Added OpenFoam running

This commit is contained in:
Edgar P. Burkhart 2022-01-23 12:27:04 +01:00
parent 3eb45ecc47
commit cfb19010a7
Signed by: edpibu
GPG key ID: 9833D3C5A25BD227
34 changed files with 3353 additions and 0 deletions

68
openfoam/artha/0.org/U Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.x |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
inlet
{
type waveVelocity;
waveDictName waveDict;
value uniform (0 0 0);
}
atmosphere
{
type pressureInletOutletVelocity;
value uniform (0 0 0);
}
"wall."
{
type fixedValue;
value uniform (0 0 0);
}
bathy
{
type fixedValue;
value uniform (0 0 0);
}
bloc0
{
type fixedValue;
value uniform (0 0 0);
}
bloc1
{
type fixedValue;
value uniform (0 0 0);
}
defaultFaces
{
type empty;
}
outlet
{
type waveAbsorption2DVelocity;
absorptionDir 666.0;
value uniform (0 0 0);
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5-dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object alpha.water;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type waveAlpha;
waveDictName waveDict;
value uniform 0;
}
outlet
{
type zeroGradient;
}
"wall."
{
type zeroGradient;
}
bathy
{
type zeroGradient;
}
bloc0
{
type zeroGradient;
}
bloc1
{
type zeroGradient;
}
defaultFaces
{
type empty;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5-dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object alpha.water;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type waveAlpha;
waveDictName waveDict;
value uniform 0;
}
outlet
{
type zeroGradient;
}
"wall."
{
type zeroGradient;
}
bathy
{
type zeroGradient;
}
bloc0
{
type zeroGradient;
}
bloc1
{
type zeroGradient;
}
defaultFaces
{
type empty;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.1.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 0.0001;
boundaryField
{
inlet
{
type inletOutlet;
inletValue uniform 0.0001;
value uniform 0.0001;
}
outlet
{
type inletOutlet;
inletValue uniform 0.0001;
value uniform 0.0001;
}
"wall."
{
type epsilonWallFunction;
value uniform 0.0001;
}
bathy
{
type epsilonWallFunction;
value uniform 0.0001;
}
bloc0
{
type epsilonWallFunction;
value uniform 0.0001;
}
bloc1
{
type epsilonWallFunction;
value uniform 0.0001;
}
defaultFaces
{
type empty;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0.0001;
value uniform 0.0001;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.1 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0.00000001;
boundaryField
{
inlet
{
type inletOutlet;
inletValue uniform 0.00000001;
value uniform 0.00000001;
}
outlet
{
type inletOutlet;
inletValue uniform 0.00000001;
value uniform 0.00000001;
}
"wall."
{
type kqRWallFunction;
value uniform 0.00000001;
}
bathy
{
type kqRWallFunction;
value uniform 0.00000001;
}
bloc0
{
type kqRWallFunction;
value uniform 0.00000001;
}
bloc1
{
type kqRWallFunction;
value uniform 0.00000001;
}
defaultFaces
{
type empty;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0.00000001;
value uniform 0.00000001;
}
}
// ************************************************************************* //

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openfoam/artha/0.org/nut Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 3.0.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
"wall."
{
type nutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
atmosphere
{
type calculated;
value uniform 0;
}
defaultFaces
{
type empty;
}
bathy
{
type nutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
bloc0
{
type nutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
bloc1
{
type nutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.1 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 -1 0 0 0 0];
internalField uniform 0.001;
boundaryField
{
inlet
{
type inletOutlet;
inletValue uniform 0.001;
value uniform 0.001;
}
outlet
{
type inletOutlet;
inletValue uniform 0.001;
value uniform 0.001;
}
"wall."
{
type omegaWallFunction;
value uniform 0.001;
}
bathy
{
type omegaWallFunction;
value uniform 0.001;
}
bloc0
{
type omegaWallFunction;
value uniform 0.001;
}
bloc1
{
type omegaWallFunction;
value uniform 0.001;
}
defaultFaces
{
type empty;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0.001;
value uniform 0.001;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5-dev |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p_rgh;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
"wall."
{
type fixedFluxPressure;
value uniform 0;
}
bathy
{
type fixedFluxPressure;
value uniform 0;
}
bloc0
{
type fixedFluxPressure;
value uniform 0;
}
bloc1
{
type fixedFluxPressure;
value uniform 0;
}
defaultFaces
{
type empty;
}
outlet
{
type fixedFluxPressure;
value uniform 0;
}
inlet
{
type fixedFluxPressure;
value uniform 0;
}
atmosphere
{
type totalPressure;
U U;
phi phi;
rho rho;
psi none;
gamma 1;
p0 uniform 0;
value uniform 0;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.1.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object porosityIndex;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type zeroGradient;
}
outlet
{
type zeroGradient;
}
"wall."
{
type zeroGradient;
}
bathy
{
type zeroGradient;
}
bloc0
{
type zeroGradient;
}
bloc1
{
type zeroGradient;
}
defaultFaces
{
type empty;
}
atmosphere
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.1.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object porosityIndex;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
inlet
{
type zeroGradient;
}
outlet
{
type zeroGradient;
}
"wall."
{
type zeroGradient;
}
bathy
{
type zeroGradient;
}
bloc0
{
type zeroGradient;
}
bloc1
{
type zeroGradient;
}
defaultFaces
{
type empty;
}
atmosphere
{
type zeroGradient;
}
}
// ************************************************************************* //

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#!/bin/bash
shopt -s extglob
directory=`pwd`
read -p "Clearing case. Are you sure? (y/N) " -n 1 -r
echo ' '
if ! [[ $REPLY =~ ^[Yy]$ ]]
then
exit
fi
if [ -d "./constant/polyMesh" ]; then
cd ./constant/polyMesh
rm -fr !(blockMeshDict)
cd $directory
fi
rm -fr *[0-9].[0-9]* [0-9] [1-9]* gaugesVOF gaugesP postProcessing processor*
rm -f *.log
#rm -f constant/turbulenceProperties

22
openfoam/artha/constant/g Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.1.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class uniformDimensionedVectorField;
location "constant";
object g;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -2 0 0 0 0];
value ( 0 0 -9.81 );
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.1.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object porosityDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Materials: clear region, core, secondary armour layer, primary armour layer
// a,b,c: tuning parameters
a 2(0 50);
b 2(0 1.2);
c 2(0 0.34);
// D50: mean nominal diameter
D50 2(1 4);
// porosity (phi)
porosity 2(1 0.5);
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 3.0.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
phases (water air);
water
{
transportModel Newtonian;
nu [0 2 -1 0 0 0 0] 1e-06;
rho [1 -3 0 0 0 0 0] 1000;
}
air
{
transportModel Newtonian;
nu [0 2 -1 0 0 0 0] 1.48e-05;
rho [1 -3 0 0 0 0 0] 1;
}
sigma [1 0 -2 0 0 0 0] 0.07;
// ************************************************************************* //

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endfacet
facet normal -0.189543 0 0.981872
outer loop
vertex 50.8798 10 -13.1112
vertex 50.8798 -10 -13.1112
vertex 51.0264 -10 -13.0829
endloop
endfacet
facet normal -0.179628 0 0.983735
outer loop
vertex 46.3343 10 -13.9412
vertex 50.8798 -10 -13.1112
vertex 50.8798 10 -13.1112
endloop
endfacet
facet normal -0.179628 0 0.983735
outer loop
vertex 46.3343 10 -13.9412
vertex 46.3343 -10 -13.9412
vertex 50.8798 -10 -13.1112
endloop
endfacet
facet normal -0.138489 0 0.990364
outer loop
vertex 46.1877 10 -13.9617
vertex 46.3343 -10 -13.9412
vertex 46.3343 10 -13.9412
endloop
endfacet
facet normal -0.138489 0 0.990364
outer loop
vertex 46.1877 10 -13.9617
vertex 46.1877 -10 -13.9617
vertex 46.3343 -10 -13.9412
endloop
endfacet
facet normal -0.13139 0 0.991331
outer loop
vertex 38.4164 10 -14.9917
vertex 46.1877 -10 -13.9617
vertex 46.1877 10 -13.9617
endloop
endfacet
facet normal -0.13139 0 0.991331
outer loop
vertex 38.4164 10 -14.9917
vertex 38.4164 -10 -14.9917
vertex 46.1877 -10 -13.9617
endloop
endfacet
facet normal -0 0 -1
outer loop
vertex 150 10 -14.9917
vertex 38.4164 -10 -14.9917
vertex 38.4164 10 -14.9917
endloop
endfacet
facet normal 0 -0 -1
outer loop
vertex 150 10 -14.9917
vertex 150 -10 -14.9917
vertex 38.4164 -10 -14.9917
endloop
endfacet
facet normal 1 0 0
outer loop
vertex 150 10 -5.02534
vertex 150 -10 -14.9917
vertex 150 10 -14.9917
endloop
endfacet
facet normal 1 0 0
outer loop
vertex 150 10 -5.02534
vertex 150 -10 -5.02534
vertex 150 -10 -14.9917
endloop
endfacet
endsolid OpenSCAD_Model

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@ -0,0 +1,29 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.1.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
RASModel kEpsilon;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

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@ -0,0 +1,29 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.1.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
RASModel kEpsilon;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.1.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
RASModel kOmegaSST;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.3 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object waveDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
waveType regular;
waveTheory cnoidal;
genAbs 1;
absDir 0.0;
nPaddles 1;
wavePeriod 20.0;
waveHeight 15.0;
waveDir 0.0;
wavePhase 0.;
tSmooth 0.0;
// ************************************************************************* //

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#!/bin/bash
set -e
cp constant/turbulenceProperties_keps constant/turbulenceProperties
echo blockMesh meshing...
blockMesh #> blockMesh.log
echo snappyHexMesh meshing...
snappyHexMesh -overwrite #> snappyHexMesh.log
echo Preparing 0 folder...
cp -r 0.org/ 0
echo Setting the fields...
setFields #> setFields.log
#olaFlow
echo Decomposing domain...
decomposePar #> decomposePar.log
echo Running...
mpirun -np 4 olaFlow -parallel #> olaFlow.log
echo Reconstructing domain...
reconstructPar
echo Simulation complete

26
openfoam/artha/runCaseSST Normal file
View file

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#!/bin/bash
mkdir -p 0
cp constant/turbulenceProperties_sst constant/turbulenceProperties
echo blockMesh meshing...
blockMesh #> blockMesh.log
echo snappyHexMesh meshing...
snappyHexMesh -overwrite #> snappyHexMesh.log
echo Preparing 0 folder...
rm -fr 0
cp -r 0.org 0
echo Setting the fields...
setFields #> setFields.log
echo Decomposing domain...
decomposePar #> decomposePar.log
echo Running...
mpirun -np 4 olaFlow -parallel #> olaFlow.log
echo Simulation complete

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.1 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
scale 1;
vertices
(
(0 0 -30)
(150 0 -30)
(150 0 20)
(0 0 20)
(0 1 -30)
(150 1 -30)
(150 1 20)
(0 1 20)
);
blocks
(
hex (0 1 5 4 3 2 6 7) (300 1 100) simpleGrading (1 1 1)
);
edges
(
);
boundary
(
inlet
{
type patch;
faces
(
(0 4 7 3)
);
}
outlet
{
type patch;
faces
(
(1 5 6 2)
);
}
wall1
{
type wall;
faces
(
(0 1 5 4)
);
}
atmosphere
{
type patch;
faces
(
(3 2 6 7)
);
}
);
mergePatchPairs
(
);
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.3 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
location "system";
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application olaFlow;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 1;
deltaT 0.05;
writeControl adjustableRunTime;
writeInterval 0.2;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
compression off;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep yes;
maxCo 0.45;
maxAlphaCo 0.45;
maxDeltaT 0.2;
/*
functions
{
gaugesVOF
{
type sets;
libs ("libsampling.so");
writeControl outputTime;
writeInterval 1;
setFormat raw;
surfaceFormat raw;
interpolationScheme cell;
fields ( alpha.water );
sets
(
GaugeVOF01
{
type lineCellFace;
axis xyz;
start ( 0.5 0.001 0 );
end ( 0.5 0.001 1.2 );
}
GaugeVOF02
{
type lineCellFace;
axis xyz;
start ( 9.25 0.001 0 );
end ( 9.25 0.001 1.2 );
}
GaugeVOF03
{
type lineCellFace;
axis xyz;
start ( 15.75 0.001 0 );
end ( 15.75 0.001 1.2 );
}
GaugeVOF04
{
type lineCellFace;
axis xyz;
start ( 17.75 0.001 0 );
end ( 17.75 0.001 1.2 );
}
GaugeVOF05
{
type lineCellFace;
axis xyz;
start ( 21.1 0.001 0 );
end ( 21.1 0.001 1.2 );
}
);
}
gaugesP
{
type sets;
libs ("libsampling.so");
writeControl outputTime;
writeInterval 1;
setFormat raw;
surfaceFormat raw;
interpolationScheme cellPointFace;
fields ( p );
sets
(
GaugesP
{
type boundaryPoints;
axis xyz;
patches 1(caisson);
points ((18.0 0.01 0.75)
(18.00 0.01 0.80)
(18.00 0.01 0.85)
(18.00 0.01 0.95)
(18.01 0.01 0.70)
(18.25 0.01 0.70)
(18.50 0.01 0.70)
(18.75 0.01 0.70));
maxDistance 0.01;
}
);
}
}
*/
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.3 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
location "system";
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 ();
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
div(rhoPhi,U) Gauss limitedLinearV 1;
div(U) Gauss linear;
div((rhoPhi|interpolate(porosity)),U) Gauss limitedLinearV 1;
div(rhoPhiPor,UPor) Gauss limitedLinearV 1;
div(rhoPhi,UPor) Gauss limitedLinearV 1;
div(rhoPhiPor,U) Gauss limitedLinearV 1;
div(phi,alpha) Gauss vanLeer;
div(phirb,alpha) Gauss interfaceCompression;
div((muEff*dev(T(grad(U))))) Gauss linear;
div(phi,k) Gauss upwind;
div(phi,epsilon) Gauss upwind;
div((phi|interpolate(porosity)),k) Gauss upwind;
div((phi*interpolate(rho)),k) Gauss upwind;
div((phi|interpolate(porosity)),epsilon) Gauss upwind;
div(phi,omega) Gauss upwind;
div((phi|interpolate(porosity)),omega) Gauss upwind;
div((phi*interpolate(rho)),omega) Gauss upwind;
div((phi*interpolate(rho)),epsilon) Gauss upwind;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p_rgh;
pcorr;
alpha.water;
}
wallDist
{
method meshWave;
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"alpha.water.*"
{
nAlphaCorr 1;
nAlphaSubCycles 2;
alphaOuterCorrectors yes;
cAlpha 1;
MULESCorr no;
nLimiterIter 3;
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-8;
relTol 0;
}
"pcorr.*"
{
solver PCG;
preconditioner DIC;
tolerance 1e-5;
relTol 0;
}
p_rgh
{
solver PCG;
preconditioner DIC;
tolerance 1e-07;
relTol 0.05;
}
p_rghFinal
{
$p_rgh;
relTol 0;
}
U
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-06;
relTol 0;
}
"(k|epsilon|omega|B|nuTilda).*"
{
solver smoothSolver;
smoother symGaussSeidel;
tolerance 1e-08;
relTol 0;
}
}
PIMPLE
{
momentumPredictor no;
nOuterCorrectors 1;
nCorrectors 3;
nNonOrthogonalCorrectors 0;
}
relaxationFactors
{
fields
{
}
equations
{
".*" 1;
}
}
// ************************************************************************* //

View file

@ -0,0 +1,53 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.3 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object setFieldsDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
defaultFieldValues
(
volScalarFieldValue alpha.water 0
volScalarFieldValue porosityIndex 0
);
regions
(
boxToCell
{
box (-10 -10 -100) (500 10 5);
fieldValues
(
volScalarFieldValue alpha.water 1
);
}
surfaceToCell
{
file "./constant/triSurface/rub.stl";
outsidePoints ((0 0 0)); // definition of outside
includeCut true; // cells cut by surface
includeInside true; // cells not on outside of surf
includeOutside false; // cells on outside of surf
nearDistance -1; // cells with centre near surf
// (set to -1 if not used)
curvature -100; // cells within nearDistance
// and near surf curvature
// (set to -100 if not used)
fieldValues
(
volScalarFieldValue porosityIndex 1
);
}
);

View file

@ -0,0 +1,359 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.7.1 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object snappyHexMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Which of the steps to run
castellatedMesh true;
snap false;
addLayers false;
// Geometry. Definition of all surfaces. All surfaces are of class
// searchableSurface.
// Surfaces are used
// - to specify refinement for any mesh cell intersecting it
// - to specify refinement for any mesh cell inside/outside/near
// - to 'snap' the mesh boundary to the surface
geometry
{
bloc0.stl
{
type triSurfaceMesh;
name bloc0;
}
bloc1.stl
{
type triSurfaceMesh;
name bloc1;
}
bathy.stl
{
type triSurfaceMesh;
name bathy;
}
};
// Settings for the castellatedMesh generation.
castellatedMeshControls
{
// Refinement parameters
// ~~~~~~~~~~~~~~~~~~~~~
// If local number of cells is >= maxLocalCells on any processor
// switches from from refinement followed by balancing
// (current method) to (weighted) balancing before refinement.
maxLocalCells 10000000;
// Overall cell limit (approximately). Refinement will stop immediately
// upon reaching this number so a refinement level might not complete.
// Note that this is the number of cells before removing the part which
// is not 'visible' from the keepPoint. The final number of cells might
// actually be a lot less.
maxGlobalCells 10000000;
// The surface refinement loop might spend lots of iterations refining just a
// few cells. This setting will cause refinement to stop if <= minimumRefine
// are selected for refinement. Note: it will at least do one iteration
// (unless the number of cells to refine is 0)
minRefinementCells 10;
// Allow a certain level of imbalance during refining
// (since balancing is quite expensive)
// Expressed as fraction of perfect balance (= overall number of cells /
// nProcs). 0=balance always.
maxLoadUnbalance 0.10;
// Number of buffer layers between different levels.
// 1 means normal 2:1 refinement restriction, larger means slower
// refinement.
nCellsBetweenLevels 3;
// Explicit feature edge refinement
// ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
// Specifies a level for any cell intersected by its edges.
// This is a featureEdgeMesh, read from constant/triSurface for now.
features
(
//{
// file "tanque.stl";
// level 2;
//}
);
// Surface based refinement
// ~~~~~~~~~~~~~~~~~~~~~~~~
// Specifies two levels for every surface. The first is the minimum level,
// every cell intersecting a surface gets refined up to the minimum level.
// The second level is the maximum level. Cells that 'see' multiple
// intersections where the intersections make an
// angle > resolveFeatureAngle get refined up to the maximum level.
refinementSurfaces
{
//caisson
//{
// // Surface-wise min and max refinement level
// level ( 1 1 );
//}
bathy
{
level ( 0 0 );
}
bloc0
{
level ( 0 0 );
}
bloc1
{
level ( 0 0 );
}
}
// Resolve sharp angles
resolveFeatureAngle 65;
// Region-wise refinement
// ~~~~~~~~~~~~~~~~~~~~~~
// Specifies refinement level for cells in relation to a surface. One of
// three modes
// - distance. 'levels' specifies per distance to the surface the
// wanted refinement level. The distances need to be specified in
// descending order.
// - inside. 'levels' is only one entry and only the level is used. All
// cells inside the surface get refined up to the level. The surface
// needs to be closed for this to be possible.
// - outside. Same but cells outside.
refinementRegions
{
//mode distance;
//levels
//(
// (1.0 4)
// (2.0 3)
//);
}
// Mesh selection
// ~~~~~~~~~~~~~~
// After refinement patches get added for all refinementSurfaces and
// all cells intersecting the surfaces get put into these patches. The
// section reachable from the locationInMesh is kept.
// NOTE: This point should never be on a face, always inside a cell, even
// after refinement.
locationInMesh (0.25 0.01 0.25);
// Whether any faceZones (as specified in the refinementSurfaces)
// are only on the boundary of corresponding cellZones or also allow
// free-standing zone faces. Not used if there are no faceZones.
allowFreeStandingZoneFaces true;
}
// Settings for the snapping.
snapControls
{
//- Number of patch smoothing iterations before finding correspondence
// to surface
nSmoothPatch 3;
//- Relative distance for points to be attracted by surface feature point
// or edge. True distance is this factor times local
// maximum edge length.
tolerance 4.0;
//- Number of mesh displacement relaxation iterations.
nSolveIter 30;
//- Maximum number of snapping relaxation iterations. Should stop
// before upon reaching a correct mesh.
nRelaxIter 5;
}
// Settings for the layer addition.
addLayersControls
{
// Are the thickness parameters below relative to the undistorted
// size of the refined cell outside layer (true) or absolute sizes (false).
relativeSizes true;
// Per final patch (so not geometry!) the layer information
layers
{
//batimetria_patch0
//{
// nSurfaceLayers 2; //was 1 //was 4
//}
}
// Expansion factor for layer mesh
expansionRatio 1.0;
//- Wanted thickness of final added cell layer. If multiple layers
// is the thickness of the layer furthest away from the wall.
// See relativeSizes parameter.
finalLayerThickness 0.3;
//- Minimum thickness of cell layer. If for any reason layer
// cannot be above minThickness do not add layer.
// Relative to undistorted size of cell outside layer.
minThickness 0.1;
//- If points get not extruded do nGrow layers of connected faces that are
// also not grown. This helps convergence of the layer addition process
// close to features.
nGrow 1;
// Advanced settings
//- When not to extrude surface. 0 is flat surface, 90 is when two faces
// make straight angle.
featureAngle 30;
//- Maximum number of snapping relaxation iterations. Should stop
// before upon reaching a correct mesh.
nRelaxIter 3;
// Number of smoothing iterations of surface normals
nSmoothSurfaceNormals 1;
// Number of smoothing iterations of interior mesh movement direction
nSmoothNormals 3;
// Smooth layer thickness over surface patches
nSmoothThickness 10;
// Stop layer growth on highly warped cells
maxFaceThicknessRatio 0.5;
// Reduce layer growth where ratio thickness to medial
// distance is large
maxThicknessToMedialRatio 0.3;
// Angle used to pick up medial axis points
minMedianAxisAngle 130;
// Create buffer region for new layer terminations
nBufferCellsNoExtrude 0;
// Overall max number of layer addition iterations
nLayerIter 50;
}
// Generic mesh quality settings. At any undoable phase these determine
// where to undo.
meshQualityControls
{
//- Maximum non-orthogonality allowed. Set to 180 to disable.
maxNonOrtho 65;
//- Max skewness allowed. Set to <0 to disable.
maxBoundarySkewness 20;
maxInternalSkewness 4;
//- Max concaveness allowed. Is angle (in degrees) below which concavity
// is allowed. 0 is straight face, <0 would be convex face.
// Set to 180 to disable.
maxConcave 80;
//- Minimum projected area v.s. actual area. Set to -1 to disable.
minFlatness 0.5;
//- Minimum pyramid volume. Is absolute volume of cell pyramid.
// Set to a sensible fraction of the smallest cell volume expected.
// Set to very negative number (e.g. -1E30) to disable.
minVol 1e-13;
//- Minimum quality of the tet formed by the face-centre
// and variable base point minimum decomposition triangles and
// the cell centre. This has to be a positive number for tracking
// to work. Set to very negative number (e.g. -1E30) to
// disable.
// <0 = inside out tet,
// 0 = flat tet
// 1 = regular tet
minTetQuality 1e-30;
//- Minimum face area. Set to <0 to disable.
minArea -1;
//- Minimum face twist. Set to <-1 to disable. dot product of face normal
//- and face centre triangles normal
minTwist 0.02;
//- minimum normalised cell determinant
//- 1 = hex, <= 0 = folded or flattened illegal cell
minDeterminant 0.001;
//- minFaceWeight (0 -> 0.5)
minFaceWeight 0.02;
//- minVolRatio (0 -> 1)
minVolRatio 0.01;
//must be >0 for Fluent compatibility
minTriangleTwist -1;
// Advanced
//- Number of error distribution iterations
nSmoothScale 4;
//- amount to scale back displacement at error points
errorReduction 0.75;
}
// Advanced
// Flags for optional output
// 0 : only write final meshes
// 1 : write intermediate meshes
// 2 : write volScalarField with cellLevel for postprocessing
// 4 : write current intersections as .obj files
debug 0;
// Merge tolerance. Is fraction of overall bounding box of initial mesh.
// Note: the write tolerance needs to be higher than this.
mergeTolerance 1E-6;
// ************************************************************************* //

View file

@ -0,0 +1,19 @@
[main]
input_dir = .
work_dir = /home/masterccce/OpenFOAM/work
case = artha
#log_file = openfoam.log
[blockMesh]
enable = True
[snappyHexMesh]
enable = True
[setFields]
enable = True
[olaFlow]
enable = True
[parallel]
enable = False
threads = 4
[reconstructPar]
enable = True

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openfoam/run/__main__.py Normal file
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import sys
import argparse
import logging
import configparser
from pprint import pp
from time import time
from datetime import timedelta
from pathlib import Path
from distutils import dir_util
import subprocess as sp
_t0 = time()
parser = argparse.ArgumentParser(
description='Run the OpenFoam simulation'
)
parser.add_argument('-c', '--config', default='config.ini', type=Path,
help='Configuration file (default config.ini)')
parser.add_argument('-l', '--log-level', default='INFO', type=str,
help='Log level')
args = parser.parse_args()
config = configparser.ConfigParser()
config.read(args.config)
logging.basicConfig(
filename=config['main'].get('log_file', None),
level=args.log_level
)
log = logging.getLogger('openfoam')
log.info('Starting program')
input_dir = Path(config['main']['input_dir'], config['main']['case'])
work_dir = Path(config['main']['work_dir'])
if not work_dir.exists():
log.error(f'Work directory ({work_dir}) not found')
sys.exit(1)
case_dir = work_dir.joinpath(config['main']['case'])
if case_dir.exists():
log.info(f'Deleting case ({case_dir})')
dir_util.remove_tree(str(case_dir))
log.info(f'Copying case ({input_dir} -> {case_dir})')
dir_util.copy_tree(
str(input_dir),
str(case_dir),
)
if config['blockMesh'].getboolean('enable'):
log.info('Running blockMesh')
blockmesh_log = logging.getLogger('blockMesh')
proc = sp.Popen(
('blockMesh'),
cwd=case_dir,
stdout=sp.PIPE,
stderr=sp.PIPE,
text=True,
)
for line in proc.stdout:
blockmesh_log.info(line[:-1])
for line in proc.stderr:
blockmesh_log.error(line[:-1])
code = proc.wait()
if code != 0:
log.error('blockMesh failed')
sys.exit(code)
log.info(f'blockMesh finished successfully')
if config['snappyHexMesh'].getboolean('enable'):
log.info('Running snappyHexMesh')
snappy_log = logging.getLogger('snappyHexMesh')
proc = sp.Popen(
('snappyHexMesh', '-overwrite'),
cwd=case_dir,
stdout=sp.PIPE,
stderr=sp.PIPE,
text=True,
)
for line in proc.stdout:
snappy_log.info(line[:-1])
for line in proc.stderr:
snappy_log.error(line[:-1])
code = proc.wait()
if code != 0:
log.error('snappyHexMesh failed')
sys.exit(code)
log.info(f'snappyHexMesh finished successfully')
log.info('Copying 0.org -> 0')
dir_util.copy_tree(
str(case_dir.joinpath('0.org')),
str(case_dir.joinpath('0')),
)
if config['setFields'].getboolean('enable'):
log.info('Running setFields')
setfields_log = logging.getLogger('setFields')
proc = sp.Popen(
('setFields'),
cwd=case_dir,
stdout=sp.PIPE,
stderr=sp.PIPE,
text=True,
)
for line in proc.stdout:
setfields_log.info(line[:-1])
for line in proc.stderr:
setfields_log.info(line[:-1])
code = proc.wait()
if code != 0:
log.error('setFields failed')
sys.exit(code)
log.info(f'setFields finished successfully')
if config['olaFlow'].getboolean('enable'):
cmd = ('olaFlow')
if config['parallel'].getboolean('enable'):
cmd = (
'mpirun',
'-np', config['parallel'].getint('threads'),
'olaFlow', '-parallel'
)
decpar_log = logging.getLogger('decomposePar')
proc = sp.Popen(
('decomposePar'),
cwd=case_dir,
stdout=sp.PIPE,
stderr=sp.PIPE,
text=True,
)
for line in proc.stdout:
decpar_log.info(line[:-1])
for line in proc.stderr:
decpar_log.error(line[:-1])
code = proc.wait()
if code != 0:
log.error('decomposePar failed')
sys.exit(code)
log.info(f'decomposePar finished successfully')
log.info('Running olaFlow')
olaflow_log = logging.getLogger('olaFlow')
proc = sp.Popen(
cmd,
cwd=case_dir,
stdout=sp.PIPE,
stderr=sp.PIPE,
text=True,
)
for line in proc.stdout:
olaflow_log.info(line[:-1])
for line in proc.stderr:
olaflow_log.error(line[:-1])
code = proc.wait()
if code != 0:
log.error('olaFlow failed')
sys.exit(code)
log.info(f'olaFlow finished successfully')
if config['parallel'].getboolean('enable') \
and config['reconstructPar'].getboolean('enable'):
recpar_log = logging.getLogger('reconstructPar')
proc = sp.Popen(
('reconstructPar'),
cwd=case_dir,
stdout=sp.PIPE,
stderr=sp.PIPE,
text=True,
)
for line in proc.stdout:
recpar_log.info(line[:-1])
for line in proc.stderr:
recpar_log.error(line[:-1])
code = proc.wait()
if code != 0:
log.error('reconstructPar failed')
sys.exit(code)
log.info(f'reconstructPar finished successfully')
log.info(f'Deleting processor directories')
for proc_dir in case_dir.glob(r'processor*'):
log.info(f'Deleting {proc_dir}')
dir_util.remove_tree(str(proc_dir))
_t1 = time()
log.info(f'Program ended successfully after {timedelta(seconds=_t1-_t0)}')