more updates...

This commit is contained in:
andy
2009-02-13 17:03:05 +00:00
parent ef874be0b9
commit 4b81f44378
23 changed files with 204 additions and 72 deletions

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@ -1,8 +1,8 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
@ -10,6 +10,7 @@ FoamFile
version 2.0;
format binary;
class polyBoundaryMesh;
location "constant/polyMesh";
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
transportModel Newtonian;
nu nu [ 0 2 -1 0 0 0 0 ] 1e-05;
CrossPowerLawCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
m m [ 0 0 1 0 0 0 0 ] 1;
n n [ 0 0 0 0 0 0 0 ] 1;
}
BirdCarreauCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
k k [ 0 0 1 0 0 0 0 ] 0;
n n [ 0 0 0 0 0 0 0 ] 1;
}
// ************************************************************************* //

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@ -8,14 +8,14 @@
FoamFile
{
version 2.0;
format binary;
format ascii;
class dictionary;
location "constant";
object transportProperties;
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
nu nu [ 0 2 -1 0 0 0 0 ] 1e-05;
simulationType laminar;
// ************************************************************************* //

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@ -30,6 +30,7 @@ divSchemes
{
default none;
div(phi,U) Gauss linear;
div((nuEff*dev(grad(U).T()))) Gauss linear;
}
laplacianSchemes
@ -39,6 +40,7 @@ laplacianSchemes
laplacian(rAU,pcorr) Gauss linear corrected;
laplacian(rAU,p) Gauss linear corrected;
laplacian(diffusivity,cellMotionU) Gauss linear uncorrected;
laplacian(nuEff,U) Gauss linear uncorrected;
}
interpolationSchemes

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@ -33,12 +33,16 @@ boundaryField
innerWall
{
type zeroGradient;
type epsilonWallFunction;
U Urel;
value uniform 14.855;
}
outerWall
{
type zeroGradient;
type epsilonWallFunction;
U Urel;
value uniform 14.855;
}
cyclic

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@ -1,8 +1,8 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
@ -10,6 +10,7 @@ FoamFile
version 2.0;
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -25,26 +26,26 @@ boundaryField
type fixedValue;
value uniform 0.375;
}
outlet
{
type zeroGradient;
}
innerWall
{
type zeroGradient;
type kQRWallFunction;
value uniform 0.375;
}
outerWall
{
type zeroGradient;
type kQRWallFunction;
value uniform 0.375;
}
cyclic
{
type cyclic;
value uniform 0.375;
}
}
// ************************************************************************* //

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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 volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
innerWall
{
type nutWallFunction;
U Urel;
value uniform 0;
}
outerWall
{
type nutWallFunction;
U Urel;
value uniform 0;
}
cyclic
{
type cyclic;
value uniform 0;
}
}
// ************************************************************************* //

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@ -1,8 +1,8 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
@ -10,6 +10,7 @@ FoamFile
version 2.0;
format ascii;
class volScalarField;
location "0";
object omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -25,26 +26,28 @@ boundaryField
type fixedValue;
value uniform 3.5;
}
outlet
{
type zeroGradient;
}
innerWall
{
type zeroGradient;
type omegaWallFunction;
U Urel;
value uniform 3.5;
}
outerWall
{
type zeroGradient;
type omegaWallFunction;
U Urel;
value uniform 3.5;
}
cyclic
{
type cyclic;
value uniform 3.5;
}
}
// ************************************************************************* //

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@ -1,7 +1,9 @@
EXE_INC = \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/turbulenceModels/RAS \
-I$(LIB_SRC)/transportModels
-I$(LIB_SRC)/turbulenceModels \
-I$(LIB_SRC)/turbulenceModels/incompressible/RAS/RASModel \
-I$(LIB_SRC)/transportModels \
-I$(LIB_SRC)/transportModels/incompressible/singlePhaseTransportModel
EXE_LIBS = \
-lincompressibleRASModels \

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@ -0,0 +1,16 @@
// Momentum predictor
tmp<fvVectorMatrix> UrelEqn
(
fvm::div(phi, Urel)
+ turbulence->divDevReff(Urel)
+ SRF->Su()
);
UrelEqn().relax();
eqnResidual = solve
(
UrelEqn() == -fvc::grad(p)
).initialResidual();
maxResidual = max(eqnResidual, maxResidual);

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@ -0,0 +1,9 @@
// check convergence
if (maxResidual < convergenceCriterion)
{
Info<< "reached convergence criterion: " << convergenceCriterion << endl;
runTime.writeAndEnd();
Info<< "latestTime = " << runTime.timeName() << endl;
}

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@ -0,0 +1,7 @@
// initialize values for convergence checks
scalar eqnResidual = 1, maxResidual = 0;
scalar convergenceCriterion = 0;
simple.readIfPresent("convergence", convergenceCriterion);

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@ -0,0 +1,34 @@
{
p.boundaryField().updateCoeffs();
volScalarField AUrel = UrelEqn().A();
Urel = UrelEqn().H()/AUrel;
UrelEqn.clear();
phi = fvc::interpolate(Urel) & mesh.Sf();
adjustPhi(phi, Urel, p);
// Non-orthogonal pressure corrector loop
for (int nonOrth=0; nonOrth<=nNonOrthCorr; nonOrth++)
{
fvScalarMatrix pEqn
(
fvm::laplacian(1.0/AUrel, p) == fvc::div(phi)
);
pEqn.setReference(pRefCell, pRefValue);
pEqn.solve();
if (nonOrth == nNonOrthCorr)
{
phi -= pEqn.flux();
}
}
# include "continuityErrs.H"
// Explicitly relax pressure for momentum corrector
p.relax();
// Momentum corrector
Urel -= fvc::grad(p)/AUrel;
Urel.correctBoundaryConditions();
}

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@ -32,8 +32,8 @@ Description
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "incompressible/singlePhaseTransportModel/singlePhaseTransportModel.H"
#include "incompressible/RASModel/RASModel.H"
#include "singlePhaseTransportModel.H"
#include "RASModel.H"
#include "SRFModel.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
@ -42,7 +42,6 @@ int main(int argc, char *argv[])
{
# include "setRootCase.H"
# include "createTime.H"
# include "createMesh.H"
# include "createFields.H"
@ -59,55 +58,14 @@ int main(int argc, char *argv[])
Info<< "Time = " << runTime.timeName() << nl << endl;
# include "readSIMPLEControls.H"
# include "initConvergenceCheck.H"
p.storePrevIter();
// Pressure-velocity SIMPLE corrector
{
// Momentum predictor
tmp<fvVectorMatrix> UrelEqn
(
fvm::div(phi, Urel)
+ turbulence->divDevReff(Urel)
+ SRF->Su()
);
UrelEqn().relax();
solve(UrelEqn() == -fvc::grad(p));
p.boundaryField().updateCoeffs();
volScalarField AUrel = UrelEqn().A();
Urel = UrelEqn().H()/AUrel;
UrelEqn.clear();
phi = fvc::interpolate(Urel) & mesh.Sf();
adjustPhi(phi, Urel, p);
// Non-orthogonal pressure corrector loop
for (int nonOrth=0; nonOrth<=nNonOrthCorr; nonOrth++)
{
fvScalarMatrix pEqn
(
fvm::laplacian(1.0/AUrel, p) == fvc::div(phi)
);
pEqn.setReference(pRefCell, pRefValue);
pEqn.solve();
if (nonOrth == nNonOrthCorr)
{
phi -= pEqn.flux();
}
}
# include "continuityErrs.H"
// Explicitly relax pressure for momentum corrector
p.relax();
// Momentum corrector
Urel -= fvc::grad(p)/AUrel;
Urel.correctBoundaryConditions();
# include "UEqn.H"
# include "pEqn.H"
}
turbulence->correct();
@ -134,6 +92,8 @@ int main(int argc, char *argv[])
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< nl << endl;
# include "convergenceCheck.H"
}
Info<< "End\n" << endl;