli] = 0.44;
}
}
volScalarField Cds
(
neg(Re - 1000)*(24.0*(1.0 + 0.15*pow(Re, 0.687))/Re)
+ pos(Re - 1000)*0.44
);
return 0.75*Cds*phase2_.rho()*Ur/phase1_.d();
}

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@ -72,15 +72,11 @@ Foam::tmp<Foam::volScalarField> Foam::dragModels::SyamlalOBrien::K
{
volScalarField beta(max(phase2_, scalar(1.0e-6)));
volScalarField A(pow(beta, 4.14));
volScalarField B(0.8*pow(beta, 1.28));
forAll (beta, celli)
{
if (beta[celli] > 0.85)
{
B[celli] = pow(beta[celli], 2.65);
}
}
volScalarField B
(
neg(beta - 0.85)*(0.8*pow(beta, 1.28))
+ pos(beta - 0.85)*(pow(beta, 2.65))
);
volScalarField Re(max(Ur*phase1_.d()/phase2_.nu(), scalar(1.0e-3)));

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@ -74,15 +74,11 @@ Foam::tmp<Foam::volScalarField> Foam::dragModels::WenYu::K
volScalarField bp(pow(beta, -2.65));
volScalarField Re(max(Ur*phase1_.d()/phase2_.nu(), scalar(1.0e-3)));
volScalarField Cds(24.0*(scalar(1) + 0.15*pow(Re, 0.687))/Re);
forAll(Re, celli)
{
if (Re[celli] > 1000.0)
{
Cds[celli] = 0.44;
}
}
volScalarField Cds
(
neg(Re - 1000)*(24.0*(1.0 + 0.15*pow(Re, 0.687))/Re)
+ pos(Re - 1000)*0.44
);
return 0.75*Cds*phase2_.rho()*Ur*bp/phase1_.d();
}

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@ -149,6 +149,8 @@ Foam::kineticTheoryModels::frictionalStressModels::Schaeffer::muf
}
}
muff.correctBoundaryConditions();
return tmuf;
}

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@ -82,7 +82,6 @@ int main(int argc, char *argv[])
rho = fluid.rho();
#include "zonePhaseVolumes.H"
//#include "interfacialCoeffs.H"
//#include "TEqns.H"
#include "UEqns.H"

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@ -37,8 +37,10 @@
U0s.set(phasei, new volVectorField(phase.U()));
phi0s.set(phasei, new surfaceScalarField(phase.phi()));
mrfZones.absoluteFlux(phi0s[phasei]);
phasei++;
}
surfaceScalarField phi0
@ -67,6 +69,8 @@
phase.U() = rAUs[phasei]*UEqns[phasei].H();
phase.phi().oldTime();
mrfZones.absoluteFlux(phase.phi().oldTime());
mrfZones.absoluteFlux(phase.phi());
phase.phi() =
(
@ -74,7 +78,8 @@
+ fvc::ddtPhiCorr(rAUs[phasei], alpha, phase.U(), phase.phi())
);
mrfZones.relativeFlux(phase.phi());
surfaceScalarField pphi0("pphi0", phase.phi());
mrfZones.relativeFlux(phase.phi().oldTime());
surfaceScalarField pphi0("pphi0", 1.0*phase.phi());
pphi0 += rAlphaAUfs[phasei]*(g & mesh.Sf());
multiphaseSystem::dragModelTable::const_iterator dmIter =
@ -196,7 +201,7 @@
p.relax();
mSfGradp = pEqnIncomp.flux()/Dp;
U = dimensionedVector("U", dimVelocity, vector::zero);
U = dimensionedVector("U", dimVelocity, vector::zero);
phasei = 0;
forAllIter(PtrDictionary<phaseModel>, fluid.phases(), iter)
@ -254,9 +259,17 @@
phasej++;
}
phase.U() +=
(1.0/phase.rho())
*rAUs[phasei]*(*dcIter())*U0s[phasej];
// phase.U() +=
// (1.0/phase.rho())*rAUs[phasei]*(*dcIter())
// *U0s[phasej];
phase.U() += fvc::reconstruct
(
fvc::interpolate
(
(1.0/phase.rho())*rAUs[phasei]*(*dcIter())
)*phi0s[phasej]
);
}
}

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@ -50,10 +50,14 @@ int main()
<< (t1 & t7 & t1.T()) << " " << transform(t1, t7) << endl;
symmTensor st1(1, 2, 3, 4, 5, 6);
symmTensor st2(7, 8, 9, 10, 11, 12);
Info<< "Check symmetric transformation "
<< transform(t1, st1) << endl;
Info<< "Check for dot product of symmetric tensors "
<< (st1 & st2) << endl;
vector v1(1, 2, 3);
Info<< sqr(v1) << endl;

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@ -55,6 +55,9 @@ UNARY_FUNCTION(symmTensor, symmTensor, inv)
UNARY_OPERATOR(vector, symmTensor, *, hdual)
BINARY_OPERATOR(tensor, symmTensor, symmTensor, &, dot)
BINARY_TYPE_OPERATOR(tensor, symmTensor, symmTensor, &, dot)
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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@ -65,6 +65,9 @@ UNARY_FUNCTION(symmTensor, symmTensor, inv)
UNARY_OPERATOR(vector, symmTensor, *, hdual)
BINARY_OPERATOR(tensor, symmTensor, symmTensor, &, dot)
BINARY_TYPE_OPERATOR(tensor, symmTensor, symmTensor, &, dot)
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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@ -164,6 +164,9 @@ tmp<Field<symmTensor> > transformFieldMask<symmTensor>
UNARY_OPERATOR(vector, symmTensor, *, hdual)
BINARY_OPERATOR(tensor, symmTensor, symmTensor, &, dot)
BINARY_TYPE_OPERATOR(tensor, symmTensor, symmTensor, &, dot)
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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@ -39,6 +39,7 @@ SourceFiles
#include "vectorField.H"
#include "sphericalTensor.H"
#include "symmTensor.H"
#include "tensor.H"
#define TEMPLATE
#include "FieldFunctionsM.H"
@ -69,6 +70,9 @@ UNARY_FUNCTION(symmTensor, symmTensor, inv)
UNARY_OPERATOR(vector, symmTensor, *, hdual)
BINARY_OPERATOR(tensor, symmTensor, symmTensor, &, dot)
BINARY_TYPE_OPERATOR(tensor, symmTensor, symmTensor, &, dot)
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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@ -53,6 +53,9 @@ UNARY_FUNCTION(symmTensor, symmTensor, inv, inv)
UNARY_OPERATOR(vector, symmTensor, *, hdual, transform)
BINARY_OPERATOR(tensor, symmTensor, symmTensor, &, '&', dot)
BINARY_TYPE_OPERATOR(tensor, symmTensor, symmTensor, &, '&', dot)
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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@ -65,6 +65,10 @@ UNARY_FUNCTION(symmTensor, symmTensor, inv, inv)
UNARY_OPERATOR(vector, symmTensor, *, hdual, transform)
BINARY_OPERATOR(tensor, symmTensor, symmTensor, &, '&', dot)
BINARY_TYPE_OPERATOR(tensor, symmTensor, symmTensor, &, '&', dot)
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
} // End namespace Foam

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@ -24,6 +24,7 @@ License
\*---------------------------------------------------------------------------*/
#include "Vector.H"
#include "Tensor.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -184,18 +185,21 @@ inline Vector<Cmpt> operator*(const SymmTensor<Cmpt>& st)
//- Inner-product between two symmetric tensors
template <class Cmpt>
inline SymmTensor<Cmpt>
inline Tensor<Cmpt>
operator&(const SymmTensor<Cmpt>& st1, const SymmTensor<Cmpt>& st2)
{
return SymmTensor<Cmpt>
return Tensor<Cmpt>
(
st1.xx()*st2.xx() + st1.xy()*st2.xy() + st1.xz()*st2.xz(),
st1.xx()*st2.xy() + st1.xy()*st2.yy() + st1.xz()*st2.yz(),
st1.xx()*st2.xz() + st1.xy()*st2.yz() + st1.xz()*st2.zz(),
st1.xy()*st2.xx() + st1.yy()*st2.xy() + st1.yz()*st2.xz(),
st1.xy()*st2.xy() + st1.yy()*st2.yy() + st1.yz()*st2.yz(),
st1.xy()*st2.xz() + st1.yy()*st2.yz() + st1.yz()*st2.zz(),
st1.xz()*st2.xx() + st1.yz()*st2.xy() + st1.zz()*st2.xz(),
st1.xz()*st2.xy() + st1.yz()*st2.yy() + st1.zz()*st2.yz(),
st1.xz()*st2.xz() + st1.yz()*st2.yz() + st1.zz()*st2.zz()
);
}

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@ -40,13 +40,15 @@ SourceFiles
#include "Vector.H"
#include "SphericalTensor.H"
#include "SymmTensor.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
namespace Foam
{
template<class Cmpt>
class SymmTensor;
/*---------------------------------------------------------------------------*\
Class Tensor Declaration
\*---------------------------------------------------------------------------*/

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@ -23,6 +23,8 @@ License
\*---------------------------------------------------------------------------*/
#include "SymmTensor.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
namespace Foam

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@ -970,381 +970,381 @@ internalField nonuniform List<scalar>
0
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1
1
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1

View File

@ -970,381 +970,381 @@ internalField nonuniform List<scalar>
1
1
1
0
0
0
0
0
0
0
0
0
0
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0
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0

View File

@ -970,381 +970,381 @@ internalField nonuniform List<scalar>
1
1
1
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
0
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0

View File

@ -15,7 +15,7 @@ FoamFile
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
LESModel Smagorinsky;
LESModel laminar;
printCoeffs on;
@ -26,61 +26,4 @@ cubeRootVolCoeffs
deltaCoeff 1;
}
PrandtlCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
smoothCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
maxDeltaRatio 1.1;
}
Cdelta 0.158;
}
vanDriestCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
smoothCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
maxDeltaRatio 1.1;
}
Aplus 26;
Cdelta 0.158;
}
smoothCoeffs
{
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
maxDeltaRatio 1.1;
}
// ************************************************************************* //

View File

@ -25,7 +25,7 @@ regions
(
boxToCell
{
box (0 0 -0.1) (0.15 0.501 0.1);
box (0 0 -0.1) (0.15 0.701 0.1);
fieldValues
(
volScalarFieldValue alphaair 0

View File

@ -0,0 +1,51 @@
/*--------------------------------*- 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
{
leftWall
{
type fixedValue;
value uniform (0 0 0);
}
rightWall
{
type fixedValue;
value uniform (0 0 0);
}
lowerWall
{
type fixedValue;
value uniform (0 0 0);
}
atmosphere
{
type fluxCorrectedVelocity;
value uniform (0 0 0);
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,51 @@
/*--------------------------------*- 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 Uair;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
leftWall
{
type fixedValue;
value uniform (0 0 0);
}
rightWall
{
type fixedValue;
value uniform (0 0 0);
}
lowerWall
{
type fixedValue;
value uniform (0 0 0);
}
atmosphere
{
type fluxCorrectedVelocity;
value uniform (0 0 0);
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,51 @@
/*--------------------------------*- 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 Umercury;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
leftWall
{
type fixedValue;
value uniform (0 0 0);
}
rightWall
{
type fixedValue;
value uniform (0 0 0);
}
lowerWall
{
type fixedValue;
value uniform (0 0 0);
}
atmosphere
{
type fluxCorrectedVelocity;
value uniform (0 0 0);
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,51 @@
/*--------------------------------*- 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 Uoil;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
leftWall
{
type fixedValue;
value uniform (0 0 0);
}
rightWall
{
type fixedValue;
value uniform (0 0 0);
}
lowerWall
{
type fixedValue;
value uniform (0 0 0);
}
atmosphere
{
type fluxCorrectedVelocity;
value uniform (0 0 0);
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,51 @@
/*--------------------------------*- 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 Uwater;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
leftWall
{
type fixedValue;
value uniform (0 0 0);
}
rightWall
{
type fixedValue;
value uniform (0 0 0);
}
lowerWall
{
type fixedValue;
value uniform (0 0 0);
}
atmosphere
{
type fluxCorrectedVelocity;
value uniform (0 0 0);
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,79 @@
/*--------------------------------*- 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;
location "0";
object alphaair;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
leftWall
{
type alphaContactAngle;
thetaProperties
(
( water air ) 90 0 0 0
( oil air ) 90 0 0 0
( mercury air ) 90 0 0 0
( water oil ) 90 0 0 0
( water mercury ) 90 0 0 0
( oil mercury ) 90 0 0 0
);
value uniform 0;
}
rightWall
{
type alphaContactAngle;
thetaProperties
(
( water air ) 90 0 0 0
( oil air ) 90 0 0 0
( mercury air ) 90 0 0 0
( water oil ) 90 0 0 0
( water mercury ) 90 0 0 0
( oil mercury ) 90 0 0 0
);
value uniform 1;
}
lowerWall
{
type alphaContactAngle;
thetaProperties
(
( water air ) 90 0 0 0
( oil air ) 90 0 0 0
( mercury air ) 90 0 0 0
( water oil ) 90 0 0 0
( water mercury ) 90 0 0 0
( oil mercury ) 90 0 0 0
);
value uniform 0;
}
atmosphere
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,49 @@
/*--------------------------------*- 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;
location "0";
object alphamercury;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
leftWall
{
type zeroGradient;
}
rightWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,49 @@
/*--------------------------------*- 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;
location "0";
object alphaoil;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
leftWall
{
type zeroGradient;
}
rightWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,47 @@
/*--------------------------------*- 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;
location "0";
object alphas;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
leftWall
{
type zeroGradient;
}
rightWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
atmosphere
{
type zeroGradient;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,49 @@
/*--------------------------------*- 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;
location "0";
object alphawater;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
leftWall
{
type zeroGradient;
}
rightWall
{
type zeroGradient;
}
lowerWall
{
type zeroGradient;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
leftWall
{
type multiphaseFixedFluxPressure;
value uniform 0;
}
rightWall
{
type multiphaseFixedFluxPressure;
value uniform 0;
}
lowerWall
{
type multiphaseFixedFluxPressure;
value uniform 0;
}
atmosphere
{
type totalPressure;
p0 uniform 0;
U Uair;
phi phiair;
rho rho;
psi none;
gamma 1;
value uniform 0;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,11 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cleanCase
\rm -rf 0
# ----------------------------------------------------------------- end-of-file

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@ -0,0 +1,19 @@
#!/bin/sh
cd ${0%/*} || exit 1 # run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Set application name
application=`getApplication`
\rm -rf 0
cp -r 0.org 0
runApplication blockMesh
runApplication setFields
runApplication decomposePar
runParallel $application 4
runApplication reconstructPar
# ----------------------------------------------------------------- end-of-file

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@ -0,0 +1,29 @@
/*--------------------------------*- 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 LESProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
LESModel laminar;
printCoeffs on;
delta cubeRootVol;
cubeRootVolCoeffs
{
deltaCoeff 1;
}
// ************************************************************************* //

View File

@ -0,0 +1,20 @@
/*--------------------------------*- 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 MRFZones;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
0()
// ************************************************************************* //

View File

@ -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 );
// ************************************************************************* //

View File

@ -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 dictionary;
location "constant";
object motionProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
movingFvMesh staticFvMesh;
// ************************************************************************* //

View File

@ -0,0 +1,108 @@
/*--------------------------------*- 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 0.146;
vertices
(
(0 0 0)
(2 0 0)
(2.16438 0 0)
(4 0 0)
(0 0.32876 0)
(2 0.32876 0)
(2.16438 0.32876 0)
(4 0.32876 0)
(0 4 0)
(2 4 0)
(2.16438 4 0)
(4 4 0)
(0 0 0.1)
(2 0 0.1)
(2.16438 0 0.1)
(4 0 0.1)
(0 0.32876 0.1)
(2 0.32876 0.1)
(2.16438 0.32876 0.1)
(4 0.32876 0.1)
(0 4 0.1)
(2 4 0.1)
(2.16438 4 0.1)
(4 4 0.1)
);
blocks
(
hex (0 1 5 4 12 13 17 16) (92 15 1) simpleGrading (1 1 1)
hex (2 3 7 6 14 15 19 18) (76 15 1) simpleGrading (1 1 1)
hex (4 5 9 8 16 17 21 20) (92 180 1) simpleGrading (1 1 1)
hex (5 6 10 9 17 18 22 21) (8 180 1) simpleGrading (1 1 1)
hex (6 7 11 10 18 19 23 22) (76 180 1) simpleGrading (1 1 1)
);
edges
(
);
boundary
(
leftWall
{
type wall;
faces
(
(0 12 16 4)
(4 16 20 8)
);
}
rightWall
{
type wall;
faces
(
(7 19 15 3)
(11 23 19 7)
);
}
lowerWall
{
type wall;
faces
(
(0 1 13 12)
(1 5 17 13)
(5 6 18 17)
(2 14 18 6)
(2 3 15 14)
);
}
atmosphere
{
type patch;
faces
(
(8 20 21 9)
(9 21 22 10)
(10 22 23 11)
);
}
);
mergePatchPairs
(
);
// ************************************************************************* //

View File

@ -0,0 +1,52 @@
/*--------------------------------*- 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;
location "constant/polyMesh";
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
5
(
leftWall
{
type wall;
nFaces 195;
startFace 68014;
}
rightWall
{
type wall;
nFaces 195;
startFace 68209;
}
lowerWall
{
type wall;
nFaces 206;
startFace 68404;
}
atmosphere
{
type patch;
nFaces 176;
startFace 68610;
}
defaultFaces
{
type empty;
nFaces 68400;
startFace 68786;
}
)
// ************************************************************************* //

View File

@ -0,0 +1,248 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
phases
(
water
{
nu 1e-06;
kappa 1e-06;
Cp 4195;
rho 1000;
diameterModel constant;
constantCoeffs
{
d 1e-3;
}
}
oil
{
nu 1e-06;
kappa 1e-06;
Cp 4195;
rho 500;
diameterModel constant;
constantCoeffs
{
d 1e-3;
}
}
mercury
{
nu 1.125e-07;
kappa 1e-06;
Cp 4195;
rho 13529;
diameterModel constant;
constantCoeffs
{
d 1e-3;
}
}
air
{
nu 1.48e-05;
kappa 2.63e-2;
Cp 1007;
rho 1;
diameterModel constant;
constantCoeffs
{
d 3e-3;
}
}
);
sigmas
(
(air water) 0.07
(air oil) 0.07
(air mercury) 0.07
(water oil) 0
(water mercury) 0
(oil mercury) 0
);
interfaceCompression
(
(air water) 1
(air oil) 1
(air mercury) 1
(water oil) 0
(water mercury) 0
(oil mercury) 0
);
virtualMass
(
(air water) 0
(air oil) 0
(air mercury) 0
(water oil) 0.5
(water mercury) 0.5
(oil mercury) 0.5
);
drag
(
(air water)
{
type blended;
air
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
water
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
residualPhaseFraction 1e-3;
residualSlip 1e-3;
}
(air oil)
{
type blended;
air
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
oil
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
residualPhaseFraction 1e-3;
residualSlip 1e-3;
}
(air mercury)
{
type blended;
air
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
mercury
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
residualPhaseFraction 1e-3;
residualSlip 1e-3;
}
(water oil)
{
type blended;
water
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
oil
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
residualPhaseFraction 1e-3;
residualSlip 1e-3;
}
(water mercury)
{
type blended;
water
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
mercury
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
residualPhaseFraction 1e-3;
residualSlip 1e-3;
}
(oil mercury)
{
type blended;
oil
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
mercury
{
type SchillerNaumann;
residualPhaseFraction 0;
residualSlip 0;
}
residualPhaseFraction 1e-3;
residualSlip 1e-3;
}
);
// This is a dummy to support the Smagorinsky model
transportModel Newtonian;
nu nu [ 0 2 -1 0 0 0 0 ] 0;
// ************************************************************************* //

View File

@ -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 dictionary;
location "constant";
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType laminar;
// ************************************************************************* //

View File

@ -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 multiphaseEulerFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 6;
deltaT 0.001;
writeControl adjustableRunTime;
writeInterval 0.01;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep yes;
maxCo 0.5;
maxAlphaCo 0.5;
maxDeltaT 1;
// ************************************************************************* //

View File

@ -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 dictionary;
location "system";
object decomposeParDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
numberOfSubdomains 4;
method simple;
simpleCoeffs
{
n ( 2 2 1 );
delta 0.001;
}
hierarchicalCoeffs
{
n ( 1 1 1 );
delta 0.001;
order xyz;
}
manualCoeffs
{
dataFile "";
}
distributed no;
roots ( );
// ************************************************************************* //

View File

@ -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 ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
"div\(phi,alpha.*\)" Gauss vanLeer;
"div\(phir,alpha.*,alpha.*\)" Gauss vanLeer;
"div\(phiAlpha.*,U.*\)" Gauss limitedLinearV 1;
div(Rc) Gauss linear;
"div\(phi.*,U.*\)" Gauss limitedLinearV 1;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p;
pcorr;
}
// ************************************************************************* //

View File

@ -0,0 +1,94 @@
/*--------------------------------*- 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
{
p
{
solver GAMG;
tolerance 1e-7;
relTol 0.05;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
nFinestSweeps 2;
cacheAgglomeration on;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
}
pFinal
{
solver PCG;
preconditioner
{
preconditioner GAMG;
tolerance 1e-7;
relTol 0;
nVcycles 2;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
nFinestSweeps 2;
cacheAgglomeration on;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
}
tolerance 1e-7;
relTol 0;
maxIter 20;
}
pcorr
{
$pFinal;
tolerance 1e-5;
relTol 0;
}
U
{
solver smoothSolver;
smoother GaussSeidel;
tolerance 1e-8;
relTol 0.1;
nSweeps 1;
}
UFinal
{
$U;
tolerance 1e-7;
relTol 0;
}
}
PIMPLE
{
nCorrectors 3;
nNonOrthogonalCorrectors 0;
nAlphaSubCycles 3;
}
relaxationFactors
{
"U.*" 1;
}
// ************************************************************************* //

View File

@ -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 setFieldsDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
defaultFieldValues
(
volScalarFieldValue alphaair 1
volScalarFieldValue alphawater 0
volScalarFieldValue alphaoil 0
volScalarFieldValue alphamercury 0
volVectorFieldValue U ( 0 0 0 )
);
regions
(
boxToCell
{
box ( 0 0 -1 ) ( 0.1461 0.292 1 );
fieldValues
(
volScalarFieldValue alphawater 1
volScalarFieldValue alphaoil 0
volScalarFieldValue alphamercury 0
volScalarFieldValue alphaair 0
);
}
boxToCell
{
box ( 0.1461 0 -1 ) ( 0.2922 0.292 1 );
fieldValues
(
volScalarFieldValue alphawater 0
volScalarFieldValue alphaoil 1
volScalarFieldValue alphamercury 0
volScalarFieldValue alphaair 0
);
}
boxToCell
{
box ( 0 0 -1 ) ( 0.1461 0.1 1 );
fieldValues
(
volScalarFieldValue alphawater 0
volScalarFieldValue alphaoil 0
volScalarFieldValue alphamercury 1
volScalarFieldValue alphaair 0
);
}
);
// ************************************************************************* //