adding SRF library, and tutorial with demonstration solver

This commit is contained in:
andy
2008-05-08 17:43:17 +01:00
parent 3e9f272de9
commit 082165d1c5
26 changed files with 2209 additions and 0 deletions

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#!/bin/sh
currDir=`pwd`
application=`basename $currDir`
cases="mixer"
tutorialPath=`dirname $0`/..
. $tutorialPath/CleanFunctions
wclean $application
for case in $cases
do
cleanCase $case
done

16
tutorials/simpleSRFFoam/Allrun Executable file
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#!/bin/sh
currDir=`pwd`
application=`basename $currDir`
cases="mixer"
tutorialPath=`dirname $0`/..
. $tutorialPath/RunFunctions
compileApplication $currDir $application
for case in $cases
do
runApplication blockMesh $case
runApplication $application $case
done

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volVectorField;
object Urel;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
inlet
{
type SRFVelocity;
inletValue uniform (0 0 -10);
relative yes;
value uniform (0 0 0);
}
outlet
{
type zeroGradient;
}
innerWall
{
type fixedValue;
value uniform (0 0 0);
}
outerWall
{
type SRFVelocity;
inletValue uniform (0 0 0);
relative yes;
value uniform (0 0 0);
}
cyclic
{
type cyclic;
}
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 14.855;
boundaryField
{
inlet
{
type fixedValue;
value uniform 14.855;
}
outlet
{
type zeroGradient;
}
innerWall
{
type zeroGradient;
}
outerWall
{
type zeroGradient;
}
cyclic
{
type cyclic;
}
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0.375;
boundaryField
{
inlet
{
type fixedValue;
value uniform 0.375;
}
outlet
{
type zeroGradient;
}
innerWall
{
type zeroGradient;
}
outerWall
{
type zeroGradient;
}
cyclic
{
type cyclic;
}
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 -1 0 0 0 0];
internalField uniform 3.5;
boundaryField
{
inlet
{
type fixedValue;
value uniform 3.5;
}
outlet
{
type zeroGradient;
}
innerWall
{
type zeroGradient;
}
outerWall
{
type zeroGradient;
}
cyclic
{
type cyclic;
}
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue;
value uniform 0;
}
innerWall
{
type zeroGradient;
}
outerWall
{
type zeroGradient;
}
cyclic
{
type cyclic;
}
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object SRFProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
SRFModel rpm;
axis (0 0 1);
rpmCoeffs
{
rpm 5000.0;
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.1;
vertices
(
( 0.500 0.000 0.000)
( 0.369 0.338 0.000)
( 0.338 0.369 0.000)
( 0.000 0.500 0.000)
( 0.737 0.676 0.000)
( 0.074 0.068 0.000)
( 0.676 0.737 0.000)
( 0.068 0.074 0.000)
( 0.000 1.000 0.000)
( 1.000 0.000 0.000)
( 0.100 0.000 0.000)
( 0.000 0.100 0.000)
( 0.500 0.000 2.000)
( 0.369 0.338 2.000)
( 0.338 0.369 2.000)
( 0.000 0.500 2.000)
( 0.737 0.676 2.000)
( 0.074 0.068 2.000)
( 0.676 0.737 2.000)
( 0.068 0.074 2.000)
( 0.000 1.000 2.000)
( 1.000 0.000 2.000)
( 0.100 0.000 2.000)
( 0.000 0.100 2.000)
);
blocks
(
hex (1 0 9 4 13 12 21 16) (10 20 40) simpleGrading (1 1 1)
hex (2 1 4 6 14 13 16 18) (2 20 40) simpleGrading (1 1 1)
hex (3 2 6 8 15 14 18 20) (10 20 40) simpleGrading (1 1 1)
hex (5 10 0 1 17 22 12 13) (10 20 40) simpleGrading (1 1 1)
hex (11 7 2 3 23 19 14 15) (10 20 40) simpleGrading (1 1 1)
);
edges
(
arc 0 1 ( 0.470 0.171 0.000 )
arc 12 13 ( 0.470 0.171 2.000 )
arc 2 3 ( 0.171 0.470 0.000 )
arc 14 15 ( 0.171 0.470 2.000 )
arc 9 4 ( 0.940 0.342 0.000 )
arc 21 16 ( 0.940 0.342 2.000 )
arc 5 10 ( 0.094 0.034 0.000 )
arc 17 22 ( 0.094 0.034 2.000 )
arc 6 8 ( 0.342 0.940 0.000 )
arc 18 20 ( 0.342 0.940 2.000 )
arc 11 7 ( 0.034 0.094 0.000 )
arc 23 19 ( 0.034 0.094 2.000 )
);
patches
(
patch inlet
(
(13 12 21 16)
(14 13 16 18)
(15 14 18 20)
(17 22 12 13)
(23 19 14 15)
)
patch outlet
(
(1 4 9 0)
(2 6 4 1)
(3 8 6 2)
(5 1 0 10)
(11 3 2 7)
)
wall innerWall
(
(2 1 13 14)
(5 10 22 17)
(5 17 13 1)
(11 7 19 23)
(7 2 14 19)
)
wall outerWall
(
(4 16 21 9)
(6 18 16 4)
(8 20 18 6)
)
cyclic cyclic
(
(0 9 21 12)
(10 0 12 22)
(3 15 20 8)
(11 23 15 3)
)
);
mergeMatchPairs
(
);

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 1.5e-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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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
turbulenceModel kOmegaSST;
turbulence on;
laminarCoeffs
{
}
kEpsilonCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
RNGkEpsilonCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.0845;
C1 C1 [0 0 0 0 0 0 0] 1.42;
C2 C2 [0 0 0 0 0 0 0] 1.68;
alphak alphaK [0 0 0 0 0 0 0] 1.39;
alphaEps alphaEps [0 0 0 0 0 0 0] 1.39;
eta0 eta0 [0 0 0 0 0 0 0] 4.38;
beta beta [0 0 0 0 0 0 0] 0.012;
}
kOmegaSSTCoeffs
{
alphaK1 alphaK1 [0 0 0 0 0 0 0] 0.85034;
alphaK2 alphaK1 [0 0 0 0 0 0 0] 1.0;
alphaOmega1 alphaOmega1 [0 0 0 0 0 0 0] 0.5;
alphaOmega2 alphaOmega2 [0 0 0 0 0 0 0] 0.85616;
gamma1 gamma1 [0 0 0 0 0 0 0] 0.5532;
gamma2 gamma2 [0 0 0 0 0 0 0] 0.4403;
beta1 beta1 [0 0 0 0 0 0 0] 0.0750;
beta2 beta2 [0 0 0 0 0 0 0] 0.0828;
betaStar betaStar [0 0 0 0 0 0 0] 0.09;
a1 a1 [0 0 0 0 0 0 0] 0.31;
c1 c1 [0 0 0 0 0 0 0] 10;
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
}
NonlinearKEShihCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphak alphak [0 0 0 0 0 0 0] 1;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76932;
A1 A1 [0 0 0 0 0 0 0] 1.25;
A2 A2 [0 0 0 0 0 0 0] 1000;
Ctau1 Ctau1 [0 0 0 0 0 0 0] -4;
Ctau2 Ctau2 [0 0 0 0 0 0 0] 13;
Ctau3 Ctau3 [0 0 0 0 0 0 0] -2;
alphaKsi alphaKsi [0 0 0 0 0 0 0] 0.9;
}
LienCubicKECoeffs
{
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphak alphak [0 0 0 0 0 0 0] 1;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
A1 A1 [0 0 0 0 0 0 0] 1.25;
A2 A2 [0 0 0 0 0 0 0] 1000;
Ctau1 Ctau1 [0 0 0 0 0 0 0] -4;
Ctau2 Ctau2 [0 0 0 0 0 0 0] 13;
Ctau3 Ctau3 [0 0 0 0 0 0 0] -2;
alphaKsi alphaKsi [0 0 0 0 0 0 0] 0.9;
}
QZetaCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphaZeta alphaZeta [0 0 0 0 0 0 0] 0.76923;
anisotropic no;
}
LaunderSharmaKECoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
LamBremhorstKECoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
LienCubicKELowReCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphak alphak [0 0 0 0 0 0 0] 1;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
A1 A1 [0 0 0 0 0 0 0] 1.25;
A2 A2 [0 0 0 0 0 0 0] 1000;
Ctau1 Ctau1 [0 0 0 0 0 0 0] -4;
Ctau2 Ctau2 [0 0 0 0 0 0 0] 13;
Ctau3 Ctau3 [0 0 0 0 0 0 0] -2;
alphaKsi alphaKsi [0 0 0 0 0 0 0] 0.9;
Am Am [0 0 0 0 0 0 0] 0.016;
Aepsilon Aepsilon [0 0 0 0 0 0 0] 0.263;
Amu Amu [0 0 0 0 0 0 0] 0.00222;
}
LienLeschzinerLowReCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
alphak alphak [0 0 0 0 0 0 0] 1;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
Am Am [0 0 0 0 0 0 0] 0.016;
Aepsilon Aepsilon [0 0 0 0 0 0 0] 0.263;
Amu Amu [0 0 0 0 0 0 0] 0.00222;
}
LRRCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
Clrr1 Clrr1 [0 0 0 0 0 0 0] 1.8;
Clrr2 Clrr2 [0 0 0 0 0 0 0] 0.6;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
Cs Cs [0 0 0 0 0 0 0] 0.25;
Ceps Ceps [0 0 0 0 0 0 0] 0.15;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
}
LaunderGibsonRSTMCoeffs
{
Cmu Cmu [0 0 0 0 0 0 0] 0.09;
Clg1 Clg1 [0 0 0 0 0 0 0] 1.8;
Clg2 Clg2 [0 0 0 0 0 0 0] 0.6;
C1 C1 [0 0 0 0 0 0 0] 1.44;
C2 C2 [0 0 0 0 0 0 0] 1.92;
C1Ref C1Ref [0 0 0 0 0 0 0] 0.5;
C2Ref C2Ref [0 0 0 0 0 0 0] 0.3;
Cs Cs [0 0 0 0 0 0 0] 0.25;
Ceps Ceps [0 0 0 0 0 0 0] 0.15;
alphaEps alphaEps [0 0 0 0 0 0 0] 0.76923;
alphaR alphaR [0 0 0 0 0 0 0] 1.22;
}
SpalartAllmarasCoeffs
{
alphaNut alphaNut [0 0 0 0 0 0 0] 1.5;
Cb1 Cb1 [0 0 0 0 0 0 0] 0.1355;
Cb2 Cb2 [0 0 0 0 0 0 0] 0.622;
Cw2 Cw2 [0 0 0 0 0 0 0] 0.3;
Cw3 Cw3 [0 0 0 0 0 0 0] 2;
Cv1 Cv1 [0 0 0 0 0 0 0] 7.1;
Cv2 Cv2 [0 0 0 0 0 0 0] 5.0;
}
wallFunctionCoeffs
{
kappa kappa [0 0 0 0 0 0 0] 0.4187;
E E [0 0 0 0 0 0 0] 9;
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application simpleSRFFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 1000;
deltaT 1;
writeControl timeStep;
writeInterval 100;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(Urel) Gauss linear;
}
divSchemes
{
default none;
div(phi,Urel) Gauss upwind;
div(phi,k) Gauss upwind;
div(phi,epsilon) Gauss upwind;
div(phi,omega) Gauss upwind;
div(phi,R) Gauss upwind;
div(R) Gauss linear;
div(phi,nuTilda) Gauss upwind;
div((nuEff*dev(grad(Urel).T()))) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuEff,Urel) Gauss linear corrected;
laplacian((1|A(Urel)),p) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
laplacian(DomegaEff,omega) Gauss linear corrected;
laplacian(DREff,R) Gauss linear corrected;
laplacian(DnuTildaEff,nuTilda) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(Urel) linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p;
}
// ************************************************************************* //

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@ -0,0 +1,88 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p PCG
{
preconditioner DIC;
tolerance 1e-06;
relTol 0.01;
};
Urel PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0.1;
};
k PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0.1;
};
epsilon PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0.1;
};
omega PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0.1;
};
R PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0.1;
};
nuTilda PBiCG
{
preconditioner DILU;
tolerance 1e-05;
relTol 0.1;
};
}
SIMPLE
{
nNonOrthogonalCorrectors 0;
}
relaxationFactors
{
p 0.3;
Urel 0.7;
k 0.7;
epsilon 0.7;
omega 0.7;
R 0.7;
nuTilda 0.7;
}
// ************************************************************************* //

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simpleSRFFoam.C
EXE = $(FOAM_USER_APPBIN)/simpleSRFFoam

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EXE_INC = \
-I$(LIB_SRC)/finiteVolume/lnInclude \
-I$(LIB_SRC)/turbulenceModels \
-I$(LIB_SRC)/transportModels
EXE_LIBS = \
-lincompressibleTurbulenceModels \
-lincompressibleTransportModels \
-lfiniteVolume \
-lmeshTools

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Info << "Reading field p\n" << endl;
volScalarField p
(
IOobject
(
"p",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
Info<< "Reading field Urel\n" << endl;
volVectorField Urel
(
IOobject
(
"Urel",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
// Create absolute velocity field (post-processing only)
// Will be updated before first use, so can be initialised by Urel
Info<< "Creating field Uabs\n" << endl;
volVectorField Uabs
(
IOobject
(
"Uabs",
runTime.timeName(),
mesh,
IOobject::NO_READ,
IOobject::AUTO_WRITE
),
Urel
);
Info<< "Reading/calculating face flux field phi\n" << endl;
surfaceScalarField phi
(
IOobject
(
"phi",
runTime.timeName(),
mesh,
IOobject::READ_IF_PRESENT,
IOobject::AUTO_WRITE
),
linearInterpolate(Urel) & mesh.Sf()
);
label pRefCell = 0;
scalar pRefValue = 0.0;
setRefCell(p, mesh.solutionDict().subDict("SIMPLE"), pRefCell, pRefValue);
singlePhaseTransportModel laminarTransport(Urel, phi);
autoPtr<turbulenceModel> turbulence
(
turbulenceModel::New(Urel, phi, laminarTransport)
);
Info<< "Creating SRF model\n" << endl;
autoPtr<SRF::SRFModel> SRF
(
SRF::SRFModel::New(Urel)
);

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@ -0,0 +1,130 @@
/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 1991-2007 OpenCFD Ltd.
\\/ 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 2 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, write to the Free Software Foundation,
Inc., 51 Franklin St, Fifth Floor, Boston, MA 02110-1301 USA
Application
simpleSRFFoam
Description
Steady-state solver for incompressible, turbulent flow of non-Newtonian
fluids with single rotating frame.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "incompressible/singlePhaseTransportModel/singlePhaseTransportModel.H"
#include "incompressible/turbulenceModel/turbulenceModel.H"
#include "SRFModel.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
# include "setRootCase.H"
# include "createTime.H"
# include "createMesh.H"
# include "createFields.H"
# include "initContinuityErrs.H"
//mesh.clearPrimitives();
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
for (runTime++; !runTime.end(); runTime++)
{
Info<< "Time = " << runTime.timeName() << nl << endl;
# include "readSIMPLEControls.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();
}
turbulence->correct();
Uabs = Urel + SRF->U();
runTime.write();
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< nl << endl;
}
Info<< "End\n" << endl;
return(0);
}
// ************************************************************************* //