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Merge commit 'OpenCFD/master' into olesenm

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This commit is contained in:
Mark Olesen
2008-06-26 14:08:49 +02:00
parent 7f4a999257 0d45add454
commit 69bcc1baad
89 changed files with 3755 additions and 44940 deletions
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3939
tutorials/gnemdFoam/constrictedChannel/constant/polyMesh/cellZones
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tutorials/gnemdFoam/constrictedChannel/constant/polyMesh/faces
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tutorials/gnemdFoam/constrictedChannel/constant/polyMesh/neighbour
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tutorials/gnemdFoam/constrictedChannel/constant/polyMesh/owner
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tutorials/gnemdFoam/constrictedChannel/constant/polyMesh/points
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tutorials/lesCavitatingFoam/Allclean Executable file
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#!/bin/sh
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
cd throttle
rm -rf constant/polyMesh/sets > /dev/null 2>&1
rm -rf 0/polyMesh > /dev/null 2>&1
rm system/cellSetDict > /dev/null 2>&1
cleanCase
cd ..
cd throttle3D
rm -rf constant/polyMesh/sets > /dev/null 2>&1
rm -rf 0 > /dev/null 2>&1
cp -r 0.orig 0
rm system/cellSetDict > /dev/null 2>&1
rm -rf processor[0-9] > /dev/null 2>&1
cleanCase
cd ..

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tutorials/lesCavitatingFoam/Allrun Executable file
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#!/bin/sh
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
application="lesCavitatingFoam"
refineMeshByCellSet()
{
echo "creating cell set for primary zone - $1"
cp system/cellSetDict.$1 system/cellSetDict
cellSet >& log.cellSet.$1
echo "refining primary zone - $1"
refineMesh -dict -overwrite >& log.refineMesh.$1
}
cd throttle
runApplication blockMesh
refineMeshByCellSet 1
refineMeshByCellSet 2
refineMeshByCellSet 3
runApplication $application
cd ..
cd throttle3D
cp -r 0.orig 0
runApplication blockMesh
refineMeshByCellSet 1
refineMeshByCellSet 2
refineMeshByCellSet 3
echo "mapping fields from 2D throttle case"
mapFields ../throttle -sourceTime latestTime >& log.mapFields
runApplication decomposePar
hostname > system/machines
runParallel $application 4 system/machines
runApplication reconstructPar
cd ..

47
tutorials/lesCavitatingFoam/throttle/0/U Normal file
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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];
internalField uniform (0 0 0);
boundaryField
{
inlet
{
type zeroGradient;
value uniform (0 0 0);
}
outlet
{
type zeroGradient;
value uniform (0 0 0);
}
walls
{
type fixedValue;
value uniform (0 0 0);
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

47
tutorials/lesCavitatingFoam/throttle/0/gamma Normal file
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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 gamma;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
walls
{
type calculated;
value uniform 0;
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

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tutorials/lesCavitatingFoam/throttle/0/k Normal file
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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];
internalField uniform 10.0;
boundaryField
{
inlet
{
type fixedValue;
value uniform 0.5;
}
outlet
{
type zeroGradient;
}
walls
{
type zeroGradient;
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

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tutorials/lesCavitatingFoam/throttle/0/nuSgs Normal file
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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 binary;
class volScalarField;
object nuSgs;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 1e-11;
boundaryField
{
inlet
{
type zeroGradient;
}
outlet
{
type zeroGradient;
}
walls
{
type fixedValue;
value uniform 0;
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

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tutorials/lesCavitatingFoam/throttle/0/p Normal file
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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 [1 -1 -2 0 0];
internalField uniform 300e5;
boundaryField
{
inlet
{
type totalPressure;
U U;
phi phiv;
rho rho;
psi none;
gamma 1;
p0 uniform 300e5;
}
outlet
{
type fixedValue;
value uniform 100e5;
}
walls
{
type zeroGradient;
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

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tutorials/lesCavitatingFoam/throttle/0/rho Normal file
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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 rho;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -3 0 0 0];
internalField uniform 845;
boundaryField
{
inlet
{
type fixedValue;
value uniform 845;
}
outlet
{
type fixedValue;
value uniform 835;
}
walls
{
type zeroGradient;
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

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tutorials/lesCavitatingFoam/throttle/constant/LESProperties Normal file
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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 LESProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
LESModel devOneEqEddy;
delta smooth;
laminarCoeffs
{
}
devOneEqEddyCoeffs
{
ck 0.07;
ce 1.05;
}
oneEqEddyCoeffs
{
ck 0.07;
ce 1.05;
}
dynOneEqEddyCoeffs
{
ce 1.05;
filter simple;
}
locDynOneEqEddyCoeffs
{
ce 1.05;
filter simple;
}
SmagorinskyCoeffs
{
ce 1.05;
ck 0.07;
}
Smagorinsky2Coeffs
{
ce 1.05;
ck 0.07;
cD2 0.02;
}
spectEddyViscCoeffs
{
ce 1.05;
cB 8.22;
cK1 0.83;
cK2 1.03;
cK3 4.75;
cK4 2.55;
}
dynSmagorinskyCoeffs
{
ce 1.05;
filter simple;
}
mixedSmagorinskyCoeffs
{
ce 1.05;
ck 0.07;
filter simple;
}
dynMixedSmagorinskyCoeffs
{
ce 1.05;
filter simple;
}
LRRDiffStressCoeffs
{
ce 1.05;
ck 0.09;
c1 1.8;
c2 0.6;
}
DeardorffDiffStressCoeffs
{
ce 1.05;
ck 0.09;
cm 4.13;
}
SpalartAllmarasCoeffs
{
alphaNut 1.5;
Cb1 0.1355;
Cb2 0.622;
Cw2 0.3;
Cw3 2;
Cv1 7.1;
Cv2 5.0;
CDES 0.65;
ck 0.07;
}
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;
}
kappa 0.4187;
wallFunctionCoeffs
{
E 9;
}
// ************************************************************************* //

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tutorials/lesCavitatingFoam/throttle/constant/polyMesh/blockMeshDict Normal file
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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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1.0e-3;
vertices
(
( 0.00 -2.50 -0.50)
( 5.00 -2.50 -0.50)
( 5.00 -0.15 -0.50)
( 7.00 -0.15 -0.50)
( 7.00 -2.50 -0.50)
(17.00 -2.50 -0.50)
(17.00 -0.15 -0.50)
(17.00 0.15 -0.50)
(17.00 2.50 -0.50)
( 7.00 2.50 -0.50)
( 7.00 0.15 -0.50)
( 5.00 0.15 -0.50)
( 5.00 2.50 -0.50)
( 0.00 2.50 -0.50)
( 0.00 0.15 -0.50)
( 0.00 -0.15 -0.50)
( 0.00 -2.50 0.50)
( 5.00 -2.50 0.50)
( 5.00 -0.15 0.50)
( 7.00 -0.15 0.50)
( 7.00 -2.50 0.50)
(17.00 -2.50 0.50)
(17.00 -0.15 0.50)
(17.00 0.15 0.50)
(17.00 2.50 0.50)
( 7.00 2.50 0.50)
( 7.00 0.15 0.50)
( 5.00 0.15 0.50)
( 5.00 2.50 0.50)
( 0.00 2.50 0.50)
( 0.00 0.15 0.50)
( 0.00 -0.15 0.50)
);
blocks
(
hex ( 0 1 2 15 16 17 18 31) ( 50 24 1) simpleGrading (1 1 1)
hex (15 2 11 14 31 18 27 30) ( 50 3 1) simpleGrading (1 1 1)
hex (14 11 12 13 30 27 28 29) ( 50 24 1) simpleGrading (1 1 1)
hex ( 2 3 10 11 18 19 26 27) ( 20 3 1) simpleGrading (1 1 1)
hex ( 4 5 6 3 20 21 22 19) (100 24 1) simpleGrading (1 1 1)
hex ( 3 6 7 10 19 22 23 26) (100 3 1) simpleGrading (1 1 1)
hex (10 7 8 9 26 23 24 25) (100 24 1) simpleGrading (1 1 1)
);
edges
(
);
patches
(
patch inlet
(
(15 0 16 31)
(14 15 31 30)
(13 14 30 29)
)
patch outlet
(
( 5 6 22 21)
( 6 7 23 22)
( 7 8 24 23)
)
wall walls
(
( 1 0 16 17)
( 2 1 17 18)
( 3 2 18 19)
( 4 3 19 20)
( 5 4 20 21)
( 9 8 24 25)
(10 9 25 26)
(11 10 26 27)
(12 11 27 28)
(13 12 28 29)
)
empty frontBack
(
( 0 15 2 1)
(15 14 11 2)
(14 13 12 11)
( 2 11 10 3)
( 4 3 6 5)
( 3 10 7 6)
(10 9 8 7)
(16 17 18 31)
(31 18 27 30)
(30 27 28 29)
(18 19 26 27)
(20 21 22 19)
(19 22 23 26)
(26 23 24 25)
)
);
// ************************************************************************* //

45
tutorials/lesCavitatingFoam/throttle/constant/polyMesh/boundary Normal file
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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 binary;
class polyBoundaryMesh;
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
4
(
inlet
{
type patch;
nFaces 51;
startFace 15151;
}
outlet
{
type patch;
nFaces 51;
startFace 15202;
}
walls
{
type wall;
nFaces 436;
startFace 15253;
}
frontBack
{
type empty;
nFaces 15420;
startFace 15689;
}
)
// ************************************************************************* //

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tutorials/lesCavitatingFoam/throttle/constant/thermodynamicProperties Normal file
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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 thermodynamicProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
barotropicCompressibilityModel linear; //Chung;
psiv psiv [0 -2 2 0 0] 2.5e-06;
rholSat rholSat [1 -3 0 0 0] 830;
psil psil [0 -2 2 0 0] 5e-07;
pSat pSat [1 -1 -2 0 0] 4500;
rhoMin rhoMin [1 -3 0 0 0] 0.001;
// ************************************************************************* //

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tutorials/lesCavitatingFoam/throttle/constant/transportProperties Normal file
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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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
mul mul [1 -1 -1 0 0] 6.500e-03;
muv muv [1 -1 -1 0 0] 5.953e-06;
twoPhase
{
transportModel twoPhase;
phase1 phase1;
phase2 phase2;
}
phase1
{
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 7.831e-06;
rho rho [1 -3 0 0 0 0 0] 830;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
m m [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
k k [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
}
phase2
{
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 4.252e-05;
rho rho [1 -3 0 0 0 0 0] 0.14;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
m m [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
k k [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
}
// ************************************************************************* //

29
tutorials/lesCavitatingFoam/throttle/system/cellSetDict.1 Normal file
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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 cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name c0;
action new;
topoSetSources
(
boxToCell
{
box (4e-03 -1e-03 -1) (12e-3 1e-03 1);
}
);
// ************************************************************************* //

29
tutorials/lesCavitatingFoam/throttle/system/cellSetDict.2 Normal file
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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 cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name c0;
action new;
topoSetSources
(
boxToCell
{
box (4.5e-03 -0.75e-03 -1) (9.5e-3 0.75e-03 1);
}
);
// ************************************************************************* //

29
tutorials/lesCavitatingFoam/throttle/system/cellSetDict.3 Normal file
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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 cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name c0;
action new;
topoSetSources
(
boxToCell
{
box (4.75e-03 -0.375e-03 -1) (9e-03 0.375e-03 1);
}
);
// ************************************************************************* //

86
tutorials/lesCavitatingFoam/throttle/system/controlDict Normal file
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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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 2e-3;
deltaT 1e-8;
writeControl adjustableRunTime;
writeInterval 1e-4;
purgeWrite 0;
writeFormat binary;
writePrecision 6;
writeCompression compressed;
timeFormat general;
runTimeModifiable yes;
adjustTimeStep on;
maxCo 0.5;
maxAcousticCo 50.0;
functions
(
/*
fieldAverage1
{
// Type of functionObject
type fieldAverage;
// Where to load it from (if not already in solver)
functionObjectLibs ("libfieldAverage.so");
// Fields to be probed. runTime modifiable!
fields
(
U
{
mean on;
prime2Mean off;
base time;
}
p
{
mean on;
prime2Mean off;
base time;
}
gamma
{
mean on;
prime2Mean off;
base time;
}
);
}
*/
);
// ************************************************************************* //

70
tutorials/lesCavitatingFoam/throttle/system/fvSchemes Normal file
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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;
}
interpolationSchemes
{
default linear;
}
divSchemes
{
default none;
// div(phiv,rho) Gauss upwind;
// div(phi,U) Gauss upwind;
// div(phiv,k) Gauss upwind;
div(phiv,rho) Gauss limitedLinear 0.2;
div(phi,U) Gauss filteredLinear2V 0.2 0;
div(phiv,k) Gauss filteredLinear2 0.2 0;
}
gradSchemes
{
default Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuf,rhoU) Gauss linear corrected;
laplacian(muEff,U) Gauss linear corrected;
laplacian(rrhoUAf,p) Gauss linear corrected;
laplacian(rUAf,p) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(1,p) Gauss linear corrected;
}
snGradSchemes
{
default none;
snGrad(p) corrected;
}
fluxRequired
{
default none;
p;
rho;
}
// ************************************************************************* //

77
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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
{
omega PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
k PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
rho PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
U PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
p GAMG
{
tolerance 1e-8;
relTol 0;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
cacheAgglomeration true;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
};
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
// removeSwirl 2;
}
SIMPLE
{
}
// ************************************************************************* //

39
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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 refineMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
set c0;
coordinateSystem global;
globalCoeffs
{
tan1 (1 0 0);
tan2 (0 1 0);
}
directions
(
tan1
tan2
);
useHexTopology yes;
geometricCut no;
writeMesh no;
// ************************************************************************* //

48
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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];
internalField uniform (0 0 0);
boundaryField
{
inlet
{
type zeroGradient;
value uniform (0 0 0);
}
outlet
{
type zeroGradient;
value uniform (0 0 0);
}
walls
{
type fixedValue;
value uniform (0 0 0);
}
frontBack
{
type fixedValue;
value uniform (0 0 0);
}
}
// ************************************************************************* //

48
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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 gamma;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
walls
{
type calculated;
value uniform 0;
}
frontBack
{
type calculated;
value uniform 0;
}
}
// ************************************************************************* //

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tutorials/lesCavitatingFoam/throttle3D/0/k Normal file
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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];
internalField uniform 10.0;
boundaryField
{
inlet
{
type fixedValue;
value uniform 0.5;
}
outlet
{
type zeroGradient;
}
walls
{
type zeroGradient;
}
frontBack
{
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 binary;
class volScalarField;
object nuSgs;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 1e-11;
boundaryField
{
inlet
{
type zeroGradient;
}
outlet
{
type zeroGradient;
}
walls
{
type fixedValue;
value uniform 0;
}
frontBack
{
type fixedValue;
value uniform 0;
}
}
// ************************************************************************* //

51
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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 [1 -1 -2 0 0];
internalField uniform 300e5;
boundaryField
{
inlet
{
type totalPressure;
U U;
phi phiv;
rho rho;
psi none;
gamma 1;
p0 uniform 300e5;
}
outlet
{
type fixedValue;
value uniform 100e5;
}
walls
{
type zeroGradient;
}
frontBack
{
type zeroGradient;
}
}
// ************************************************************************* //

46
tutorials/lesCavitatingFoam/throttle3D/0/rho Normal file
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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 rho;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -3 0 0 0];
internalField uniform 845;
boundaryField
{
inlet
{
type fixedValue;
value uniform 845;
}
outlet
{
type fixedValue;
value uniform 835;
}
walls
{
type zeroGradient;
}
frontBack
{
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 dictionary;
object LESProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
LESModel devOneEqEddy;
delta smooth;
laminarCoeffs
{
}
devOneEqEddyCoeffs
{
ck 0.07;
ce 1.05;
}
oneEqEddyCoeffs
{
ck 0.07;
ce 1.05;
}
dynOneEqEddyCoeffs
{
ce 1.05;
filter simple;
}
locDynOneEqEddyCoeffs
{
ce 1.05;
filter simple;
}
SmagorinskyCoeffs
{
ce 1.05;
ck 0.07;
}
Smagorinsky2Coeffs
{
ce 1.05;
ck 0.07;
cD2 0.02;
}
spectEddyViscCoeffs
{
ce 1.05;
cB 8.22;
cK1 0.83;
cK2 1.03;
cK3 4.75;
cK4 2.55;
}
dynSmagorinskyCoeffs
{
ce 1.05;
filter simple;
}
mixedSmagorinskyCoeffs
{
ce 1.05;
ck 0.07;
filter simple;
}
dynMixedSmagorinskyCoeffs
{
ce 1.05;
filter simple;
}
LRRDiffStressCoeffs
{
ce 1.05;
ck 0.09;
c1 1.8;
c2 0.6;
}
DeardorffDiffStressCoeffs
{
ce 1.05;
ck 0.09;
cm 4.13;
}
SpalartAllmarasCoeffs
{
alphaNut 1.5;
Cb1 0.1355;
Cb2 0.622;
Cw2 0.3;
Cw3 2;
Cv1 7.1;
Cv2 5.0;
CDES 0.65;
ck 0.07;
}
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;
}
kappa 0.4187;
wallFunctionCoeffs
{
E 9;
}
// ************************************************************************* //

121
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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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1.0e-3;
vertices
(
( 0.00 -2.50 -0.50)
( 5.00 -2.50 -0.50)
( 5.00 -0.15 -0.50)
( 7.00 -0.15 -0.50)
( 7.00 -2.50 -0.50)
(17.00 -2.50 -0.50)
(17.00 -0.15 -0.50)
(17.00 0.15 -0.50)
(17.00 2.50 -0.50)
( 7.00 2.50 -0.50)
( 7.00 0.15 -0.50)
( 5.00 0.15 -0.50)
( 5.00 2.50 -0.50)
( 0.00 2.50 -0.50)
( 0.00 0.15 -0.50)
( 0.00 -0.15 -0.50)
( 0.00 -2.50 0.50)
( 5.00 -2.50 0.50)
( 5.00 -0.15 0.50)
( 7.00 -0.15 0.50)
( 7.00 -2.50 0.50)
(17.00 -2.50 0.50)
(17.00 -0.15 0.50)
(17.00 0.15 0.50)
(17.00 2.50 0.50)
( 7.00 2.50 0.50)
( 7.00 0.15 0.50)
( 5.00 0.15 0.50)
( 5.00 2.50 0.50)
( 0.00 2.50 0.50)
( 0.00 0.15 0.50)
( 0.00 -0.15 0.50)
);
blocks
(
hex ( 0 1 2 15 16 17 18 31) ( 50 24 10) simpleGrading (1 1 1)
hex (15 2 11 14 31 18 27 30) ( 50 3 10) simpleGrading (1 1 1)
hex (14 11 12 13 30 27 28 29) ( 50 24 10) simpleGrading (1 1 1)
hex ( 2 3 10 11 18 19 26 27) ( 20 3 10) simpleGrading (1 1 1)
hex ( 4 5 6 3 20 21 22 19) (100 24 10) simpleGrading (1 1 1)
hex ( 3 6 7 10 19 22 23 26) (100 3 10) simpleGrading (1 1 1)
hex (10 7 8 9 26 23 24 25) (100 24 10) simpleGrading (1 1 1)
);
edges
(
);
patches
(
patch inlet
(
(15 0 16 31)
(14 15 31 30)
(13 14 30 29)
)
patch outlet
(
( 5 6 22 21)
( 6 7 23 22)
( 7 8 24 23)
)
wall walls
(
( 1 0 16 17)
( 2 1 17 18)
( 3 2 18 19)
( 4 3 19 20)
( 5 4 20 21)
( 9 8 24 25)
(10 9 25 26)
(11 10 26 27)
(12 11 27 28)
(13 12 28 29)
)
wall frontBack
(
( 0 15 2 1)
(15 14 11 2)
(14 13 12 11)
( 2 11 10 3)
( 4 3 6 5)
( 3 10 7 6)
(10 9 8 7)
(16 17 18 31)
(31 18 27 30)
(30 27 28 29)
(18 19 26 27)
(20 21 22 19)
(19 22 23 26)
(26 23 24 25)
)
);
// ************************************************************************* //

45
tutorials/lesCavitatingFoam/throttle3D/constant/polyMesh/boundary Normal file
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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 binary;
class polyBoundaryMesh;
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
4
(
inlet
{
type patch;
nFaces 510;
startFace 220900;
}
outlet
{
type patch;
nFaces 510;
startFace 221410;
}
walls
{
type wall;
nFaces 4360;
startFace 221920;
}
frontBack
{
type wall;
nFaces 15420;
startFace 226280;
}
)
// ************************************************************************* //

29
tutorials/lesCavitatingFoam/throttle3D/constant/thermodynamicProperties Normal file
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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 thermodynamicProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
barotropicCompressibilityModel linear; //Chung;
psiv psiv [0 -2 2 0 0] 2.5e-06;
rholSat rholSat [1 -3 0 0 0] 830;
psil psil [0 -2 2 0 0] 5e-07;
pSat pSat [1 -1 -2 0 0] 4500;
rhoMin rhoMin [1 -3 0 0 0] 0.001;
// ************************************************************************* //

69
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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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
mul mul [1 -1 -1 0 0] 6.500e-03;
muv muv [1 -1 -1 0 0] 5.953e-06;
twoPhase
{
transportModel twoPhase;
phase1 phase1;
phase2 phase2;
}
phase1
{
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 7.831e-06;
rho rho [1 -3 0 0 0 0 0] 830;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
m m [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
k k [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
}
phase2
{
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 4.252e-05;
rho rho [1 -3 0 0 0 0 0] 0.14;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
m m [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
k k [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
}
// ************************************************************************* //

29
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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 cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name c0;
action new;
topoSetSources
(
boxToCell
{
box (4e-03 -1e-03 -1) (12e-3 1e-03 1);
}
);
// ************************************************************************* //

29
tutorials/lesCavitatingFoam/throttle3D/system/cellSetDict.2 Normal file
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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 cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name c0;
action new;
topoSetSources
(
boxToCell
{
box (4.5e-03 -0.75e-03 -1) (9.5e-3 0.75e-03 1);
}
);
// ************************************************************************* //

29
tutorials/lesCavitatingFoam/throttle3D/system/cellSetDict.3 Normal file
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@ -0,0 +1,29 @@
/*--------------------------------*- 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 cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name c0;
action new;
topoSetSources
(
boxToCell
{
box (4.75e-03 -0.375e-03 -1) (9e-03 0.375e-03 1);
}
);
// ************************************************************************* //

86
tutorials/lesCavitatingFoam/throttle3D/system/controlDict Normal file
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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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 1e-4;
deltaT 1e-8;
writeControl adjustableRunTime;
writeInterval 5e-6;
purgeWrite 0;
writeFormat binary;
writePrecision 6;
writeCompression compressed;
timeFormat general;
runTimeModifiable yes;
adjustTimeStep on;
maxCo 0.5;
maxAcousticCo 50.0;
functions
(
/*
fieldAverage1
{
// Type of functionObject
type fieldAverage;
// Where to load it from (if not already in solver)
functionObjectLibs ("libfieldAverage.so");
// Fields to be probed. runTime modifiable!
fields
(
U
{
mean on;
prime2Mean off;
base time;
}
p
{
mean on;
prime2Mean off;
base time;
}
gamma
{
mean on;
prime2Mean off;
base time;
}
);
}
*/
);
// ************************************************************************* //

56
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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 decomposeParDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
numberOfSubdomains 4;
method simple;
simpleCoeffs
{
n (2 2 1);
delta 0.001;
}
hierarchicalCoeffs
{
n (1 1 1);
delta 0.001;
order xyz;
}
metisCoeffs
{
processorWeights
(
1
1
1
1
);
}
manualCoeffs
{
dataFile "";
}
distributed no;
roots
(
);
// ************************************************************************* //

70
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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;
}
interpolationSchemes
{
default linear;
}
divSchemes
{
default none;
// div(phiv,rho) Gauss upwind;
// div(phi,U) Gauss upwind;
// div(phiv,k) Gauss upwind;
div(phiv,rho) Gauss limitedLinear 0.2;
div(phi,U) Gauss filteredLinear2V 0.2 0;
div(phiv,k) Gauss filteredLinear2 0.2 0;
}
gradSchemes
{
default Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuf,rhoU) Gauss linear corrected;
laplacian(muEff,U) Gauss linear corrected;
laplacian(rrhoUAf,p) Gauss linear corrected;
laplacian(rUAf,p) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(1,p) Gauss linear corrected;
}
snGradSchemes
{
default none;
snGrad(p) corrected;
}
fluxRequired
{
default none;
p;
rho;
}
// ************************************************************************* //

77
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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
{
omega PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
k PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
rho PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
U PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
p GAMG
{
tolerance 1e-8;
relTol 0;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
cacheAgglomeration true;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
};
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
// removeSwirl 2;
}
SIMPLE
{
}
// ************************************************************************* //

1
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shelob

25
tutorials/lesCavitatingFoam/throttle3D/system/mapFieldsDict Normal file
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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 mapFieldsDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
patchMap
(
);
cuttingPatches
(
);
// ************************************************************************* //

41
tutorials/lesCavitatingFoam/throttle3D/system/refineMeshDict Normal file
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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 refineMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
set c0;
coordinateSystem global;
globalCoeffs
{
tan1 (1 0 0);
tan2 (0 1 0);
tan3 (0 0 1);
}
directions
(
tan1
tan2
tan3
);
useHexTopology yes;
geometricCut no;
writeMesh no;
// ************************************************************************* //

151
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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 sampleDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// interpolationScheme : choice of
// cell : use cell-centre value only; constant over cells
// cellPoint : use cell-centre and vertex values
// cellPointFace : use cell-centre, vertex and face values.
// 1] vertex values determined from neighbouring cell-centre values
// 2] face values determined using the current face interpolation scheme
// for the field (linear, gamma, etc.)
interpolationScheme cellPointFace;
// setFormat : choice of
// xmgr
// jplot
// gnuplot
// raw
setFormat raw;
// Surface output format. Choice of
// null : suppress output
// foamFile : separate points, faces and values file
// dx : DX scalar or vector format
// vtk : VTK ascii format
// raw : x y z value format for use with e.g. gnuplot 'splot'.
// stl : ascii stl. Does not contain values!
surfaceFormat vtk;
// sampling definition:
//
// Dictionary with fields
// type : type of sampling method
// name : name of samples. Used e.g. as filename
// axis : how to write point coordinate
// ... : depending on method
//
//
// sample: choice of
// uniform evenly distributed points on line
// face one point per face intersection
// midPoint one point per cell, inbetween two face intersections
// midPointAndFace combination of face and midPoint
//
// curve specified points, not nessecary on line, uses
// tracking
// cloud specified points, uses findCell
//
//
// axis: how to write point coordinate. Choice of
// - x/y/z: x/y/z coordinate only
// - xyz: three columns
// (probably does not make sense for anything but raw)
// - distance: distance from start of sampling line (if uses line) or
// distance from first specified sampling point
//
// type specific:
// uniform, face, midPoint, midPointAndFace : start and end coordinate
// uniform: extra number of sampling points
// curve, cloud: list of coordinates
sets
(
IN1
{
type uniform;
axis y;
start (11.8224e-3 -1.0e-3 1.0e-8);
end (11.8224e-3 1.0e-3 1.0e-8);
nPoints 100;
}
IN
{
type uniform;
axis y;
start (12.0864e-3 -1.0e-3 1.0e-8);
end (12.0864e-3 1.0e-3 1.0e-8);
nPoints 50;
}
M1
{
type uniform;
axis y;
start (12.3424e-3 -0.147539e-3 1.0e-8);
end (12.3424e-3 0.147539e-3 1.0e-8);
nPoints 50;
}
M2
{
type uniform;
axis y;
start (12.6032e-3 -0.147539e-3 1.0e-8);
end (12.6032e-3 0.147539e-3 1.0e-8);
nPoints 50;
}
OUT
{
type uniform;
axis y;
start (12.8928e-3 -0.147539e-3 1.0e-8);
end (12.8928e-3 0.147539e-3 1.0e-8);
nPoints 50;
}
IN1_GR1
{
type uniform;
axis y;
start (11.778e-3 -1.0e-3 1.0e-8);
end (11.778e-3 1.0e-3 1.0e-8);
nPoints 100;
}
OUT_GR1
{
type uniform;
axis y;
start (13.14e-3 -2.0e-3 1.0e-8);
end (13.14e-3 2.0e-3 1.0e-8);
nPoints 200;
}
);
surfaces
();
// Fields to sample.
fields
(
// magUMean
UMeanx
);
// ************************************************************************* //

47
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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];
internalField uniform (0 0 0);
boundaryField
{
inlet
{
type zeroGradient;
value uniform (0 0 0);
}
outlet
{
type zeroGradient;
value uniform (0 0 0);
}
walls
{
type fixedValue;
value uniform (0 0 0);
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

47
tutorials/rasCavitatingFoam/0/gamma Normal file
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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 gamma;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
walls
{
type calculated;
value uniform 0;
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

46
tutorials/rasCavitatingFoam/0/k Normal file
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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];
internalField uniform 10.0;
boundaryField
{
inlet
{
type turbulentIntensityKineticEnergyInlet;
intensity 0.05;
value uniform 0.05;
}
outlet
{
type zeroGradient;
}
walls
{
type zeroGradient;
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

47
tutorials/rasCavitatingFoam/0/omega Normal file
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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 omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 -1 0 0];
internalField uniform 77200;
boundaryField
{
inlet
{
type turbulentMixingLengthFrequencyInlet;
mixingLength 0.5e-03;
k k;
value uniform 77200;
}
outlet
{
type zeroGradient;
}
walls
{
type zeroGradient;
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

51
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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 [1 -1 -2 0 0];
internalField uniform 300e5;
boundaryField
{
inlet
{
type totalPressure;
U U;
phi phiv;
rho rho;
psi none;
gamma 1;
p0 uniform 300e5;
}
outlet
{
type fixedValue;
value uniform 100e5;
}
walls
{
type zeroGradient;
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

46
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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 rho;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -3 0 0 0];
internalField uniform 845;
boundaryField
{
inlet
{
type fixedValue;
value uniform 845;
}
outlet
{
type fixedValue;
value uniform 835;
}
walls
{
type zeroGradient;
}
frontBack
{
type empty;
}
}
// ************************************************************************* //

9
tutorials/rasCavitatingFoam/Allclean Executable file
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#!/bin/sh
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
rm -rf constant/polyMesh/sets > /dev/null 2>&1
rm -rf 0/polyMesh > /dev/null 2>&1
rm system/cellSetDict > /dev/null 2>&1
cleanCase

29
tutorials/rasCavitatingFoam/Allrun Executable file
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#!/bin/sh
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
application="rasCavitatingFoam"
refineMeshByCellSet()
{
echo "creating cell set for primary zone - $1"
cp system/cellSetDict.$1 system/cellSetDict
cellSet >& log.cellSet.$1
echo "refining primary zone - $1"
refineMesh -dict >& log.refineMesh.$1
rm -rf 0/polyMesh
mv 1e-08/polyMesh 0/
rm -rf 1e-08
}
runApplication blockMesh
refineMeshByCellSet 1
refineMeshByCellSet 2
refineMeshByCellSet 3
runApplication $application

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tutorials/rasCavitatingFoam/constant/RASProperties Normal file
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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 kOmegaSST;
turbulence on;
laminarCoeffs
{
}
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;
}
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;
}
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;
}
// ************************************************************************* //

121
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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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1.0e-3;
vertices
(
( 0.00 -2.50 -0.50)
( 5.00 -2.50 -0.50)
( 5.00 -0.15 -0.50)
( 7.00 -0.15 -0.50)
( 7.00 -2.50 -0.50)
(17.00 -2.50 -0.50)
(17.00 -0.15 -0.50)
(17.00 0.15 -0.50)
(17.00 2.50 -0.50)
( 7.00 2.50 -0.50)
( 7.00 0.15 -0.50)
( 5.00 0.15 -0.50)
( 5.00 2.50 -0.50)
( 0.00 2.50 -0.50)
( 0.00 0.15 -0.50)
( 0.00 -0.15 -0.50)
( 0.00 -2.50 0.50)
( 5.00 -2.50 0.50)
( 5.00 -0.15 0.50)
( 7.00 -0.15 0.50)
( 7.00 -2.50 0.50)
(17.00 -2.50 0.50)
(17.00 -0.15 0.50)
(17.00 0.15 0.50)
(17.00 2.50 0.50)
( 7.00 2.50 0.50)
( 7.00 0.15 0.50)
( 5.00 0.15 0.50)
( 5.00 2.50 0.50)
( 0.00 2.50 0.50)
( 0.00 0.15 0.50)
( 0.00 -0.15 0.50)
);
blocks
(
hex ( 0 1 2 15 16 17 18 31) ( 50 24 1) simpleGrading (1 1 1)
hex (15 2 11 14 31 18 27 30) ( 50 3 1) simpleGrading (1 1 1)
hex (14 11 12 13 30 27 28 29) ( 50 24 1) simpleGrading (1 1 1)
hex ( 2 3 10 11 18 19 26 27) ( 20 3 1) simpleGrading (1 1 1)
hex ( 4 5 6 3 20 21 22 19) (100 24 1) simpleGrading (1 1 1)
hex ( 3 6 7 10 19 22 23 26) (100 3 1) simpleGrading (1 1 1)
hex (10 7 8 9 26 23 24 25) (100 24 1) simpleGrading (1 1 1)
);
edges
(
);
patches
(
patch inlet
(
(15 0 16 31)
(14 15 31 30)
(13 14 30 29)
)
patch outlet
(
( 5 6 22 21)
( 6 7 23 22)
( 7 8 24 23)
)
wall walls
(
( 1 0 16 17)
( 2 1 17 18)
( 3 2 18 19)
( 4 3 19 20)
( 5 4 20 21)
( 9 8 24 25)
(10 9 25 26)
(11 10 26 27)
(12 11 27 28)
(13 12 28 29)
)
empty frontBack
(
( 0 15 2 1)
(15 14 11 2)
(14 13 12 11)
( 2 11 10 3)
( 4 3 6 5)
( 3 10 7 6)
(10 9 8 7)
(16 17 18 31)
(31 18 27 30)
(30 27 28 29)
(18 19 26 27)
(20 21 22 19)
(19 22 23 26)
(26 23 24 25)
)
);
// ************************************************************************* //

45
tutorials/rasCavitatingFoam/constant/polyMesh/boundary Normal file
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@ -0,0 +1,45 @@
/*--------------------------------*- 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 polyBoundaryMesh;
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
4
(
inlet
{
type patch;
nFaces 51;
startFace 15151;
}
outlet
{
type patch;
nFaces 51;
startFace 15202;
}
walls
{
type wall;
nFaces 436;
startFace 15253;
}
frontBack
{
type empty;
nFaces 15420;
startFace 15689;
}
)
// ************************************************************************* //

29
tutorials/rasCavitatingFoam/constant/thermodynamicProperties Normal file
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@ -0,0 +1,29 @@
/*--------------------------------*- 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 thermodynamicProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
barotropicCompressibilityModel linear; //Chung;
psiv psiv [0 -2 2 0 0] 2.5e-06;
rholSat rholSat [1 -3 0 0 0] 830;
psil psil [0 -2 2 0 0] 5e-07;
pSat pSat [1 -1 -2 0 0] 4500;
rhoMin rhoMin [1 -3 0 0 0] 0.001;
// ************************************************************************* //

69
tutorials/rasCavitatingFoam/constant/transportProperties Normal file
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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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
mul mul [1 -1 -1 0 0] 6.500e-03;
muv muv [1 -1 -1 0 0] 5.953e-06;
twoPhase
{
transportModel twoPhase;
phase1 phase1;
phase2 phase2;
}
phase1
{
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 7.831e-06;
rho rho [1 -3 0 0 0 0 0] 830;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
m m [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
k k [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
}
phase2
{
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 4.252e-05;
rho rho [1 -3 0 0 0 0 0] 0.14;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
m m [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] -999;
nuInf nuInf [0 2 -1 0 0 0 0] -999;
k k [0 0 1 0 0 0 0] -999;
n n [0 0 0 0 0 0 0] -999;
}
}
// ************************************************************************* //

29
tutorials/rasCavitatingFoam/system/cellSetDict.1 Normal file
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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 cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name c0;
action new;
topoSetSources
(
boxToCell
{
box (4e-03 -1e-03 -1) (12e-3 1e-03 1);
}
);
// ************************************************************************* //

29
tutorials/rasCavitatingFoam/system/cellSetDict.2 Normal file
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@ -0,0 +1,29 @@
/*--------------------------------*- 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 cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name c0;
action new;
topoSetSources
(
boxToCell
{
box (4.5e-03 -0.75e-03 -1) (9.5e-3 0.75e-03 1);
}
);
// ************************************************************************* //

29
tutorials/rasCavitatingFoam/system/cellSetDict.3 Normal file
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@ -0,0 +1,29 @@
/*--------------------------------*- 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 cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name c0;
action new;
topoSetSources
(
boxToCell
{
box (4.75e-03 -0.375e-03 -1) (9e-03 0.375e-03 1);
}
);
// ************************************************************************* //

49
tutorials/rasCavitatingFoam/system/controlDict Normal file
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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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 2e-3;
deltaT 1e-8;
writeControl adjustableRunTime;
writeInterval 1e-4;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
runTimeModifiable yes;
adjustTimeStep on;
maxCo 0.5;
maxAcousticCo 50.0;
// ************************************************************************* //

68
tutorials/rasCavitatingFoam/system/fvSchemes Normal file
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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;
}
interpolationSchemes
{
default linear;
}
divSchemes
{
default none;
div(phiv,rho) Gauss limitedLinear 0.2;
div(phi,U) Gauss limitedLinearV 0.2;
div(phiv,omega) Gauss limitedLinear 0.2;
div(phiv,k) Gauss limitedLinear 0.2;
}
gradSchemes
{
default Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuf,rhoU) Gauss linear corrected;
laplacian(muEff,U) Gauss linear corrected;
laplacian(rrhoUAf,p) Gauss linear corrected;
laplacian(rUAf,p) Gauss linear corrected;
laplacian(DomegaEff,omega) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(1,p) Gauss linear corrected;
}
snGradSchemes
{
default none;
snGrad(p) corrected;
}
fluxRequired
{
default none;
p;
rho;
}
// ************************************************************************* //

75
tutorials/rasCavitatingFoam/system/fvSolution Normal file
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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
{
omega PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
k PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
rho PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
U PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
p GAMG
{
preconditioner 1e-5;
relTol 0;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
cacheAgglomeration true;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
};
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 1;
// removeSwirl 2;
}
SIMPLE
{}
// ************************************************************************* //

39
tutorials/rasCavitatingFoam/system/refineMeshDict Normal file
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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 refineMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
set c0;
coordinateSystem global;
globalCoeffs
{
tan1 (1 0 0);
tan2 (0 1 0);
}
directions
(
tan1
tan2
);
useHexTopology yes;
geometricCut no;
writeMesh no;
// ************************************************************************* //