Merge commit 'OpenCFD/master' into olesenm

This commit is contained in:
Mark Olesen
2009-02-17 16:35:00 +01:00
1633 changed files with 85791 additions and 19492 deletions

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/*---------------------------------------------------------------------------*\
========= |
\\ / F ield | OpenFOAM: The Open Source CFD Toolbox
\\ / O peration |
\\ / A nd | Copyright (C) 1991-2009 OpenCFD Ltd.
\\/ M anipulation |
-------------------------------------------------------------------------------
License
This file is part of OpenFOAM.
OpenFOAM is free software; you can redistribute it and/or modify it
under the terms of the GNU General Public License as published by the
Free Software Foundation; either version 2 of the License, or (at your
option) any later version.
OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
for more details.
You should have received a copy of the GNU General Public License
along with OpenFOAM; if not, write to the Free Software Foundation,
Inc., 51 Franklin St, Fifth Floor, Boston, MA 02110-1301 USA
Application
MRFSimpleFoam
Description
Steady-state solver for incompressible, turbulent flow of non-Newtonian
fluids with MRF regions.
\*---------------------------------------------------------------------------*/
#include "fvCFD.H"
#include "incompressible/singlePhaseTransportModel/singlePhaseTransportModel.H"
#include "incompressible/RASModel/RASModel.H"
#include "MRFZones.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
int main(int argc, char *argv[])
{
# include "setRootCase.H"
# include "createTime.H"
# include "createMesh.H"
# include "createFields.H"
# include "initContinuityErrs.H"
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Info<< "\nStarting time loop\n" << endl;
while (runTime.run())
{
runTime++;
Info<< "Time = " << runTime.timeName() << nl << endl;
# include "readSIMPLEControls.H"
p.storePrevIter();
// Pressure-velocity SIMPLE corrector
{
// Momentum predictor
tmp<fvVectorMatrix> UEqn
(
fvm::div(phi, U)
+ turbulence->divDevReff(U)
);
mrfZones.addCoriolis(UEqn());
UEqn().relax();
solve(UEqn() == -fvc::grad(p));
p.boundaryField().updateCoeffs();
volScalarField rAU = 1.0/UEqn().A();
U = rAU*UEqn().H();
UEqn.clear();
phi = fvc::interpolate(U, "interpolate(HbyA)") & mesh.Sf();
mrfZones.relativeFlux(phi);
adjustPhi(phi, U, p);
// Non-orthogonal pressure corrector loop
for (int nonOrth=0; nonOrth<=nNonOrthCorr; nonOrth++)
{
fvScalarMatrix pEqn
(
fvm::laplacian(rAU, p) == fvc::div(phi)
);
pEqn.setReference(pRefCell, pRefValue);
pEqn.solve();
if (nonOrth == nNonOrthCorr)
{
phi -= pEqn.flux();
}
}
# include "continuityErrs.H"
// Explicitly relax pressure for momentum corrector
p.relax();
// Momentum corrector
U -= rAU*fvc::grad(p);
U.correctBoundaryConditions();
}
turbulence->correct();
runTime.write();
Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
<< " ClockTime = " << runTime.elapsedClockTime() << " s"
<< nl << endl;
}
Info<< "End\n" << endl;
return(0);
}
// ************************************************************************* //

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MRFSimpleFoam.C
EXE = $(FOAM_USER_APPBIN)/MRFSimpleFoam

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

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Info << "Reading field p\n" << endl;
volScalarField p
(
IOobject
(
"p",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
Info << "Reading field U\n" << endl;
volVectorField U
(
IOobject
(
"U",
runTime.timeName(),
mesh,
IOobject::MUST_READ,
IOobject::AUTO_WRITE
),
mesh
);
# include "createPhi.H"
label pRefCell = 0;
scalar pRefValue = 0.0;
setRefCell(p, mesh.solutionDict().subDict("SIMPLE"), pRefCell, pRefValue);
singlePhaseTransportModel laminarTransport(U, phi);
autoPtr<incompressible::RASModel> turbulence
(
incompressible::RASModel::New(U, phi, laminarTransport)
);
MRFZones mrfZones(mesh);
mrfZones.correctBoundaryVelocity(U);

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
rotor
{
type fixedValue;
value uniform (0 0 0);
}
stator
{
type fixedValue;
value uniform (0 0 0);
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 20;
boundaryField
{
rotor
{
type zeroGradient;
}
stator
{
type zeroGradient;
}
front
{
type empty;
}
back
{
type empty;
}
}
// ************************************************************************* //

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

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

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#!/bin/sh
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
application="MRFSimpleFoam"
./makeMesh
runApplication $application

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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;
location "constant";
object MRFZones;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
1
(
rotor
{
patches (rotor);
origin origin [0 1 0 0 0 0 0] (0 0 0);
axis axis [0 0 0 0 0 0 0] (0 0 1);
omega omega [0 0 -1 0 0 0 0] 104.72;
}
)
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel kEpsilon;
turbulence on;
printCoeffs on;
laminarCoeffs
{
}
kEpsilonCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
RNGkEpsilonCoeffs
{
Cmu 0.0845;
C1 1.42;
C2 1.68;
alphak 1.39;
alphaEps 1.39;
eta0 4.38;
beta 0.012;
}
kOmegaSSTCoeffs
{
alphaK1 0.85034;
alphaK2 1;
alphaOmega1 0.5;
alphaOmega2 0.85616;
gamma1 0.5532;
gamma2 0.4403;
beta1 0.075;
beta2 0.0828;
betaStar 0.09;
a1 0.31;
c1 10;
Cmu 0.09;
}
NonlinearKEShihCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76932;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
}
LienCubicKECoeffs
{
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
}
QZetaCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaZeta 0.76923;
anisotropic no;
}
LaunderSharmaKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
LamBremhorstKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
LienCubicKELowReCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
Am 0.016;
Aepsilon 0.263;
Amu 0.00222;
}
LienLeschzinerLowReCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
Am 0.016;
Aepsilon 0.263;
Amu 0.00222;
}
LRRCoeffs
{
Cmu 0.09;
Clrr1 1.8;
Clrr2 0.6;
C1 1.44;
C2 1.92;
Cs 0.25;
Ceps 0.15;
alphaEps 0.76923;
}
LaunderGibsonRSTMCoeffs
{
Cmu 0.09;
Clg1 1.8;
Clg2 0.6;
C1 1.44;
C2 1.92;
C1Ref 0.5;
C2Ref 0.3;
Cs 0.25;
Ceps 0.15;
alphaEps 0.76923;
alphaR 1.22;
}
SpalartAllmarasCoeffs
{
alphaNut 1.5;
Cb1 0.1355;
Cb2 0.622;
Cw2 0.3;
Cw3 2;
Cv1 7.1;
Cv2 5;
}
wallFunctionCoeffs
{
kappa 0.4187;
E 9;
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object dynamicMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dynamicFvMeshLib "libtopoChangerFvMesh.so";
dynamicFvMesh mixerFvMesh;
mixerFvMeshCoeffs
{
coordinateSystem
{
type cylindrical;
origin ( 0 0 0 );
axis ( 0 0 1 );
direction ( 1 0 0 );
}
rpm 10;
slider
{
inside insideSlider;
outside outsideSlider;
}
}
// ************************************************************************* //

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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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// General macros to create 2D/extruded-2D meshes
//define(calc, [esyscmd(echo $1 | bc | tr -d \\n)])
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.1;
// Hub radius
// Impeller-tip radius
// Baffle-tip radius
// Tank radius
// MRF region radius
// Thickness of 2D slab
// Base z
// Top z
// Number of cells radially between hub and impeller tip
// Number of cells radially in each of the two regions between
// impeller and baffle tips
// Number of cells radially between baffle tip and tank
// Number of cells azimuthally in each of the 8 blocks
// Number of cells in the thickness of the slab
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
vertices
(
(0.2 0 0) // Vertex r0b = 0
(0.2 0 0) // Vertex r0sb = 1
(0.141421356364228 -0.141421356110391 0) // Vertex r1b = 2
(3.58979347393082e-10 -0.2 0) // Vertex r2b = 3
(3.58979347393082e-10 -0.2 0) // Vertex r2sb = 4
(-0.141421355856554 -0.141421356618065 0) // Vertex r3b = 5
(-0.2 7.17958694786164e-10 0) // Vertex r4b = 6
(-0.2 7.17958694786164e-10 0) // Vertex r4sb = 7
(-0.141421355856554 0.141421356618065 0) // Vertex r5b = 8
(3.58979347393082e-10 0.2 0) // Vertex r6b = 9
(3.58979347393082e-10 0.2 0) // Vertex r6sb = 10
(0.141421356364228 0.141421356110391 0) // Vertex r7b = 11
(0.5 0 0) // Vertex rb0b = 12
(0.353553390910569 -0.353553390275978 0) // Vertex rb1b = 13
(8.97448368482705e-10 -0.5 0) // Vertex rb2b = 14
(-0.353553389641386 -0.353553391545162 0) // Vertex rb3b = 15
(-0.5 1.79489673696541e-09 0) // Vertex rb4b = 16
(-0.353553389641386 0.353553391545162 0) // Vertex rb5b = 17
(8.97448368482705e-10 0.5 0) // Vertex rb6b = 18
(0.353553390910569 0.353553390275978 0) // Vertex rb7b = 19
(0.6 0 0) // Vertex ri0b = 20
(0.424264069092683 -0.424264068331174 0) // Vertex ri1b = 21
(1.07693804217925e-09 -0.6 0) // Vertex ri2b = 22
(-0.424264067569663 -0.424264069854194 0) // Vertex ri3b = 23
(-0.6 2.15387608435849e-09 0) // Vertex ri4b = 24
(-0.424264067569663 0.424264069854194 0) // Vertex ri5b = 25
(1.07693804217925e-09 0.6 0) // Vertex ri6b = 26
(0.424264069092683 0.424264068331174 0) // Vertex ri7b = 27
(0.7 0 0) // Vertex Rb0b = 28
(0.494974747274797 -0.494974746386369 0) // Vertex Rb1b = 29
(1.25642771587579e-09 -0.7 0) // Vertex Rb2b = 30
(-0.49497474549794 -0.494974748163226 0) // Vertex Rb3b = 31
(-0.7 2.51285543175157e-09 0) // Vertex Rb4b = 32
(-0.49497474549794 0.494974748163226 0) // Vertex Rb5b = 33
(1.25642771587579e-09 0.7 0) // Vertex Rb6b = 34
(0.494974747274797 0.494974746386369 0) // Vertex Rb7b = 35
(1 0 0) // Vertex R0b = 36
(0.707106781821139 -0.707106780551956 0) // Vertex R1b = 37
(0.707106781821139 -0.707106780551956 0) // Vertex R1sb = 38
(1.79489673696541e-09 -1 0) // Vertex R2b = 39
(-0.707106779282772 -0.707106783090323 0) // Vertex R3b = 40
(-0.707106779282772 -0.707106783090323 0) // Vertex R3sb = 41
(-1 3.58979347393082e-09 0) // Vertex R4b = 42
(-0.707106779282772 0.707106783090323 0) // Vertex R5b = 43
(-0.707106779282772 0.707106783090323 0) // Vertex R5sb = 44
(1.79489673696541e-09 1 0) // Vertex R6b = 45
(0.707106781821139 0.707106780551956 0) // Vertex R7b = 46
(0.707106781821139 0.707106780551956 0) // Vertex R7sb = 47
(0.2 0 0.1) // Vertex r0t = 48
(0.2 0 0.1) // Vertex r0st = 49
(0.141421356364228 -0.141421356110391 0.1) // Vertex r1t = 50
(3.58979347393082e-10 -0.2 0.1) // Vertex r2t = 51
(3.58979347393082e-10 -0.2 0.1) // Vertex r2st = 52
(-0.141421355856554 -0.141421356618065 0.1) // Vertex r3t = 53
(-0.2 7.17958694786164e-10 0.1) // Vertex r4t = 54
(-0.2 7.17958694786164e-10 0.1) // Vertex r4st = 55
(-0.141421355856554 0.141421356618065 0.1) // Vertex r5t = 56
(3.58979347393082e-10 0.2 0.1) // Vertex r6t = 57
(3.58979347393082e-10 0.2 0.1) // Vertex r6st = 58
(0.141421356364228 0.141421356110391 0.1) // Vertex r7t = 59
(0.5 0 0.1) // Vertex rb0t = 60
(0.353553390910569 -0.353553390275978 0.1) // Vertex rb1t = 61
(8.97448368482705e-10 -0.5 0.1) // Vertex rb2t = 62
(-0.353553389641386 -0.353553391545162 0.1) // Vertex rb3t = 63
(-0.5 1.79489673696541e-09 0.1) // Vertex rb4t = 64
(-0.353553389641386 0.353553391545162 0.1) // Vertex rb5t = 65
(8.97448368482705e-10 0.5 0.1) // Vertex rb6t = 66
(0.353553390910569 0.353553390275978 0.1) // Vertex rb7t = 67
(0.6 0 0.1) // Vertex ri0t = 68
(0.424264069092683 -0.424264068331174 0.1) // Vertex ri1t = 69
(1.07693804217925e-09 -0.6 0.1) // Vertex ri2t = 70
(-0.424264067569663 -0.424264069854194 0.1) // Vertex ri3t = 71
(-0.6 2.15387608435849e-09 0.1) // Vertex ri4t = 72
(-0.424264067569663 0.424264069854194 0.1) // Vertex ri5t = 73
(1.07693804217925e-09 0.6 0.1) // Vertex ri6t = 74
(0.424264069092683 0.424264068331174 0.1) // Vertex ri7t = 75
(0.7 0 0.1) // Vertex Rb0t = 76
(0.494974747274797 -0.494974746386369 0.1) // Vertex Rb1t = 77
(1.25642771587579e-09 -0.7 0.1) // Vertex Rb2t = 78
(-0.49497474549794 -0.494974748163226 0.1) // Vertex Rb3t = 79
(-0.7 2.51285543175157e-09 0.1) // Vertex Rb4t = 80
(-0.49497474549794 0.494974748163226 0.1) // Vertex Rb5t = 81
(1.25642771587579e-09 0.7 0.1) // Vertex Rb6t = 82
(0.494974747274797 0.494974746386369 0.1) // Vertex Rb7t = 83
(1 0 0.1) // Vertex R0t = 84
(0.707106781821139 -0.707106780551956 0.1) // Vertex R1t = 85
(0.707106781821139 -0.707106780551956 0.1) // Vertex R1st = 86
(1.79489673696541e-09 -1 0.1) // Vertex R2t = 87
(-0.707106779282772 -0.707106783090323 0.1) // Vertex R3t = 88
(-0.707106779282772 -0.707106783090323 0.1) // Vertex R3st = 89
(-1 3.58979347393082e-09 0.1) // Vertex R4t = 90
(-0.707106779282772 0.707106783090323 0.1) // Vertex R5t = 91
(-0.707106779282772 0.707106783090323 0.1) // Vertex R5st = 92
(1.79489673696541e-09 1 0.1) // Vertex R6t = 93
(0.707106781821139 0.707106780551956 0.1) // Vertex R7t = 94
(0.707106781821139 0.707106780551956 0.1) // Vertex R7st = 95
);
blocks
(
// block0
hex (0 2 13 12 48 50 61 60)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block1
hex (2 4 14 13 50 52 62 61)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block2
hex (3 5 15 14 51 53 63 62)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block3
hex (5 7 16 15 53 55 64 63)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block4
hex (6 8 17 16 54 56 65 64)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block5
hex (8 10 18 17 56 58 66 65)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block6
hex (9 11 19 18 57 59 67 66)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block7
hex (11 1 12 19 59 49 60 67)
rotor
(12 12 1)
simpleGrading (1 1 1)
// block0
hex (12 13 21 20 60 61 69 68)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block1
hex (13 14 22 21 61 62 70 69)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block2
hex (14 15 23 22 62 63 71 70)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block3
hex (15 16 24 23 63 64 72 71)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block4
hex (16 17 25 24 64 65 73 72)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block5
hex (17 18 26 25 65 66 74 73)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block6
hex (18 19 27 26 66 67 75 74)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block7
hex (19 12 20 27 67 60 68 75)
rotor
(12 4 1)
simpleGrading (1 1 1)
// block0
hex (20 21 29 28 68 69 77 76)
(12 4 1)
simpleGrading (1 1 1)
// block1
hex (21 22 30 29 69 70 78 77)
(12 4 1)
simpleGrading (1 1 1)
// block2
hex (22 23 31 30 70 71 79 78)
(12 4 1)
simpleGrading (1 1 1)
// block3
hex (23 24 32 31 71 72 80 79)
(12 4 1)
simpleGrading (1 1 1)
// block4
hex (24 25 33 32 72 73 81 80)
(12 4 1)
simpleGrading (1 1 1)
// block5
hex (25 26 34 33 73 74 82 81)
(12 4 1)
simpleGrading (1 1 1)
// block6
hex (26 27 35 34 74 75 83 82)
(12 4 1)
simpleGrading (1 1 1)
// block7
hex (27 20 28 35 75 68 76 83)
(12 4 1)
simpleGrading (1 1 1)
// block0
hex (28 29 38 36 76 77 86 84)
(12 12 1)
simpleGrading (1 1 1)
// block1
hex (29 30 39 37 77 78 87 85)
(12 12 1)
simpleGrading (1 1 1)
// block2
hex (30 31 41 39 78 79 89 87)
(12 12 1)
simpleGrading (1 1 1)
// block3
hex (31 32 42 40 79 80 90 88)
(12 12 1)
simpleGrading (1 1 1)
// block4
hex (32 33 44 42 80 81 92 90)
(12 12 1)
simpleGrading (1 1 1)
// block5
hex (33 34 45 43 81 82 93 91)
(12 12 1)
simpleGrading (1 1 1)
// block6
hex (34 35 47 45 82 83 95 93)
(12 12 1)
simpleGrading (1 1 1)
// block7
hex (35 28 36 46 83 76 84 94)
(12 12 1)
simpleGrading (1 1 1)
);
edges
(
arc 0 2 (0.184775906536601 -0.0765366863901046 0)
arc 2 4 (0.0765366867217582 -0.184775906399226 0)
arc 3 5 (-0.0765366860584508 -0.184775906673977 0)
arc 5 7 (-0.18477590626185 -0.0765366870534118 0)
arc 6 8 (-0.18477590626185 0.0765366870534118 0)
arc 8 10 (-0.0765366860584508 0.184775906673977 0)
arc 9 11 (0.0765366867217582 0.184775906399226 0)
arc 11 1 (0.184775906536601 0.0765366863901046 0)
arc 12 13 (0.461939766341503 -0.191341715975262 0)
arc 13 14 (0.191341716804395 -0.461939765998065 0)
arc 14 15 (-0.191341715146127 -0.461939766684942 0)
arc 15 16 (-0.461939765654626 -0.19134171763353 0)
arc 16 17 (-0.461939765654626 0.19134171763353 0)
arc 17 18 (-0.191341715146127 0.461939766684942 0)
arc 18 19 (0.191341716804395 0.461939765998065 0)
arc 19 12 (0.461939766341503 0.191341715975262 0)
arc 20 21 (0.554327719609804 -0.229610059170314 0)
arc 21 22 (0.229610060165275 -0.554327719197677 0)
arc 22 23 (-0.229610058175352 -0.55432772002193 0)
arc 23 24 (-0.554327718785551 -0.229610061160235 0)
arc 24 25 (-0.554327718785551 0.229610061160235 0)
arc 25 26 (-0.229610058175352 0.55432772002193 0)
arc 26 27 (0.229610060165275 0.554327719197677 0)
arc 27 20 (0.554327719609804 0.229610059170314 0)
arc 28 29 (0.646715672878104 -0.267878402365366 0)
arc 29 30 (0.267878403526154 -0.64671567239729 0)
arc 30 31 (-0.267878401204578 -0.646715673358918 0)
arc 31 32 (-0.646715671916476 -0.267878404686941 0)
arc 32 33 (-0.646715671916476 0.267878404686941 0)
arc 33 34 (-0.267878401204578 0.646715673358918 0)
arc 34 35 (0.267878403526154 0.64671567239729 0)
arc 35 28 (0.646715672878104 0.267878402365366 0)
arc 36 38 (0.923879532683006 -0.382683431950523 0)
arc 37 39 (0.382683433608791 -0.923879531996129 0)
arc 39 41 (-0.382683430292254 -0.923879533369883 0)
arc 40 42 (-0.923879531309252 -0.382683435267059 0)
arc 42 44 (-0.923879531309252 0.382683435267059 0)
arc 43 45 (-0.382683430292254 0.923879533369883 0)
arc 45 47 (0.382683433608791 0.923879531996129 0)
arc 46 36 (0.923879532683006 0.382683431950523 0)
arc 48 50 (0.184775906536601 -0.0765366863901046 0.1)
arc 50 52 (0.0765366867217582 -0.184775906399226 0.1)
arc 51 53 (-0.0765366860584508 -0.184775906673977 0.1)
arc 53 55 (-0.18477590626185 -0.0765366870534118 0.1)
arc 54 56 (-0.18477590626185 0.0765366870534118 0.1)
arc 56 58 (-0.0765366860584508 0.184775906673977 0.1)
arc 57 59 (0.0765366867217582 0.184775906399226 0.1)
arc 59 49 (0.184775906536601 0.0765366863901046 0.1)
arc 60 61 (0.461939766341503 -0.191341715975262 0.1)
arc 61 62 (0.191341716804395 -0.461939765998065 0.1)
arc 62 63 (-0.191341715146127 -0.461939766684942 0.1)
arc 63 64 (-0.461939765654626 -0.19134171763353 0.1)
arc 64 65 (-0.461939765654626 0.19134171763353 0.1)
arc 65 66 (-0.191341715146127 0.461939766684942 0.1)
arc 66 67 (0.191341716804395 0.461939765998065 0.1)
arc 67 60 (0.461939766341503 0.191341715975262 0.1)
arc 68 69 (0.554327719609804 -0.229610059170314 0.1)
arc 69 70 (0.229610060165275 -0.554327719197677 0.1)
arc 70 71 (-0.229610058175352 -0.55432772002193 0.1)
arc 71 72 (-0.554327718785551 -0.229610061160235 0.1)
arc 72 73 (-0.554327718785551 0.229610061160235 0.1)
arc 73 74 (-0.229610058175352 0.55432772002193 0.1)
arc 74 75 (0.229610060165275 0.554327719197677 0.1)
arc 75 68 (0.554327719609804 0.229610059170314 0.1)
arc 76 77 (0.646715672878104 -0.267878402365366 0.1)
arc 77 78 (0.267878403526154 -0.64671567239729 0.1)
arc 78 79 (-0.267878401204578 -0.646715673358918 0.1)
arc 79 80 (-0.646715671916476 -0.267878404686941 0.1)
arc 80 81 (-0.646715671916476 0.267878404686941 0.1)
arc 81 82 (-0.267878401204578 0.646715673358918 0.1)
arc 82 83 (0.267878403526154 0.64671567239729 0.1)
arc 83 76 (0.646715672878104 0.267878402365366 0.1)
arc 84 86 (0.923879532683006 -0.382683431950523 0.1)
arc 85 87 (0.382683433608791 -0.923879531996129 0.1)
arc 87 89 (-0.382683430292254 -0.923879533369883 0.1)
arc 88 90 (-0.923879531309252 -0.382683435267059 0.1)
arc 90 92 (-0.923879531309252 0.382683435267059 0.1)
arc 91 93 (-0.382683430292254 0.923879533369883 0.1)
arc 93 95 (0.382683433608791 0.923879531996129 0.1)
arc 94 84 (0.923879532683006 0.382683431950523 0.1)
);
patches
(
wall rotor
(
(0 2 50 48)
(2 4 52 50)
(3 5 53 51)
(5 7 55 53)
(6 8 56 54)
(8 10 58 56)
(9 11 59 57)
(11 1 49 59)
(0 12 60 48)
(1 12 60 49)
(3 14 62 51)
(4 14 62 52)
(6 16 64 54)
(7 16 64 55)
(9 18 66 57)
(10 18 66 58)
)
wall stator
(
(36 38 86 84)
(37 39 87 85)
(39 41 89 87)
(40 42 90 88)
(42 44 92 90)
(43 45 93 91)
(45 47 95 93)
(46 36 84 94)
(37 29 77 85)
(38 29 77 86)
(40 31 79 88)
(41 31 79 89)
(43 33 81 91)
(44 33 81 92)
(46 35 83 94)
(47 35 83 95)
)
empty front
(
(48 50 61 60)
(50 52 62 61)
(51 53 63 62)
(53 55 64 63)
(54 56 65 64)
(56 58 66 65)
(57 59 67 66)
(59 49 60 67)
(60 61 69 68)
(61 62 70 69)
(62 63 71 70)
(63 64 72 71)
(64 65 73 72)
(65 66 74 73)
(66 67 75 74)
(67 60 68 75)
(68 69 77 76)
(69 70 78 77)
(70 71 79 78)
(71 72 80 79)
(72 73 81 80)
(73 74 82 81)
(74 75 83 82)
(75 68 76 83)
(76 77 86 84)
(77 78 87 85)
(78 79 89 87)
(79 80 90 88)
(80 81 92 90)
(81 82 93 91)
(82 83 95 93)
(83 76 84 94)
)
empty back
(
(0 12 13 2)
(2 13 14 4)
(3 14 15 5)
(5 15 16 7)
(6 16 17 8)
(8 17 18 10)
(9 18 19 11)
(11 19 12 1)
(12 20 21 13)
(13 21 22 14)
(14 22 23 15)
(15 23 24 16)
(16 24 25 17)
(17 25 26 18)
(18 26 27 19)
(19 27 20 12)
(20 28 29 21)
(21 29 30 22)
(22 30 31 23)
(23 31 32 24)
(24 32 33 25)
(25 33 34 26)
(26 34 35 27)
(27 35 28 20)
(28 36 38 29)
(29 37 39 30)
(30 39 41 31)
(31 40 42 32)
(32 42 44 33)
(33 43 45 34)
(34 45 47 35)
(35 46 36 28)
)
);
// ************************************************************************* //

View File

@ -0,0 +1,818 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// General macros to create 2D/extruded-2D meshes
changecom(//)changequote([,])
define(calc, [esyscmd(perl -e 'print ($1)')])
define(VCOUNT, 0)
define(vlabel, [[// ]Vertex $1 = VCOUNT define($1, VCOUNT)define([VCOUNT], incr(VCOUNT))])
define(pi, 3.14159265)
define(hex2D, hex ($1b $2b $3b $4b $1t $2t $3t $4t))
define(quad2D, ($1b $2b $2t $1t))
define(frontQuad, ($1t $2t $3t $4t))
define(backQuad, ($1b $4b $3b $2b))
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.1;
// Hub radius
define(r, 0.2)
// Impeller-tip radius
define(rb, 0.5)
// Baffle-tip radius
define(Rb, 0.7)
// Tank radius
define(R, 1)
// MRF region radius
define(ri, calc(0.5*(rb + Rb)))
// Thickness of 2D slab
define(z, 0.1)
// Base z
define(Zb, 0)
// Top z
define(Zt, calc(Zb + z))
// Number of cells radially between hub and impeller tip
define(Nr, 12)
// Number of cells radially in each of the two regions between
// impeller and baffle tips
define(Ni, 4)
// Number of cells radially between baffle tip and tank
define(NR, 12)
// Number of cells azimuthally in each of the 8 blocks
define(Na, 12)
// Number of cells in the thickness of the slab
define(Nz, 1)
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
define(vert, (x$1$2 y$1$2 $3))
define(evert, (ex$1$2 ey$1$2 $3))
define(a0, 0)
define(a1, -45)
define(a2, -90)
define(a3, -135)
define(a4, 180)
define(a5, 135)
define(a6, 90)
define(a7, 45)
define(ea0, -22.5)
define(ea1, -67.5)
define(ea2, -112.5)
define(ea3, -157.5)
define(ea4, 157.5)
define(ea5, 112.5)
define(ea6, 67.5)
define(ea7, 22.5)
define(ca0, calc(cos((pi/180)*a0)))
define(ca1, calc(cos((pi/180)*a1)))
define(ca2, calc(cos((pi/180)*a2)))
define(ca3, calc(cos((pi/180)*a3)))
define(ca4, calc(cos((pi/180)*a4)))
define(ca5, calc(cos((pi/180)*a5)))
define(ca6, calc(cos((pi/180)*a6)))
define(ca7, calc(cos((pi/180)*a7)))
define(sa0, calc(sin((pi/180)*a0)))
define(sa1, calc(sin((pi/180)*a1)))
define(sa2, calc(sin((pi/180)*a2)))
define(sa3, calc(sin((pi/180)*a3)))
define(sa4, calc(sin((pi/180)*a4)))
define(sa5, calc(sin((pi/180)*a5)))
define(sa6, calc(sin((pi/180)*a6)))
define(sa7, calc(sin((pi/180)*a7)))
define(cea0, calc(cos((pi/180)*ea0)))
define(cea1, calc(cos((pi/180)*ea1)))
define(cea2, calc(cos((pi/180)*ea2)))
define(cea3, calc(cos((pi/180)*ea3)))
define(cea4, calc(cos((pi/180)*ea4)))
define(cea5, calc(cos((pi/180)*ea5)))
define(cea6, calc(cos((pi/180)*ea6)))
define(cea7, calc(cos((pi/180)*ea7)))
define(sea0, calc(sin((pi/180)*ea0)))
define(sea1, calc(sin((pi/180)*ea1)))
define(sea2, calc(sin((pi/180)*ea2)))
define(sea3, calc(sin((pi/180)*ea3)))
define(sea4, calc(sin((pi/180)*ea4)))
define(sea5, calc(sin((pi/180)*ea5)))
define(sea6, calc(sin((pi/180)*ea6)))
define(sea7, calc(sin((pi/180)*ea7)))
define(x00, calc(r*ca0))
define(x01, calc(r*ca1))
define(x02, calc(r*ca2))
define(x03, calc(r*ca3))
define(x04, calc(r*ca4))
define(x05, calc(r*ca5))
define(x06, calc(r*ca6))
define(x07, calc(r*ca7))
define(x10, calc(rb*ca0))
define(x11, calc(rb*ca1))
define(x12, calc(rb*ca2))
define(x13, calc(rb*ca3))
define(x14, calc(rb*ca4))
define(x15, calc(rb*ca5))
define(x16, calc(rb*ca6))
define(x17, calc(rb*ca7))
define(x20, calc(ri*ca0))
define(x21, calc(ri*ca1))
define(x22, calc(ri*ca2))
define(x23, calc(ri*ca3))
define(x24, calc(ri*ca4))
define(x25, calc(ri*ca5))
define(x26, calc(ri*ca6))
define(x27, calc(ri*ca7))
define(x30, calc(Rb*ca0))
define(x31, calc(Rb*ca1))
define(x32, calc(Rb*ca2))
define(x33, calc(Rb*ca3))
define(x34, calc(Rb*ca4))
define(x35, calc(Rb*ca5))
define(x36, calc(Rb*ca6))
define(x37, calc(Rb*ca7))
define(x40, calc(R*ca0))
define(x41, calc(R*ca1))
define(x42, calc(R*ca2))
define(x43, calc(R*ca3))
define(x44, calc(R*ca4))
define(x45, calc(R*ca5))
define(x46, calc(R*ca6))
define(x47, calc(R*ca7))
define(y00, calc(r*sa0))
define(y01, calc(r*sa1))
define(y02, calc(r*sa2))
define(y03, calc(r*sa3))
define(y04, calc(r*sa4))
define(y05, calc(r*sa5))
define(y06, calc(r*sa6))
define(y07, calc(r*sa7))
define(y10, calc(rb*sa0))
define(y11, calc(rb*sa1))
define(y12, calc(rb*sa2))
define(y13, calc(rb*sa3))
define(y14, calc(rb*sa4))
define(y15, calc(rb*sa5))
define(y16, calc(rb*sa6))
define(y17, calc(rb*sa7))
define(y20, calc(ri*sa0))
define(y21, calc(ri*sa1))
define(y22, calc(ri*sa2))
define(y23, calc(ri*sa3))
define(y24, calc(ri*sa4))
define(y25, calc(ri*sa5))
define(y26, calc(ri*sa6))
define(y27, calc(ri*sa7))
define(y30, calc(Rb*sa0))
define(y31, calc(Rb*sa1))
define(y32, calc(Rb*sa2))
define(y33, calc(Rb*sa3))
define(y34, calc(Rb*sa4))
define(y35, calc(Rb*sa5))
define(y36, calc(Rb*sa6))
define(y37, calc(Rb*sa7))
define(y40, calc(R*sa0))
define(y41, calc(R*sa1))
define(y42, calc(R*sa2))
define(y43, calc(R*sa3))
define(y44, calc(R*sa4))
define(y45, calc(R*sa5))
define(y46, calc(R*sa6))
define(y47, calc(R*sa7))
define(ex00, calc(r*cea0))
define(ex01, calc(r*cea1))
define(ex02, calc(r*cea2))
define(ex03, calc(r*cea3))
define(ex04, calc(r*cea4))
define(ex05, calc(r*cea5))
define(ex06, calc(r*cea6))
define(ex07, calc(r*cea7))
define(ex10, calc(rb*cea0))
define(ex11, calc(rb*cea1))
define(ex12, calc(rb*cea2))
define(ex13, calc(rb*cea3))
define(ex14, calc(rb*cea4))
define(ex15, calc(rb*cea5))
define(ex16, calc(rb*cea6))
define(ex17, calc(rb*cea7))
define(ex20, calc(ri*cea0))
define(ex21, calc(ri*cea1))
define(ex22, calc(ri*cea2))
define(ex23, calc(ri*cea3))
define(ex24, calc(ri*cea4))
define(ex25, calc(ri*cea5))
define(ex26, calc(ri*cea6))
define(ex27, calc(ri*cea7))
define(ex30, calc(Rb*cea0))
define(ex31, calc(Rb*cea1))
define(ex32, calc(Rb*cea2))
define(ex33, calc(Rb*cea3))
define(ex34, calc(Rb*cea4))
define(ex35, calc(Rb*cea5))
define(ex36, calc(Rb*cea6))
define(ex37, calc(Rb*cea7))
define(ex40, calc(R*cea0))
define(ex41, calc(R*cea1))
define(ex42, calc(R*cea2))
define(ex43, calc(R*cea3))
define(ex44, calc(R*cea4))
define(ex45, calc(R*cea5))
define(ex46, calc(R*cea6))
define(ex47, calc(R*cea7))
define(ey00, calc(r*sea0))
define(ey01, calc(r*sea1))
define(ey02, calc(r*sea2))
define(ey03, calc(r*sea3))
define(ey04, calc(r*sea4))
define(ey05, calc(r*sea5))
define(ey06, calc(r*sea6))
define(ey07, calc(r*sea7))
define(ey10, calc(rb*sea0))
define(ey11, calc(rb*sea1))
define(ey12, calc(rb*sea2))
define(ey13, calc(rb*sea3))
define(ey14, calc(rb*sea4))
define(ey15, calc(rb*sea5))
define(ey16, calc(rb*sea6))
define(ey17, calc(rb*sea7))
define(ey20, calc(ri*sea0))
define(ey21, calc(ri*sea1))
define(ey22, calc(ri*sea2))
define(ey23, calc(ri*sea3))
define(ey24, calc(ri*sea4))
define(ey25, calc(ri*sea5))
define(ey26, calc(ri*sea6))
define(ey27, calc(ri*sea7))
define(ey30, calc(Rb*sea0))
define(ey31, calc(Rb*sea1))
define(ey32, calc(Rb*sea2))
define(ey33, calc(Rb*sea3))
define(ey34, calc(Rb*sea4))
define(ey35, calc(Rb*sea5))
define(ey36, calc(Rb*sea6))
define(ey37, calc(Rb*sea7))
define(ey40, calc(R*sea0))
define(ey41, calc(R*sea1))
define(ey42, calc(R*sea2))
define(ey43, calc(R*sea3))
define(ey44, calc(R*sea4))
define(ey45, calc(R*sea5))
define(ey46, calc(R*sea6))
define(ey47, calc(R*sea7))
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
vertices
(
vert(0, 0, Zb) vlabel(r0b)
vert(0, 0, Zb) vlabel(r0sb)
vert(0, 1, Zb) vlabel(r1b)
vert(0, 2, Zb) vlabel(r2b)
vert(0, 2, Zb) vlabel(r2sb)
vert(0, 3, Zb) vlabel(r3b)
vert(0, 4, Zb) vlabel(r4b)
vert(0, 4, Zb) vlabel(r4sb)
vert(0, 5, Zb) vlabel(r5b)
vert(0, 6, Zb) vlabel(r6b)
vert(0, 6, Zb) vlabel(r6sb)
vert(0, 7, Zb) vlabel(r7b)
vert(1, 0, Zb) vlabel(rb0b)
vert(1, 1, Zb) vlabel(rb1b)
vert(1, 2, Zb) vlabel(rb2b)
vert(1, 3, Zb) vlabel(rb3b)
vert(1, 4, Zb) vlabel(rb4b)
vert(1, 5, Zb) vlabel(rb5b)
vert(1, 6, Zb) vlabel(rb6b)
vert(1, 7, Zb) vlabel(rb7b)
vert(2, 0, Zb) vlabel(ri0b)
vert(2, 1, Zb) vlabel(ri1b)
vert(2, 2, Zb) vlabel(ri2b)
vert(2, 3, Zb) vlabel(ri3b)
vert(2, 4, Zb) vlabel(ri4b)
vert(2, 5, Zb) vlabel(ri5b)
vert(2, 6, Zb) vlabel(ri6b)
vert(2, 7, Zb) vlabel(ri7b)
vert(3, 0, Zb) vlabel(Rb0b)
vert(3, 1, Zb) vlabel(Rb1b)
vert(3, 2, Zb) vlabel(Rb2b)
vert(3, 3, Zb) vlabel(Rb3b)
vert(3, 4, Zb) vlabel(Rb4b)
vert(3, 5, Zb) vlabel(Rb5b)
vert(3, 6, Zb) vlabel(Rb6b)
vert(3, 7, Zb) vlabel(Rb7b)
vert(4, 0, Zb) vlabel(R0b)
vert(4, 1, Zb) vlabel(R1b)
vert(4, 1, Zb) vlabel(R1sb)
vert(4, 2, Zb) vlabel(R2b)
vert(4, 3, Zb) vlabel(R3b)
vert(4, 3, Zb) vlabel(R3sb)
vert(4, 4, Zb) vlabel(R4b)
vert(4, 5, Zb) vlabel(R5b)
vert(4, 5, Zb) vlabel(R5sb)
vert(4, 6, Zb) vlabel(R6b)
vert(4, 7, Zb) vlabel(R7b)
vert(4, 7, Zb) vlabel(R7sb)
vert(0, 0, Zt) vlabel(r0t)
vert(0, 0, Zt) vlabel(r0st)
vert(0, 1, Zt) vlabel(r1t)
vert(0, 2, Zt) vlabel(r2t)
vert(0, 2, Zt) vlabel(r2st)
vert(0, 3, Zt) vlabel(r3t)
vert(0, 4, Zt) vlabel(r4t)
vert(0, 4, Zt) vlabel(r4st)
vert(0, 5, Zt) vlabel(r5t)
vert(0, 6, Zt) vlabel(r6t)
vert(0, 6, Zt) vlabel(r6st)
vert(0, 7, Zt) vlabel(r7t)
vert(1, 0, Zt) vlabel(rb0t)
vert(1, 1, Zt) vlabel(rb1t)
vert(1, 2, Zt) vlabel(rb2t)
vert(1, 3, Zt) vlabel(rb3t)
vert(1, 4, Zt) vlabel(rb4t)
vert(1, 5, Zt) vlabel(rb5t)
vert(1, 6, Zt) vlabel(rb6t)
vert(1, 7, Zt) vlabel(rb7t)
vert(2, 0, Zt) vlabel(ri0t)
vert(2, 1, Zt) vlabel(ri1t)
vert(2, 2, Zt) vlabel(ri2t)
vert(2, 3, Zt) vlabel(ri3t)
vert(2, 4, Zt) vlabel(ri4t)
vert(2, 5, Zt) vlabel(ri5t)
vert(2, 6, Zt) vlabel(ri6t)
vert(2, 7, Zt) vlabel(ri7t)
vert(3, 0, Zt) vlabel(Rb0t)
vert(3, 1, Zt) vlabel(Rb1t)
vert(3, 2, Zt) vlabel(Rb2t)
vert(3, 3, Zt) vlabel(Rb3t)
vert(3, 4, Zt) vlabel(Rb4t)
vert(3, 5, Zt) vlabel(Rb5t)
vert(3, 6, Zt) vlabel(Rb6t)
vert(3, 7, Zt) vlabel(Rb7t)
vert(4, 0, Zt) vlabel(R0t)
vert(4, 1, Zt) vlabel(R1t)
vert(4, 1, Zt) vlabel(R1st)
vert(4, 2, Zt) vlabel(R2t)
vert(4, 3, Zt) vlabel(R3t)
vert(4, 3, Zt) vlabel(R3st)
vert(4, 4, Zt) vlabel(R4t)
vert(4, 5, Zt) vlabel(R5t)
vert(4, 5, Zt) vlabel(R5st)
vert(4, 6, Zt) vlabel(R6t)
vert(4, 7, Zt) vlabel(R7t)
vert(4, 7, Zt) vlabel(R7st)
);
blocks
(
// block0
hex2D(r0, r1, rb1, rb0)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block1
hex2D(r1, r2s, rb2, rb1)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block2
hex2D(r2, r3, rb3, rb2)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block3
hex2D(r3, r4s, rb4, rb3)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block4
hex2D(r4, r5, rb5, rb4)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block5
hex2D(r5, r6s, rb6, rb5)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block6
hex2D(r6, r7, rb7, rb6)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block7
hex2D(r7, r0s, rb0, rb7)
rotor
(Na Nr Nz)
simpleGrading (1 1 1)
// block0
hex2D(rb0, rb1, ri1, ri0)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block1
hex2D(rb1, rb2, ri2, ri1)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block2
hex2D(rb2, rb3, ri3, ri2)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block3
hex2D(rb3, rb4, ri4, ri3)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block4
hex2D(rb4, rb5, ri5, ri4)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block5
hex2D(rb5, rb6, ri6, ri5)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block6
hex2D(rb6, rb7, ri7, ri6)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block7
hex2D(rb7, rb0, ri0, ri7)
rotor
(Na Ni Nz)
simpleGrading (1 1 1)
// block0
hex2D(ri0, ri1, Rb1, Rb0)
(Na Ni Nz)
simpleGrading (1 1 1)
// block1
hex2D(ri1, ri2, Rb2, Rb1)
(Na Ni Nz)
simpleGrading (1 1 1)
// block2
hex2D(ri2, ri3, Rb3, Rb2)
(Na Ni Nz)
simpleGrading (1 1 1)
// block3
hex2D(ri3, ri4, Rb4, Rb3)
(Na Ni Nz)
simpleGrading (1 1 1)
// block4
hex2D(ri4, ri5, Rb5, Rb4)
(Na Ni Nz)
simpleGrading (1 1 1)
// block5
hex2D(ri5, ri6, Rb6, Rb5)
(Na Ni Nz)
simpleGrading (1 1 1)
// block6
hex2D(ri6, ri7, Rb7, Rb6)
(Na Ni Nz)
simpleGrading (1 1 1)
// block7
hex2D(ri7, ri0, Rb0, Rb7)
(Na Ni Nz)
simpleGrading (1 1 1)
// block0
hex2D(Rb0, Rb1, R1s, R0)
(Na NR Nz)
simpleGrading (1 1 1)
// block1
hex2D(Rb1, Rb2, R2, R1)
(Na NR Nz)
simpleGrading (1 1 1)
// block2
hex2D(Rb2, Rb3, R3s, R2)
(Na NR Nz)
simpleGrading (1 1 1)
// block3
hex2D(Rb3, Rb4, R4, R3)
(Na NR Nz)
simpleGrading (1 1 1)
// block4
hex2D(Rb4, Rb5, R5s, R4)
(Na NR Nz)
simpleGrading (1 1 1)
// block5
hex2D(Rb5, Rb6, R6, R5)
(Na NR Nz)
simpleGrading (1 1 1)
// block6
hex2D(Rb6, Rb7, R7s, R6)
(Na NR Nz)
simpleGrading (1 1 1)
// block7
hex2D(Rb7, Rb0, R0, R7)
(Na NR Nz)
simpleGrading (1 1 1)
);
edges
(
arc r0b r1b evert(0, 0, Zb)
arc r1b r2sb evert(0, 1, Zb)
arc r2b r3b evert(0, 2, Zb)
arc r3b r4sb evert(0, 3, Zb)
arc r4b r5b evert(0, 4, Zb)
arc r5b r6sb evert(0, 5, Zb)
arc r6b r7b evert(0, 6, Zb)
arc r7b r0sb evert(0, 7, Zb)
arc rb0b rb1b evert(1, 0, Zb)
arc rb1b rb2b evert(1, 1, Zb)
arc rb2b rb3b evert(1, 2, Zb)
arc rb3b rb4b evert(1, 3, Zb)
arc rb4b rb5b evert(1, 4, Zb)
arc rb5b rb6b evert(1, 5, Zb)
arc rb6b rb7b evert(1, 6, Zb)
arc rb7b rb0b evert(1, 7, Zb)
arc ri0b ri1b evert(2, 0, Zb)
arc ri1b ri2b evert(2, 1, Zb)
arc ri2b ri3b evert(2, 2, Zb)
arc ri3b ri4b evert(2, 3, Zb)
arc ri4b ri5b evert(2, 4, Zb)
arc ri5b ri6b evert(2, 5, Zb)
arc ri6b ri7b evert(2, 6, Zb)
arc ri7b ri0b evert(2, 7, Zb)
arc Rb0b Rb1b evert(3, 0, Zb)
arc Rb1b Rb2b evert(3, 1, Zb)
arc Rb2b Rb3b evert(3, 2, Zb)
arc Rb3b Rb4b evert(3, 3, Zb)
arc Rb4b Rb5b evert(3, 4, Zb)
arc Rb5b Rb6b evert(3, 5, Zb)
arc Rb6b Rb7b evert(3, 6, Zb)
arc Rb7b Rb0b evert(3, 7, Zb)
arc R0b R1sb evert(4, 0, Zb)
arc R1b R2b evert(4, 1, Zb)
arc R2b R3sb evert(4, 2, Zb)
arc R3b R4b evert(4, 3, Zb)
arc R4b R5sb evert(4, 4, Zb)
arc R5b R6b evert(4, 5, Zb)
arc R6b R7sb evert(4, 6, Zb)
arc R7b R0b evert(4, 7, Zb)
arc r0t r1t evert(0, 0, Zt)
arc r1t r2st evert(0, 1, Zt)
arc r2t r3t evert(0, 2, Zt)
arc r3t r4st evert(0, 3, Zt)
arc r4t r5t evert(0, 4, Zt)
arc r5t r6st evert(0, 5, Zt)
arc r6t r7t evert(0, 6, Zt)
arc r7t r0st evert(0, 7, Zt)
arc rb0t rb1t evert(1, 0, Zt)
arc rb1t rb2t evert(1, 1, Zt)
arc rb2t rb3t evert(1, 2, Zt)
arc rb3t rb4t evert(1, 3, Zt)
arc rb4t rb5t evert(1, 4, Zt)
arc rb5t rb6t evert(1, 5, Zt)
arc rb6t rb7t evert(1, 6, Zt)
arc rb7t rb0t evert(1, 7, Zt)
arc ri0t ri1t evert(2, 0, Zt)
arc ri1t ri2t evert(2, 1, Zt)
arc ri2t ri3t evert(2, 2, Zt)
arc ri3t ri4t evert(2, 3, Zt)
arc ri4t ri5t evert(2, 4, Zt)
arc ri5t ri6t evert(2, 5, Zt)
arc ri6t ri7t evert(2, 6, Zt)
arc ri7t ri0t evert(2, 7, Zt)
arc Rb0t Rb1t evert(3, 0, Zt)
arc Rb1t Rb2t evert(3, 1, Zt)
arc Rb2t Rb3t evert(3, 2, Zt)
arc Rb3t Rb4t evert(3, 3, Zt)
arc Rb4t Rb5t evert(3, 4, Zt)
arc Rb5t Rb6t evert(3, 5, Zt)
arc Rb6t Rb7t evert(3, 6, Zt)
arc Rb7t Rb0t evert(3, 7, Zt)
arc R0t R1st evert(4, 0, Zt)
arc R1t R2t evert(4, 1, Zt)
arc R2t R3st evert(4, 2, Zt)
arc R3t R4t evert(4, 3, Zt)
arc R4t R5st evert(4, 4, Zt)
arc R5t R6t evert(4, 5, Zt)
arc R6t R7st evert(4, 6, Zt)
arc R7t R0t evert(4, 7, Zt)
);
patches
(
wall rotor
(
quad2D(r0, r1)
quad2D(r1, r2s)
quad2D(r2, r3)
quad2D(r3, r4s)
quad2D(r4, r5)
quad2D(r5, r6s)
quad2D(r6, r7)
quad2D(r7, r0s)
quad2D(r0, rb0)
quad2D(r0s, rb0)
quad2D(r2, rb2)
quad2D(r2s, rb2)
quad2D(r4, rb4)
quad2D(r4s, rb4)
quad2D(r6, rb6)
quad2D(r6s, rb6)
)
wall stator
(
quad2D(R0, R1s)
quad2D(R1, R2)
quad2D(R2, R3s)
quad2D(R3, R4)
quad2D(R4, R5s)
quad2D(R5, R6)
quad2D(R6, R7s)
quad2D(R7, R0)
quad2D(R1, Rb1)
quad2D(R1s, Rb1)
quad2D(R3, Rb3)
quad2D(R3s, Rb3)
quad2D(R5, Rb5)
quad2D(R5s, Rb5)
quad2D(R7, Rb7)
quad2D(R7s, Rb7)
)
empty front
(
frontQuad(r0, r1, rb1, rb0)
frontQuad(r1, r2s, rb2, rb1)
frontQuad(r2, r3, rb3, rb2)
frontQuad(r3, r4s, rb4, rb3)
frontQuad(r4, r5, rb5, rb4)
frontQuad(r5, r6s, rb6, rb5)
frontQuad(r6, r7, rb7, rb6)
frontQuad(r7, r0s, rb0, rb7)
frontQuad(rb0, rb1, ri1, ri0)
frontQuad(rb1, rb2, ri2, ri1)
frontQuad(rb2, rb3, ri3, ri2)
frontQuad(rb3, rb4, ri4, ri3)
frontQuad(rb4, rb5, ri5, ri4)
frontQuad(rb5, rb6, ri6, ri5)
frontQuad(rb6, rb7, ri7, ri6)
frontQuad(rb7, rb0, ri0, ri7)
frontQuad(ri0, ri1, Rb1, Rb0)
frontQuad(ri1, ri2, Rb2, Rb1)
frontQuad(ri2, ri3, Rb3, Rb2)
frontQuad(ri3, ri4, Rb4, Rb3)
frontQuad(ri4, ri5, Rb5, Rb4)
frontQuad(ri5, ri6, Rb6, Rb5)
frontQuad(ri6, ri7, Rb7, Rb6)
frontQuad(ri7, ri0, Rb0, Rb7)
frontQuad(Rb0, Rb1, R1s, R0)
frontQuad(Rb1, Rb2, R2, R1)
frontQuad(Rb2, Rb3, R3s, R2)
frontQuad(Rb3, Rb4, R4, R3)
frontQuad(Rb4, Rb5, R5s, R4)
frontQuad(Rb5, Rb6, R6, R5)
frontQuad(Rb6, Rb7, R7s, R6)
frontQuad(Rb7, Rb0, R0, R7)
)
empty back
(
backQuad(r0, r1, rb1, rb0)
backQuad(r1, r2s, rb2, rb1)
backQuad(r2, r3, rb3, rb2)
backQuad(r3, r4s, rb4, rb3)
backQuad(r4, r5, rb5, rb4)
backQuad(r5, r6s, rb6, rb5)
backQuad(r6, r7, rb7, rb6)
backQuad(r7, r0s, rb0, rb7)
backQuad(rb0, rb1, ri1, ri0)
backQuad(rb1, rb2, ri2, ri1)
backQuad(rb2, rb3, ri3, ri2)
backQuad(rb3, rb4, ri4, ri3)
backQuad(rb4, rb5, ri5, ri4)
backQuad(rb5, rb6, ri6, ri5)
backQuad(rb6, rb7, ri7, ri6)
backQuad(rb7, rb0, ri0, ri7)
backQuad(ri0, ri1, Rb1, Rb0)
backQuad(ri1, ri2, Rb2, Rb1)
backQuad(ri2, ri3, Rb3, Rb2)
backQuad(ri3, ri4, Rb4, Rb3)
backQuad(ri4, ri5, Rb5, Rb4)
backQuad(ri5, ri6, Rb6, Rb5)
backQuad(ri6, ri7, Rb7, Rb6)
backQuad(ri7, ri0, Rb0, Rb7)
backQuad(Rb0, Rb1, R1s, R0)
backQuad(Rb1, Rb2, R2, R1)
backQuad(Rb2, Rb3, R3s, R2)
backQuad(Rb3, Rb4, R4, R3)
backQuad(Rb4, Rb5, R5s, R4)
backQuad(Rb5, Rb6, R6, R5)
backQuad(Rb6, Rb7, R7s, R6)
backQuad(Rb7, Rb0, R0, R7)
)
);
// ************************************************************************* //

View File

@ -0,0 +1,48 @@
/*--------------------------------*- 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
(
rotor
{
type wall;
nFaces 192;
startFace 5952;
}
stator
{
type wall;
nFaces 192;
startFace 6144;
}
front
{
type empty;
nFaces 3072;
startFace 6336;
}
back
{
type empty;
nFaces 3072;
startFace 9408;
}
)
// ************************************************************************* //

File diff suppressed because it is too large Load Diff

View File

@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
transportModel Newtonian;
nu nu [ 0 2 -1 0 0 0 0 ] 1e-05;
CrossPowerLawCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
m m [ 0 0 1 0 0 0 0 ] 1;
n n [ 0 0 0 0 0 0 0 ] 1;
}
BirdCarreauCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
k k [ 0 0 1 0 0 0 0 ] 0;
n n [ 0 0 0 0 0 0 0 ] 1;
}
// ************************************************************************* //

View File

@ -0,0 +1,10 @@
#!/bin/sh
m4 < constant/polyMesh/blockMeshDict.m4 > constant/polyMesh/blockMeshDict
blockMesh
cellSet
cp system/faceSetDict_rotorFaces system/faceSetDict
faceSet
cp system/faceSetDict_noBoundaryFaces system/faceSetDict
faceSet
setsToZones -noFlipMap

View File

@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object cellSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name rotor;
action new;
topoSetSources ( zoneToCell { name rotor ; } );
// ************************************************************************* //

View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 500;
deltaT 1;
writeControl timeStep;
writeInterval 50;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
// ************************************************************************* //

View File

@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object faceSetDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name rotor;
action delete;
topoSetSources ( boundaryToFace { } );
// ************************************************************************* //

View File

@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object faceSetDict_noBoundaryFaces;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name rotor;
action delete;
topoSetSources ( boundaryToFace { } );
// ************************************************************************* //

View File

@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object faceSetDict_rotorFaces;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
name rotor;
action new;
topoSetSources ( cellToFace { set rotor ; option all ; } );
// ************************************************************************* //

View File

@ -0,0 +1,66 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
grad(p) Gauss linear;
grad(U) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phi,k) Gauss limitedLinear 1;
div(phi,epsilon) Gauss limitedLinear 1;
div((nuEff*dev(grad(U).T()))) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuEff,U) Gauss linear corrected;
laplacian((1|A(U)),p) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(U) linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p ;
}
// ************************************************************************* //

View File

@ -0,0 +1,76 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver GAMG;
tolerance 1e-08;
relTol 0.05;
smoother GaussSeidel;
cacheAgglomeration true;
nCellsInCoarsestLevel 20;
agglomerator faceAreaPair;
mergeLevels 1;
}
U
{
solver smoothSolver;
smoother GaussSeidel;
nSweeps 2;
tolerance 1e-07;
relTol 0.1;
}
k
{
solver smoothSolver;
smoother GaussSeidel;
nSweeps 2;
tolerance 1e-07;
relTol 0.1;
}
epsilon
{
solver smoothSolver;
smoother GaussSeidel;
nSweeps 2;
tolerance 1e-07;
relTol 0.1;
}
}
SIMPLE
{
nNonOrthogonalCorrectors 0;
pRefCell 0;
pRefValue 0;
}
relaxationFactors
{
p 0.3;
U 0.5;
k 0.5;
epsilon 0.5;
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- 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 volSymmTensorField;
object R;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform (0 0 0 0 0 0);
boundaryField
{
lowerWall
{
type fixedValue;
value uniform (0 0 0 0 0 0);
}
upperWall
{
type fixedValue;
value uniform (0 0 0 0 0 0);
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (10 0 0);
boundaryField
{
lowerWall
{
type fixedValue;
value uniform (0 0 0);
}
upperWall
{
type fixedValue;
value uniform (0 0 0);
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 10;
boundaryField
{
lowerWall
{
type fixedValue;
value uniform 1e-08;
}
upperWall
{
type fixedValue;
value uniform 1e-08;
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 1;
boundaryField
{
lowerWall
{
type fixedValue;
value uniform 1e-10;
}
upperWall
{
type fixedValue;
value uniform 1e-10;
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,80 @@
-0.0499719 1e-05
-0.0499122 1e-05
-0.049845 1e-05
-0.0497694 1e-05
-0.0496843 1e-05
-0.0495885 1e-05
-0.0494808 1e-05
-0.0493595 1e-05
-0.0492231 1e-05
-0.0490695 1e-05
-0.0488967 1e-05
-0.0487022 1e-05
-0.0484834 1e-05
-0.0482371 1e-05
-0.04796 1e-05
-0.0476481 1e-05
-0.0472971 1e-05
-0.0469021 1e-05
-0.0464577 1e-05
-0.0459575 1e-05
-0.0453947 1e-05
-0.0447613 1e-05
-0.0440485 1e-05
-0.0432464 1e-05
-0.0423437 1e-05
-0.0413279 1e-05
-0.0401848 1e-05
-0.0388984 1e-05
-0.0374508 1e-05
-0.0358218 1e-05
-0.0339885 1e-05
-0.0319255 1e-05
-0.029604 1e-05
-0.0269914 1e-05
-0.0240515 1e-05
-0.020743 1e-05
-0.0170199 1e-05
-0.0128301 1e-05
-0.00811521 1e-05
-0.00280937 1e-05
0.00280937 1e-05
0.00811521 1e-05
0.0128301 1e-05
0.0170199 1e-05
0.020743 1e-05
0.0240515 1e-05
0.0269914 1e-05
0.029604 1e-05
0.0319255 1e-05
0.0339885 1e-05
0.0358218 1e-05
0.0374508 1e-05
0.0388984 1e-05
0.0401848 1e-05
0.0413279 1e-05
0.0423437 1e-05
0.0432464 1e-05
0.0440485 1e-05
0.0447613 1e-05
0.0453947 1e-05
0.0459575 1e-05
0.0464577 1e-05
0.0469021 1e-05
0.0472971 1e-05
0.0476481 1e-05
0.04796 1e-05
0.0482371 1e-05
0.0484834 1e-05
0.0487022 1e-05
0.0488967 1e-05
0.0490695 1e-05
0.0492231 1e-05
0.0493595 1e-05
0.0494808 1e-05
0.0495885 1e-05
0.0496843 1e-05
0.0497694 1e-05
0.049845 1e-05
0.0499122 1e-05
0.0499719 1e-05

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object nuTilda;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
lowerWall
{
type fixedValue;
value uniform 0;
}
upperWall
{
type fixedValue;
value uniform 0;
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,192 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel LaunderSharmaKE;
turbulence on;
printCoeffs on;
laminarCoeffs
{
}
kEpsilonCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
RNGkEpsilonCoeffs
{
Cmu 0.0845;
C1 1.42;
C2 1.68;
alphak 1.39;
alphaEps 1.39;
eta0 4.38;
beta 0.012;
}
kOmegaSSTCoeffs
{
alphaK1 0.85034;
alphaK2 1;
alphaOmega1 0.5;
alphaOmega2 0.85616;
gamma1 0.5532;
gamma2 0.4403;
beta1 0.075;
beta2 0.0828;
betaStar 0.09;
a1 0.31;
c1 10;
Cmu 0.09;
}
NonlinearKEShihCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76932;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
}
LienCubicKECoeffs
{
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
}
QZetaCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaZeta 0.76923;
anisotropic no;
}
LaunderSharmaKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
LamBremhorstKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
LienCubicKELowReCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
Am 0.016;
Aepsilon 0.263;
Amu 0.00222;
}
LienLeschzinerLowReCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
Am 0.016;
Aepsilon 0.263;
Amu 0.00222;
}
LRRCoeffs
{
Cmu 0.09;
Clrr1 1.8;
Clrr2 0.6;
C1 1.44;
C2 1.92;
Cs 0.25;
Ceps 0.15;
alphaEps 0.76923;
}
LaunderGibsonRSTMCoeffs
{
Cmu 0.09;
Clg1 1.8;
Clg2 0.6;
C1 1.44;
C2 1.92;
C1Ref 0.5;
C2Ref 0.3;
Cs 0.25;
Ceps 0.15;
alphaEps 0.76923;
alphaR 1.22;
}
SpalartAllmarasCoeffs
{
alphaNut 1.5;
Cb1 0.1355;
Cb2 0.622;
Cw2 0.3;
Cw3 2;
Cv1 7.1;
Cv2 5;
}
wallFunctionCoeffs
{
kappa 0.4187;
E 9;
}
// ************************************************************************* //

View File

@ -0,0 +1,80 @@
-0.0499719 177976
-0.0499122 0
-0.049845 0
-0.0497694 0
-0.0496843 0
-0.0495885 0
-0.0494808 0
-0.0493595 0
-0.0492231 0
-0.0490695 0
-0.0488967 0
-0.0487022 0
-0.0484834 0
-0.0482371 0
-0.04796 0
-0.0476481 0
-0.0472971 0
-0.0469021 0
-0.0464577 0
-0.0459575 0
-0.0453947 0
-0.0447613 0
-0.0440485 0
-0.0432464 0
-0.0423437 0
-0.0413279 0
-0.0401848 0
-0.0388984 0
-0.0374508 0
-0.0358218 0
-0.0339885 0
-0.0319255 0
-0.029604 0
-0.0269914 0
-0.0240515 0
-0.020743 0
-0.0170199 0
-0.0128301 0
-0.00811521 0
-0.00280937 0
0.00280937 0
0.00811521 0
0.0128301 0
0.0170199 0
0.020743 0
0.0240515 0
0.0269914 0
0.029604 0
0.0319255 0
0.0339885 0
0.0358218 0
0.0374508 0
0.0388984 0
0.0401848 0
0.0413279 0
0.0423437 0
0.0432464 0
0.0440485 0
0.0447613 0
0.0453947 0
0.0459575 0
0.0464577 0
0.0469021 0
0.0472971 0
0.0476481 0
0.04796 0
0.0482371 0
0.0484834 0
0.0487022 0
0.0488967 0
0.0490695 0
0.0492231 0
0.0493595 0
0.0494808 0
0.0495885 0
0.0496843 0
0.0497694 0
0.049845 0
0.0499122 0
0.0499719 177976

View File

@ -0,0 +1,71 @@
/*--------------------------------*- 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 0.05;
vertices
(
(0 -1 0)
(0 0 0)
(0 1 0)
(0.1 -1 0)
(0.1 0 0)
(0.1 1 0)
(0 -1 0.1)
(0 0 0.1)
(0 1 0.1)
(0.1 -1 0.1)
(0.1 0 0.1)
(0.1 1 0.1)
);
blocks
(
hex (0 3 4 1 6 9 10 7) (1 40 1) simpleGrading (1 100 1)
hex (1 4 5 2 7 10 11 8) (1 40 1) simpleGrading (1 0.01 1)
);
edges
(
);
patches
(
wall lowerWall
(
(0 3 9 6)
)
wall upperWall
(
(2 8 11 5)
)
cyclic frontBack
(
(0 6 7 1)
(1 7 8 2)
(9 3 4 10)
(10 4 5 11)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- 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
(
lowerWall
{
type wall;
nFaces 1;
startFace 79;
}
upperWall
{
type wall;
nFaces 1;
startFace 80;
}
frontBack
{
type cyclic;
nFaces 160;
startFace 81;
featureCos 0.9;
}
defaultFaces
{
type empty;
nFaces 160;
startFace 241;
}
)
// ************************************************************************* //

View File

@ -0,0 +1,41 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Ubar Ubar [ 0 1 -1 0 0 0 0 ] ( 10 0 0 );
transportModel Newtonian;
nu nu [ 0 2 -1 0 0 0 0 ] 1e-05;
CrossPowerLawCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
m m [ 0 0 1 0 0 0 0 ] 1;
n n [ 0 0 0 0 0 0 0 ] 1;
}
BirdCarreauCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
k k [ 0 0 1 0 0 0 0 ] 0;
n n [ 0 0 0 0 0 0 0 ] 1;
}
// ************************************************************************* //

View File

@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 1000;
deltaT 1;
writeControl timeStep;
writeInterval 100;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
graphFormat raw;
// ************************************************************************* //

View File

@ -0,0 +1,59 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,k) Gauss linear;
div(phi,epsilon) Gauss linear;
div(phi,R) Gauss linear;
div(phi,nuTilda) Gauss linear;
div((nuEff*dev(grad(U).T()))) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuEff,U) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
laplacian(DREff,R) Gauss linear corrected;
laplacian(DnuTildaEff,nuTilda) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
// ************************************************************************* //

View File

@ -0,0 +1,77 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
U
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0;
}
k
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-06;
relTol 0;
}
epsilon
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-06;
relTol 0;
}
R
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-06;
relTol 0;
}
nuTilda
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-06;
relTol 0;
}
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
}
relaxationFactors
{
U 0.5;
k 0.7;
epsilon 0.7;
R 0.7;
nuTilda 0.7;
}
// ************************************************************************* //

View File

@ -0,0 +1,44 @@
/*--------------------------------*- 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 volSymmTensorField;
object R;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform (0 0 0 0 0 0);
boundaryField
{
lowerWall
{
type zeroGradient;
}
upperWall
{
type zeroGradient;
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
lowerWall
{
type fixedValue;
value uniform (0 0 0);
}
upperWall
{
type fixedValue;
value uniform (0 0 0);
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 1e-08;
boundaryField
{
lowerWall
{
type epsilonWallFunction;
value uniform 1e-08;
}
upperWall
{
type epsilonWallFunction;
value uniform 1e-08;
}
frontBack
{
type cyclic;
value uniform 1e-08;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,210 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 1e-10;
boundaryField
{
lowerWall
{
type kQRWallFunction;
value uniform 1e-10;
}
upperWall
{
type kQRWallFunction;
value uniform 1e-10;
}
frontBack
{
type cyclic;
value nonuniform List<scalar>
160
(
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
1e-10
)
;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,80 @@
-0.049375 1e-05
-0.048125 1e-05
-0.046875 1e-05
-0.045625 1e-05
-0.044375 1e-05
-0.043125 1e-05
-0.041875 1e-05
-0.040625 1e-05
-0.039375 1e-05
-0.038125 1e-05
-0.036875 1e-05
-0.035625 1e-05
-0.034375 1e-05
-0.033125 1e-05
-0.031875 1e-05
-0.030625 1e-05
-0.029375 1e-05
-0.028125 1e-05
-0.026875 1e-05
-0.025625 1e-05
-0.024375 1e-05
-0.023125 1e-05
-0.021875 1e-05
-0.020625 1e-05
-0.019375 1e-05
-0.018125 1e-05
-0.016875 1e-05
-0.015625 1e-05
-0.014375 1e-05
-0.013125 1e-05
-0.011875 1e-05
-0.010625 1e-05
-0.009375 1e-05
-0.008125 1e-05
-0.006875 1e-05
-0.005625 1e-05
-0.004375 1e-05
-0.003125 1e-05
-0.001875 1e-05
-0.000625 1e-05
0.000625 1e-05
0.001875 1e-05
0.003125 1e-05
0.004375 1e-05
0.005625 1e-05
0.006875 1e-05
0.008125 1e-05
0.009375 1e-05
0.010625 1e-05
0.011875 1e-05
0.013125 1e-05
0.014375 1e-05
0.015625 1e-05
0.016875 1e-05
0.018125 1e-05
0.019375 1e-05
0.020625 1e-05
0.021875 1e-05
0.023125 1e-05
0.024375 1e-05
0.025625 1e-05
0.026875 1e-05
0.028125 1e-05
0.029375 1e-05
0.030625 1e-05
0.031875 1e-05
0.033125 1e-05
0.034375 1e-05
0.035625 1e-05
0.036875 1e-05
0.038125 1e-05
0.039375 1e-05
0.040625 1e-05
0.041875 1e-05
0.043125 1e-05
0.044375 1e-05
0.045625 1e-05
0.046875 1e-05
0.048125 1e-05
0.049375 1e-05

View File

@ -0,0 +1,44 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object nuTilda;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
lowerWall
{
type zeroGradient;
}
upperWall
{
type zeroGradient;
}
frontBack
{
type cyclic;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev |
| \\ / 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
{
lowerWall
{
type nutWallFunction;
value uniform 0;
}
upperWall
{
type nutWallFunction;
value uniform 0;
}
frontBack
{
type cyclic;
value uniform 0;
}
defaultFaces
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,192 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
RASModel kEpsilon;
turbulence on;
printCoeffs on;
laminarCoeffs
{
}
kEpsilonCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
RNGkEpsilonCoeffs
{
Cmu 0.0845;
C1 1.42;
C2 1.68;
alphak 1.39;
alphaEps 1.39;
eta0 4.38;
beta 0.012;
}
kOmegaSSTCoeffs
{
alphaK1 0.85034;
alphaK2 1;
alphaOmega1 0.5;
alphaOmega2 0.85616;
gamma1 0.5532;
gamma2 0.4403;
beta1 0.075;
beta2 0.0828;
betaStar 0.09;
a1 0.31;
c1 10;
Cmu 0.09;
}
NonlinearKEShihCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76932;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
}
LienCubicKECoeffs
{
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
}
QZetaCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaZeta 0.76923;
anisotropic no;
}
LaunderSharmaKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
LamBremhorstKECoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphaEps 0.76923;
}
LienCubicKELowReCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
A1 1.25;
A2 1000;
Ctau1 -4;
Ctau2 13;
Ctau3 -2;
alphaKsi 0.9;
Am 0.016;
Aepsilon 0.263;
Amu 0.00222;
}
LienLeschzinerLowReCoeffs
{
Cmu 0.09;
C1 1.44;
C2 1.92;
alphak 1;
alphaEps 0.76923;
Am 0.016;
Aepsilon 0.263;
Amu 0.00222;
}
LRRCoeffs
{
Cmu 0.09;
Clrr1 1.8;
Clrr2 0.6;
C1 1.44;
C2 1.92;
Cs 0.25;
Ceps 0.15;
alphaEps 0.76923;
}
LaunderGibsonRSTMCoeffs
{
Cmu 0.09;
Clg1 1.8;
Clg2 0.6;
C1 1.44;
C2 1.92;
C1Ref 0.5;
C2Ref 0.3;
Cs 0.25;
Ceps 0.15;
alphaEps 0.76923;
alphaR 1.22;
}
SpalartAllmarasCoeffs
{
alphaNut 1.5;
Cb1 0.1355;
Cb2 0.622;
Cw2 0.3;
Cw3 2;
Cv1 7.1;
Cv2 5;
}
wallFunctionCoeffs
{
kappa 0.4187;
E 9;
}
// ************************************************************************* //

View File

@ -0,0 +1,80 @@
-0.049375 8000
-0.048125 0
-0.046875 0
-0.045625 0
-0.044375 0
-0.043125 0
-0.041875 0
-0.040625 0
-0.039375 0
-0.038125 0
-0.036875 0
-0.035625 0
-0.034375 0
-0.033125 0
-0.031875 0
-0.030625 0
-0.029375 0
-0.028125 0
-0.026875 0
-0.025625 0
-0.024375 0
-0.023125 0
-0.021875 0
-0.020625 0
-0.019375 0
-0.018125 0
-0.016875 0
-0.015625 0
-0.014375 0
-0.013125 0
-0.011875 0
-0.010625 0
-0.009375 0
-0.008125 0
-0.006875 0
-0.005625 0
-0.004375 0
-0.003125 0
-0.001875 0
-0.000625 0
0.000625 0
0.001875 0
0.003125 0
0.004375 0
0.005625 0
0.006875 0
0.008125 0
0.009375 0
0.010625 0
0.011875 0
0.013125 0
0.014375 0
0.015625 0
0.016875 0
0.018125 0
0.019375 0
0.020625 0
0.021875 0
0.023125 0
0.024375 0
0.025625 0
0.026875 0
0.028125 0
0.029375 0
0.030625 0
0.031875 0
0.033125 0
0.034375 0
0.035625 0
0.036875 0
0.038125 0
0.039375 0
0.040625 0
0.041875 0
0.043125 0
0.044375 0
0.045625 0
0.046875 0
0.048125 0
0.049375 8000

View File

@ -0,0 +1,71 @@
/*--------------------------------*- 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 0.05;
vertices
(
(0 -1 0)
(0 0 0)
(0 1 0)
(0.1 -1 0)
(0.1 0 0)
(0.1 1 0)
(0 -1 0.1)
(0 0 0.1)
(0 1 0.1)
(0.1 -1 0.1)
(0.1 0 0.1)
(0.1 1 0.1)
);
blocks
(
hex (0 3 4 1 6 9 10 7) (1 40 1) simpleGrading (1 1 1)
hex (1 4 5 2 7 10 11 8) (1 40 1) simpleGrading (1 1 1)
);
edges
(
);
patches
(
wall lowerWall
(
(0 3 9 6)
)
wall upperWall
(
(2 8 11 5)
)
cyclic frontBack
(
(0 6 7 1)
(1 7 8 2)
(9 3 4 10)
(10 4 5 11)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- 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
(
lowerWall
{
type wall;
nFaces 1;
startFace 79;
}
upperWall
{
type wall;
nFaces 1;
startFace 80;
}
frontBack
{
type cyclic;
nFaces 160;
startFace 81;
featureCos 0.9;
}
defaultFaces
{
type empty;
nFaces 160;
startFace 241;
}
)
// ************************************************************************* //

View File

@ -0,0 +1,41 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Ubar Ubar [ 0 1 -1 0 0 0 0 ] ( 10 0 0 );
transportModel Newtonian;
nu nu [ 0 2 -1 0 0 0 0 ] 1e-05;
CrossPowerLawCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
m m [ 0 0 1 0 0 0 0 ] 1;
n n [ 0 0 0 0 0 0 0 ] 1;
}
BirdCarreauCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
k k [ 0 0 1 0 0 0 0 ] 0;
n n [ 0 0 0 0 0 0 0 ] 1;
}
// ************************************************************************* //

View File

@ -0,0 +1,49 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 1000;
deltaT 1;
writeControl timeStep;
writeInterval 100;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
graphFormat raw;
// ************************************************************************* //

View File

@ -0,0 +1,59 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default steadyState;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,k) Gauss linear;
div(phi,epsilon) Gauss linear;
div(phi,R) Gauss linear;
div(phi,nuTilda) Gauss linear;
div((nuEff*dev(grad(U).T()))) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nuEff,U) Gauss linear corrected;
laplacian(DkEff,k) Gauss linear corrected;
laplacian(DepsilonEff,epsilon) Gauss linear corrected;
laplacian(DREff,R) Gauss linear corrected;
laplacian(DnuTildaEff,nuTilda) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
// ************************************************************************* //

View File

@ -0,0 +1,79 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
U
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0;
}
k
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-06;
relTol 0;
}
epsilon
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-06;
relTol 0;
}
R
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-06;
relTol 0;
}
nuTilda
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-06;
relTol 0;
}
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
momentumPredictor yes;
fluxGradp no;
}
relaxationFactors
{
U 0.5;
k 0.7;
epsilon 0.7;
R 0.7;
nuTilda 0.7;
}
// ************************************************************************* //

View File

@ -0,0 +1,54 @@
/*--------------------------------*- 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 volTensorField;
object B;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform (0 0 0 0 0 0 0 0 0);
boundaryField
{
bottomWall
{
type zeroGradient;
}
topWall
{
type zeroGradient;
}
sides1
{
type cyclic;
}
sides2
{
type cyclic;
}
inout1
{
type cyclic;
}
inout2
{
type cyclic;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0.1335 0 0);
boundaryField
{
bottomWall
{
type fixedValue;
value uniform (0 0 0);
}
topWall
{
type fixedValue;
value uniform (0 0 0);
}
sides1
{
type cyclic;
}
sides2
{
type cyclic;
}
inout1
{
type cyclic;
}
inout2
{
type cyclic;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
bottomWall
{
type fixedValue;
value uniform 0;
}
topWall
{
type fixedValue;
value uniform 0;
}
sides1
{
type cyclic;
}
sides2
{
type cyclic;
}
inout1
{
type cyclic;
}
inout2
{
type cyclic;
}
}
// ************************************************************************* //

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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 nuSgs;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
bottomWall
{
type zeroGradient;
}
topWall
{
type zeroGradient;
}
sides1
{
type cyclic;
}
sides2
{
type cyclic;
}
inout1
{
type cyclic;
}
inout2
{
type cyclic;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object nuTilda;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
bottomWall
{
type fixedValue;
value uniform 0;
}
topWall
{
type fixedValue;
value uniform 0;
}
sides1
{
type cyclic;
}
sides2
{
type cyclic;
}
inout1
{
type cyclic;
}
inout2
{
type cyclic;
}
}
// ************************************************************************* //

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@ -0,0 +1,54 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
bottomWall
{
type zeroGradient;
}
topWall
{
type zeroGradient;
}
sides1
{
type cyclic;
}
sides2
{
type cyclic;
}
inout1
{
type cyclic;
}
inout2
{
type cyclic;
}
}
// ************************************************************************* //

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#!/bin/sh
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Get application directory
parentDir=`dirname $PWD`
application=`basename $parentDir`
runApplication blockMesh
runApplication $application
runApplication postChannel

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object LESProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
LESModel oneEqEddy;
turbulence on;
printCoeffs on;
delta vanDriest;
laminarCoeffs
{
}
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;
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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@ -0,0 +1,81 @@
/*--------------------------------*- 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;
vertices
(
(0 0 0)
(4 0 0)
(0 1 0)
(4 1 0)
(0 2 0)
(4 2 0)
(0 0 2)
(4 0 2)
(0 1 2)
(4 1 2)
(0 2 2)
(4 2 2)
);
blocks
(
hex (0 1 3 2 6 7 9 8) (40 25 30) simpleGrading (1 10.7028 1)
hex (2 3 5 4 8 9 11 10) (40 25 30) simpleGrading (1 0.0984 1)
);
edges
(
);
patches
(
wall bottomWall
(
(0 1 7 6)
)
wall topWall
(
(4 10 11 5)
)
cyclic sides1
(
(0 2 3 1)
(6 7 9 8)
)
cyclic sides2
(
(2 4 5 3)
(8 9 11 10)
)
cyclic inout1
(
(1 3 9 7)
(0 6 8 2)
)
cyclic inout2
(
(3 5 11 9)
(2 8 10 4)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

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@ -0,0 +1,61 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
6
(
bottomWall
{
type wall;
nFaces 1200;
startFace 175300;
}
topWall
{
type wall;
nFaces 1200;
startFace 176500;
}
sides1
{
type cyclic;
nFaces 2000;
startFace 177700;
featureCos 0.9;
}
sides2
{
type cyclic;
nFaces 2000;
startFace 179700;
featureCos 0.9;
}
inout1
{
type cyclic;
nFaces 1500;
startFace 181700;
featureCos 0.9;
}
inout2
{
type cyclic;
nFaces 1500;
startFace 183200;
featureCos 0.9;
}
)
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object postChannelDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
patches ( bottomWall );
component y;
symmetric true;
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Ubar Ubar [ 0 1 -1 0 0 0 0 ] ( 0.1335 0 0 );
transportModel Newtonian;
nu nu [ 0 2 -1 0 0 0 0 ] 2e-05;
CrossPowerLawCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
m m [ 0 0 1 0 0 0 0 ] 1;
n n [ 0 0 0 0 0 0 0 ] 1;
}
BirdCarreauCoeffs
{
nu0 nu0 [ 0 2 -1 0 0 0 0 ] 1e-06;
nuInf nuInf [ 0 2 -1 0 0 0 0 ] 1e-06;
k k [ 0 0 1 0 0 0 0 ] 0;
n n [ 0 0 0 0 0 0 0 ] 1;
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 1000;
deltaT 0.2;
writeControl timeStep;
writeInterval 200;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
functions ( fieldAverage1 { type fieldAverage ; functionObjectLibs ( "libfieldFunctionObjects.so" ) ; enabled true ; outputControl outputTime ; fields ( U { mean on ; prime2Mean on ; base time ; } p { mean on ; prime2Mean on ; base time ; } ) ; } );
// ************************************************************************* //

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

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0.05;
}
pFinal
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0;
}
U
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
k
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
B
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
nuTilda
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
pRefCell 1001;
pRefValue 0;
}
// ************************************************************************* //

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#!/bin/sh
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
keepCases="cavity cavityGrade cavityClipped elbow"
loseCases="cavityFine cavityHighRe"
for case in $keepCases
do
(cd $case && foamCleanTutorials)
if [ "$case" = "elbow" ]
then
rm -rf $case/fluentInterface
fi
done
for case in $loseCases
do
removeCase $case
done

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#!/bin/sh
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Get application name from directory
application=${PWD##*/}
cavityCases="cavity cavityFine cavityGrade cavityHighRe cavityClipped"
runMapFields ()
{
echo "Running mapFields from $1 to $2"
mapFields $1 -case $2 -sourceTime latestTime > $2/log.mapFields 2>&1
}
runMapFieldsConsistent ()
{
echo "Running mapFields from $1 to $2"
mapFields $1 -case $2 -sourceTime latestTime -consistent > $2/log.mapFields 2>&1
}
runFluentMeshToFoam ()
{
echo "fluentMeshToFoam: converting mesh $2"
fluentMeshToFoam $2 -case $1 > $1/log.fluentMeshToFoam 2>&1
}
copySolutionDirs ()
{
echo "Copying $2/0* directory to $1"
cp -r $2/0* $1
}
setCavityFine ()
{
blockMeshDict="$case/constant/polyMesh/blockMeshDict"
controlDict="$case/system/controlDict"
sed s/"20 20 1"/"41 41 1"/g $blockMeshDict > temp.$$
mv temp.$$ $blockMeshDict
sed \
-e s/"\(startTime[ \t]*\) 0;"/"\1 0.5;"/g \
-e s/"\(endTime[ \t]*\) 0.5;"/"\1 0.7;"/g \
-e s/"\(deltaT[ \t]*\) 0.005;"/"\1 0.0025;"/g \
-e s/"\(writeControl[ \t]*\) timeStep;"/"\1 runTime;"/g \
-e s/"\(writeInterval[ \t]*\) 20;"/"\1 0.1;"/g \
$controlDict > temp.$$
mv temp.$$ $controlDict
}
setCavityHighRe ()
{
echo "Setting cavityHighRe to generate a secondary vortex"
controlDict="$case/system/controlDict"
transportProperties="$case/constant/transportProperties"
sed \
-e s/"\(startFrom[ \t]*\) startTime;"/"\1 latestTime;"/g \
-e s/"\(endTime[ \t]*\) 0.5;"/"\1 2.0;"/g \
$controlDict > temp.$$
mv temp.$$ $controlDict
sed s/"0.01"/"0.001"/g $transportProperties > temp.$$
mv temp.$$ $transportProperties
}
for case in $cavityCases
do
if [ "$case" = "cavityFine" ]
then
cloneCase cavity $case
setCavityFine
fi
if [ "$case" = "cavityHighRe" ]
then
cloneCase cavity $case
setCavityHighRe
copySolutionDirs $case cavity
fi
(cd $case && runApplication blockMesh)
#
if [ "$case" = "cavityFine" -o "$case" = "cavityGrade" ]
then
runMapFieldsConsistent $previousCase $case
fi
if [ "$case" = "cavityClipped" ]
then
cp -r $case/0 $case/0.5
runMapFields cavity $case
if [ ".`grep nonuniform $case/0.5/U`" != "." ]
then
sed -f resetFixedWallsScr $case/0.5/U > $case/0.5/U.temp
mv $case/0.5/U.temp $case/0.5/U
fi
fi
#
previousCase="$case"
#
(cd $case && runApplication $application)
done
# elbow case for testing Fluent-FOAM conversion tools
runFluentMeshToFoam elbow elbow/elbow.msh
(cd elbow && runApplication $application)
(cd elbow && runApplication foamMeshToFluent)
(cd elbow && runApplication foamDataToFluent)

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
movingWall
{
type fixedValue;
value uniform (1 0 0);
}
fixedWalls
{
type fixedValue;
value uniform (0 0 0);
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
movingWall
{
type zeroGradient;
}
fixedWalls
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,63 @@
/*--------------------------------*- 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 0.1;
vertices
(
(0 0 0)
(1 0 0)
(1 1 0)
(0 1 0)
(0 0 0.1)
(1 0 0.1)
(1 1 0.1)
(0 1 0.1)
);
blocks
(
hex (0 1 2 3 4 5 6 7) (20 20 1) simpleGrading (1 1 1)
);
edges
(
);
patches
(
wall movingWall
(
(3 7 6 2)
)
wall fixedWalls
(
(0 4 7 3)
(2 6 5 1)
(1 5 4 0)
)
empty frontAndBack
(
(0 3 2 1)
(4 5 6 7)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

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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 polyBoundaryMesh;
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
3
(
movingWall
{
type wall;
nFaces 20;
startFace 760;
}
fixedWalls
{
type wall;
nFaces 60;
startFace 780;
}
frontAndBack
{
type empty;
nFaces 800;
startFace 840;
}
)
// ************************************************************************* //

View File

@ -0,0 +1,21 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
nu nu [ 0 2 -1 0 0 0 0 ] 0.01;
// ************************************************************************* //

View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 0.5;
deltaT 0.005;
writeControl timeStep;
writeInterval 20;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
// ************************************************************************* //

View File

@ -0,0 +1,60 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / 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;
grad(p) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nu,U) Gauss linear corrected;
laplacian((1|A(U)),p) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(HbyA) linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p ;
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0;
}
U
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
pRefCell 0;
pRefValue 0;
}
// ************************************************************************* //

View File

@ -0,0 +1,41 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
lid
{
type fixedValue;
value uniform (1 0 0);
}
fixedWalls
{
type fixedValue;
value uniform (0 0 0);
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
lid
{
type zeroGradient;
}
fixedWalls
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,83 @@
/*--------------------------------*- 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 0.1;
vertices
(
(0 0 0)
(0.6 0 0)
(0 0.4 0)
(0.6 0.4 0)
(1 0.4 0)
(0 1 0)
(0.6 1 0)
(1 1 0)
(0 0 0.1)
(0.6 0 0.1)
(0 0.4 0.1)
(0.6 0.4 0.1)
(1 0.4 0.1)
(0 1 0.1)
(0.6 1 0.1)
(1 1 0.1)
);
blocks
(
hex (0 1 3 2 8 9 11 10) (12 8 1) simpleGrading (1 1 1)
hex (2 3 6 5 10 11 14 13) (12 12 1) simpleGrading (1 1 1)
hex (3 4 7 6 11 12 15 14) (8 12 1) simpleGrading (1 1 1)
);
edges
(
);
patches
(
wall lid
(
(5 13 14 6)
(6 14 15 7)
)
wall fixedWalls
(
(0 8 10 2)
(2 10 13 5)
(7 15 12 4)
(4 12 11 3)
(3 11 9 1)
(1 9 8 0)
)
empty frontAndBack
(
(0 2 3 1)
(2 5 6 3)
(3 6 7 4)
(8 9 11 10)
(10 11 14 13)
(11 12 15 14)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

View File

@ -0,0 +1,39 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
3
(
lid
{
type wall;
nFaces 20;
startFace 632;
}
fixedWalls
{
type wall;
nFaces 60;
startFace 652;
}
frontAndBack
{
type empty;
nFaces 672;
startFace 712;
}
)
// ************************************************************************* //

View File

@ -0,0 +1,21 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
nu nu [ 0 2 -1 0 0 0 0 ] 0.01;
// ************************************************************************* //

View File

@ -0,0 +1,47 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
startFrom startTime;
startTime 0.5;
stopAt endTime;
endTime 0.6;
deltaT 0.005;
writeControl timeStep;
writeInterval 20;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression uncompressed;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
// ************************************************************************* //

View File

@ -0,0 +1,60 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / 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;
grad(p) Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss linear;
}
laplacianSchemes
{
default none;
laplacian(nu,U) Gauss linear corrected;
laplacian((1|A(U)),p) Gauss linear corrected;
}
interpolationSchemes
{
default linear;
interpolate(HbyA) linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p ;
}
// ************************************************************************* //

View File

@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0;
}
U
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
}
}
PISO
{
nCorrectors 2;
nNonOrthogonalCorrectors 0;
pRefCell 0;
pRefValue 0;
}
// ************************************************************************* //

View File

@ -0,0 +1,23 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object mapFieldsDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
patchMap ( lid movingWall );
cuttingPatches ( fixedWalls );
// ************************************************************************* //

View File

@ -0,0 +1,39 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
movingWall
{
type fixedValue;
value uniform (1 0 0);
}
fixedWalls
{
type fixedValue;
value uniform (0 0 0);
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,37 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
movingWall
{
type zeroGradient;
}
fixedWalls
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,86 @@
/*--------------------------------*- 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 0.1;
vertices
(
(0 0 0)
(0.5 0 0)
(1 0 0)
(0 0.5 0)
(0.5 0.5 0)
(1 0.5 0)
(0 1 0)
(0.5 1 0)
(1 1 0)
(0 0 0.1)
(0.5 0 0.1)
(1 0 0.1)
(0 0.5 0.1)
(0.5 0.5 0.1)
(1 0.5 0.1)
(0 1 0.1)
(0.5 1 0.1)
(1 1 0.1)
);
blocks
(
hex (0 1 4 3 9 10 13 12) (10 10 1) simpleGrading (2 2 1)
hex (1 2 5 4 10 11 14 13) (10 10 1) simpleGrading (0.5 2 1)
hex (3 4 7 6 12 13 16 15) (10 10 1) simpleGrading (2 0.5 1)
hex (4 5 8 7 13 14 17 16) (10 10 1) simpleGrading (0.5 0.5 1)
);
edges
(
);
patches
(
wall movingWall
(
(6 15 16 7)
(7 16 17 8)
)
wall fixedWalls
(
(3 12 15 6)
(0 9 12 3)
(0 1 10 9)
(1 2 11 10)
(2 5 14 11)
(5 8 17 14)
)
empty frontAndBack
(
(0 3 4 1)
(1 4 5 2)
(3 6 7 4)
(4 7 8 5)
(9 10 13 12)
(10 11 14 13)
(12 13 16 15)
(13 14 17 16)
)
);
mergePatchPairs
(
);
// ************************************************************************* //

View File

@ -0,0 +1,39 @@
/*--------------------------------*- 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;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
3
(
movingWall
{
type wall;
nFaces 20;
startFace 760;
}
fixedWalls
{
type wall;
nFaces 60;
startFace 780;
}
frontAndBack
{
type empty;
nFaces 800;
startFace 840;
}
)
// ************************************************************************* //

View File

@ -0,0 +1,21 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 1.5 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
nu nu [ 0 2 -1 0 0 0 0 ] 0.01;
// ************************************************************************* //

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