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Updated with new run, test and clean scripts

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This commit is contained in:
henry
2008-06-16 12:49:38 +01:00
parent c52b20b10d
commit 39d9bebe26
976 changed files with 530884 additions and 0 deletions
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50
tutorials/interDyMFoam/damBreakWithObstacle/0-orig/U Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4.1 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "/home/dm2/henry/OpenFOAM/OpenFOAM-1.4.1/tutorials/interFoam";
case "damBreak";
instance "0";
local "";
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
walls
{
type fixedValue;
value uniform (0 0 0);
}
obstacle
{
type fixedValue;
value uniform (0 0 0);
}
atmosphere
{
type pressureInletOutletVelocity;
phi phi;
value uniform (0 0 0);
}
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object gamma;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type zeroGradient;
}
obstacle
{
type zeroGradient;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object gamma;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type zeroGradient;
}
obstacle
{
type zeroGradient;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object pd;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type zeroGradient;
}
obstacle
{
type zeroGradient;
}
atmosphere
{
type totalPressure;
p0 uniform 0;
U U;
phi phi;
rho none;
psi none;
gamma 1;
value uniform 0;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
location "0";
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
atmosphere
{
type pressureInletOutletVelocity;
phi phi;
value uniform (0 0 0);
}
walls
{
type fixedValue;
value uniform (0 0 0);
}
}
// ************************************************************************* //

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tutorials/interDyMFoam/damBreakWithObstacle/0/gamma.org Normal file
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object gamma;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type zeroGradient;
}
obstacle
{
type zeroGradient;
}
atmosphere
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class volScalarField;
object pd;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type zeroGradient;
}
obstacle
{
type zeroGradient;
}
atmosphere
{
type totalPressure;
p0 uniform 0;
U U;
phi phi;
rho none;
psi none;
gamma 1;
value uniform 0;
}
}
// ************************************************************************* //

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tutorials/interDyMFoam/damBreakWithObstacle/Allrun Executable file
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#!/bin/sh
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Get application name from directory
application=`basename $PWD`
runApplication blockMesh
runApplication setSet -batch createObstacle.setSet
runApplication subsetMesh c0 -patch walls
runApplication setFields -latestTime
runApplication $application

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tutorials/interDyMFoam/damBreakWithObstacle/constant/dynamicMeshDict Normal file
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object motionProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dynamicFvMesh dynamicRefineFvMesh;
// Refinement
dynamicRefineFvMeshCoeffs
{
// Refine every refineInterval timesteps
refineInterval 1;
// volScalarField to base refinement on
field gamma;
//
// 1. interpolate field
// 2. mark any cell
// - using a point value >minLevel <maxLevel
// - level < maxRefinement
// - unprotected
// 3. if too many cells determine cost function:
// - lowest level wins
// - cell closest to (0.5*minLevel + 0.5*maxLevel) wins
// Which cells to un/refine: based on point values (simple averaging).
// - refine pointCells of point value > refineLevel
// - unrefine pointCells of point value < unrefineLevel and that
// are not within nBufferLayers of points marked for refinement.
// All cells (neighbouring a cell with) gamma get refined
lowerRefineLevel 0.001;
upperRefineLevel 0.999;
// All points are candidates for unrefining (gamma always <1)
unrefineLevel 10;
nBufferLayers 1;
// Maximum refinement level (starts from 0)
maxRefinement 2;
// Maximum cell limit (approximate)
maxCells 200000;
// Fluxes to correct and variable they can be interpolated from
correctFluxes ((phi U));
// Write cellLevel?
dumpLevel true;
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object environmentalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
g g [0 1 -2 0 0 0 0] (0 0 -9.81);
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 1;
vertices
(
(0 0 0)
(1 0 0)
(1 1 0)
(0 1 0)
(0 0 1)
(1 0 1)
(1 1 1)
(0 1 1)
);
blocks
(
hex (0 1 2 3 4 5 6 7) (32 32 32) simpleGrading (1 1 1)
);
edges
(
);
patches
(
patch atmosphere
(
(3 7 6 2)
)
wall walls
(
(0 4 7 3)
(2 6 5 1)
(1 5 4 0)
(0 3 2 1)
(4 5 6 7)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

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tutorials/interDyMFoam/damBreakWithObstacle/constant/polyMesh/boundary Normal file
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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
object boundary;
location "constant/polyMesh";
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
2
(
atmosphere
{
type patch;
nFaces 1024;
startFace 95232;
}
walls
{
type wall;
nFaces 5120;
startFace 96256;
}
)
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
phase1
{
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 1e-06;
rho rho [1 -3 0 0 0 0 0] 1000;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] 1e-06;
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
m m [0 0 1 0 0 0 0] 1;
n n [0 0 0 0 0 0 0] 0;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] 0.0142515;
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
k k [0 0 1 0 0 0 0] 99.6;
n n [0 0 0 0 0 0 0] 0.1003;
}
}
phase2
{
transportModel Newtonian;
nu nu [0 2 -1 0 0 0 0] 1.48e-05;
rho rho [1 -3 0 0 0 0 0] 1;
CrossPowerLawCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] 1e-06;
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
m m [0 0 1 0 0 0 0] 1;
n n [0 0 0 0 0 0 0] 0;
}
BirdCarreauCoeffs
{
nu0 nu0 [0 2 -1 0 0 0 0] 0.0142515;
nuInf nuInf [0 2 -1 0 0 0 0] 1e-06;
k k [0 0 1 0 0 0 0] 99.6;
n n [0 0 0 0 0 0 0] 0.1003;
}
}
sigma sigma [1 0 -2 0 0 0 0] 0.07;
// ************************************************************************* //

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

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cellSet c0 new
cellSet c0 invert
cellSet c0 delete boxToCell (0.375 0.375 0) (0.625 0.625 0.25)

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tutorials/interDyMFoam/damBreakWithObstacle/system/controlDict Normal file
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application interFoam;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 2;
deltaT 0.001;
writeControl adjustableRunTime; //timeStep; //adjustableRunTime;
writeInterval 0.02; //10; //0.02;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep yes;
maxCo 0.1;
maxDeltaT 1;
// ************************************************************************* //

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tutorials/interDyMFoam/damBreakWithObstacle/system/decomposeParDict Normal file
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object decomposeParDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
numberOfSubdomains 6;
method metis;
//method hierarchical;
simpleCoeffs
{
n (2 2 1);
delta 0.001;
}
hierarchicalCoeffs
{
n (2 2 1);
delta 0.001;
order xyz;
}
metisCoeffs
{}
manualCoeffs
{
dataFile "";
}
distributed no;
roots
(
);
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
grad(U) Gauss linear;
grad(gamma) Gauss linear;
}
divSchemes
{
div(rho*phi,U) Gauss upwind; //limitedLinearV 1;
div(phi,gamma) Gauss vanLeer;
div(phirb,gamma) Gauss interfaceCompression;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
pd;
pcorr;
gamma;
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
pcorr PCG
{
preconditioner GAMG
{
tolerance 1e-3;
relTol 0;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
nBottomSweeps 2;
cacheAgglomeration false;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
};
tolerance 1e-4;
relTol 0;
maxIter 100;
};
pd GAMG
{
tolerance 1e-8;
relTol 0.05;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
nFinestSweeps 2;
cacheAgglomeration false;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
};
pdFinal PCG
{
preconditioner GAMG
{
tolerance 1e-8;
relTol 0;
nVcycles 2;
smoother GaussSeidel;
nPreSweeps 0;
nPostSweeps 2;
nFinestSweeps 2;
cacheAgglomeration false;
nCellsInCoarsestLevel 10;
agglomerator faceAreaPair;
mergeLevels 1;
};
tolerance 1e-8;
relTol 0;
maxIter 20;
};
U smoothSolver
{
smoother GaussSeidel;
tolerance 1e-6;
relTol 0;
nSweeps 1;
};
k PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
B PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
nuTilda PBiCG
{
preconditioner DILU;
tolerance 1e-08;
relTol 0;
};
}
PISO
{
momentumPredictor no;
nCorrectors 3;
nNonOrthogonalCorrectors 0;
nGammaCorr 1;
nGammaSubCycles 3;
cGamma 1;
pdRefCell 0;
pdRefValue 0;
pRefProbe
{
fields (pd);
probeLocations ((0.51 0.51 0.51));
};
}
// ************************************************************************* //

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tutorials/interDyMFoam/damBreakWithObstacle/system/setFieldsDict Normal file
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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.4 |
| \\ / A nd | Web: http://www.openfoam.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
root "";
case "";
instance "";
local "";
class dictionary;
object setFieldsDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
defaultFieldValues
(
volScalarFieldValue gamma 0
volVectorFieldValue U (0 0 0)
);
regions
(
boxToCell
{
box (0 0 0) (0.60 0.1875 0.75);
fieldValues
(
volScalarFieldValue gamma 1
);
}
);
// ************************************************************************* //