pimpleFoam tutorial

This commit is contained in:
mattijs
2008-08-15 12:20:42 +01:00
parent 4164b8efe8
commit c1cd9c4cd7
13 changed files with 877 additions and 0 deletions

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://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
{
inlet
{
type pressureInletOutletVelocity;
value uniform (0 0 0);
}
outlet1
{
type inletOutlet;
inletValue uniform (0 0 0);
value uniform (0 0 0);
}
outlet2
{
type inletOutlet;
inletValue uniform (0 0 0);
value uniform (0 0 0);
}
defaultFaces
{
type fixedValue;
value uniform (0 0 0);
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://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;
boundaryField
{
inlet
{
type turbulentMixingLengthDissipationRateInlet;
mixingLength 0.01; // 1cm - half channel height
value uniform 1;
}
outlet1
{
type inletOutlet;
inletValue uniform 1;
}
outlet2
{
type inletOutlet;
inletValue uniform 1;
}
defaultFaces
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://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 1;
boundaryField
{
inlet
{
type turbulentIntensityKineticEnergyInlet;
intensity 0.05; // 5% turbulence
value uniform 1;
}
outlet1
{
type inletOutlet;
inletValue uniform 1;
}
outlet2
{
type inletOutlet;
inletValue uniform 1;
}
defaultFaces
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object nuTilda;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type zeroGradient;
}
outlet1
{
type zeroGradient;
}
outlet2
{
type zeroGradient;
}
defaultFaces
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 100000;
boundaryField
{
inlet
{
type totalPressure;
p0 uniform 100040;
U U;
phi phi;
rho none;
psi none;
gamma 1;
value uniform 100040;
}
outlet1
{
type fixedValue;
value uniform 100010;
}
outlet2
{
type fixedValue;
value uniform 100000;
}
defaultFaces
{
type zeroGradient;
}
}
// ************************************************************************* //

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15/8/8 Simple T-junction. Inlet on left, one outlet at bottom, one at top.
To test multiple outlets.

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel kEpsilon;
turbulence on;
printCoeffs on;
laminarCoeffs
{
}
kEpsilonCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
RNGkEpsilonCoeffs
{
Cmu 0.0845;
C1 1.42;
C2 1.68;
alphak 1.39;
alphaEps 1.39;
eta0 4.38;
beta 0.012;
}
realizableKECoeffs
{
Cmu 0.09;
A0 4.0;
C2 1.9;
alphak 1;
alphaEps 0.833333;
}
kOmegaSSTCoeffs
{
alphaK1 0.85034;
alphaK2 1.0;
alphaOmega1 0.5;
alphaOmega2 0.85616;
gamma1 0.5532;
gamma2 0.4403;
beta1 0.0750;
beta2 0.0828;
betaStar 0.09;
a1 0.31;
c1 10;
Cmu 0.09;
}
NonlinearKEShihCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76932;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
}
LienCubicKECoeffs
{
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
}
QZetaCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaZeta 0.76923;
anisotropic no;
}
LaunderSharmaKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
LamBremhorstKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
LienCubicKELowReCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
Am 0.016;
Aepsilon 0.263;
Amu 0.00222;
}
LienLeschzinerLowReCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
Am 0.016;
Aepsilon 0.263;
Amu 0.00222;
}
LRRCoeffs
{
Cmu 0.09;
Clrr1 1.8;
Clrr2 0.6;
C1 1.44;
C2 1.92;
Cs 0.25;
Ceps 0.15;
alphaEps 0.76923;
}
LaunderGibsonRSTMCoeffs
{
Cmu 0.09;
Clg1 1.8;
Clg2 0.6;
C1 1.44;
C2 1.92;
C1Ref 0.5;
C2Ref 0.3;
Cs 0.25;
Ceps 0.15;
alphaEps 0.76923;
alphaR 1.22;
}
SpalartAllmarasCoeffs
{
alphaNut 1.5;
Cb1 0.1355;
Cb2 0.622;
Cw2 0.3;
Cw3 2;
Cv1 7.1;
Cv2 5.0;
}
wallFunctionCoeffs
{
kappa 0.4187;
E 9;
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// outlet1
// +-+
// | |
// | |
// | |
// | |
// +-----------+ |
// |inlet |
// +-----------+ |
// | |
// | |
// | |
// | |
// +-+
// outlet2
convertToMeters 1;
vertices
(
(0.0 -0.01 0) //0
(0.2 -0.01 0)
(0.2 0.01 0) //2
(0.0 0.01 0)
(0.22 -0.01 0) //4
(0.22 0.01 0)
(0.2 -0.21 0) //6
(0.22 -0.21 0)
(0.2 0.21 0) //8
(0.22 0.21 0)
// Z
(0.0 -0.01 0.02) //0
(0.2 -0.01 0.02)
(0.2 0.01 0.02) //2
(0.0 0.01 0.02)
(0.22 -0.01 0.02) //4
(0.22 0.01 0.02)
(0.2 -0.21 0.02) //6
(0.22 -0.21 0.02)
(0.2 0.21 0.02) //8
(0.22 0.21 0.02)
);
blocks
(
// inlet block
hex (0 1 2 3 10 11 12 13) (50 5 5) simpleGrading (1 1 1)
// central block
hex (1 4 5 2 11 14 15 12) (5 5 5) simpleGrading (1 1 1)
// bottom block
hex (6 7 4 1 16 17 14 11) (5 50 5) simpleGrading (1 1 1)
// top block
hex (2 5 9 8 12 15 19 18) (5 50 5) simpleGrading (1 1 1)
);
edges
(
);
patches
(
patch inlet
(
(0 10 13 3)
)
patch outlet1
(
(6 7 17 16)
)
patch outlet2
(
(8 18 19 9)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
location "constant/polyMesh";
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
4
(
inlet
{
type patch;
nFaces 25;
startFace 10050;
}
outlet1
{
type patch;
nFaces 25;
startFace 10075;
}
outlet2
{
type patch;
nFaces 25;
startFace 10100;
}
defaultFaces
{
type wall;
nFaces 3075;
startFace 10125;
}
)
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
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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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application turbFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 1;
deltaT 0.001;
writeControl adjustableRunTime;
writeInterval 0.1;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep yes;
maxCo 5;
functions
(
probes
{
// Type of functionObject
type probes;
// Where to load it from (if not already in solver)
functionObjectLibs ("libsampling.so");
// Name of the directory for the probe data
name probes;
// Locations to be probed. runTime modifiable!
probeLocations
(
(1E-6 0 0.01) // at inlet
(0.21 -0.20999 0.01) // at outlet1
(0.21 0.20999 0.01) // at outlet2
(0.21 0 0.01) // at central block
);
// Fields to be probed. runTime modifiable!
fields
(
p
U
);
}
);
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(U) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phi,k) Gauss limitedLinear 1;
div(phi,epsilon) Gauss limitedLinear 1;
div(phi,R) Gauss limitedLinear 1;
div(R) Gauss linear;
div(phi,nuTilda) Gauss limitedLinear 1;
div((nuEff*dev(grad(U).T()))) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuEff,U) Gauss linear corrected;
laplacian((1|A(U)),p) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
laplacian(DREff,R) Gauss linear corrected;
laplacian(DnuTildaEff,nuTilda) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(U) linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p;
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p GAMG
{
tolerance 1e-6;
relTol 0.01;
smoother GaussSeidel;
cacheAgglomeration true;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
};
pFinal GAMG
{
tolerance 1e-6;
relTol 0.0;
smoother GaussSeidel;
cacheAgglomeration true;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
};
U PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0.1;
};
UFinal PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
k PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
epsilon PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0;
};
}
PIMPLE
{
nOuterCorrectors 2;
nCorrectors 2;
nNonOrthogonalCorrectors 0;
pRefCell 0;
pRefValue 0;
}
relaxationFactors
{
//p 0.3;
U 1.0;
k 1.0;
epsilon 1.0;
}
// ************************************************************************* //