ENH: XiDyMFoam: new solver and tutorials

XiDyMFoam               : compressible version of XiFoam
oscillatingCylinder     : 2D case with cylinder moving up and down
annularCombustorTurbine : part of 3D combuster using cyclicPeriodicAMI
This commit is contained in:
mattijs
2015-11-10 12:24:34 +00:00
parent 4ef54948f7
commit 031de9c4ab
67 changed files with 27925 additions and 8 deletions

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object Su;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform 0.135;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
inletField uniform 573;
internalField uniform 2400;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $inletField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object Tu;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 573;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (4 0 0);
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type cylindricalInletVelocity;
centre (-0.64 0.5 0);
axis (1 0 0);
axialVelocity 40;
radialVelocity 20;
rpm 12732; // ut=40,r=3e-2,omega=ut/r,rpm=omega*60/(2*pi)
value uniform (0 0 0);
}
outlet
{
type pressureInletOutletVelocity;
inletValue (0 0 0);
value $internalField;
}
wall
{
type movingWallVelocity;
value uniform (0 0 0);
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object Xi;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type calculated;
}
outlet
{
type calculated;
}
wall
{
//type compressible::alphatWallFunction;
//mut mut;
//value $internalField;
type calculated;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object b;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object ft;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0.0834168596800118;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type fixedValue;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [ 0 2 -2 0 0 0 0 ];
internalField uniform 6;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type turbulentIntensityKineticEnergyInlet;
intensity 0.05;
value $internalField;
}
outlet
{
type inletOutlet;
inletValue $internalField;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [ 0 2 -1 0 0 0 0 ];
internalField uniform 0;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type calculated;
}
outlet
{
type calculated;
}
wall
{
//type nutUSpaldingWallFunction;
//value $internalField;
type calculated;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 10e5;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type zeroGradient;
}
outlet
{
type waveTransmissive;
gamma 1.28;
fieldInf 10e5;
lInf 0.2;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object pPotential;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 0;
boundaryField
{
#include "${WM_PROJECT_DIR}/etc/caseDicts/setConstraintTypes"
inlet
{
type zeroGradient;
}
outlet
{
type fixedValue;
value $internalField;
}
wall
{
type zeroGradient;
}
}
// ************************************************************************* //

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#!/bin/sh
cd ${0%/*} || exit 1
. $WM_PROJECT_DIR/bin/tools/RunFunctions
./Allrun.mesh
rm -rf 0 && cp -r 0.org 0
runApplication decomposePar -force
n=$(echo processor* | wc -w)
runParallel potentialFoam $n -pName pPotential -initialiseUBCs
rm -f processor*/0/phi
runParallel XiDyMFoam $n

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#!/bin/sh
cd ${0%/*} || exit 1
. $WM_PROJECT_DIR/bin/tools/RunFunctions
rm -f log.* constant/polyMesh/*Level
runApplication blockMesh
runApplication -l log.createPatch.cyclic \
createPatch -dict system/createPatchDict.cyclic -overwrite
runApplication snappyHexMesh -overwrite
rm -rf 0
runApplication -l log.createPatch.ami \
createPatch -dict system/createPatchDict.ami -overwrite
runApplication transformPoints -scale '(0.01 0.01 0.01)'
runApplication mergeOrSplitBaffles -split -overwrite

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object combustionProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
laminarFlameSpeedCorrelation Gulders;
fuel Methane;
Su Su [ 0 1 -1 0 0 0 0 ] 0.434;
SuModel unstrained;
equivalenceRatio equivalenceRatio [ 0 0 0 0 0 0 0 ] 0.7;
sigmaExt sigmaExt [ 0 0 -1 0 0 0 0 ] 100000;
XiModel transport;
XiCoef XiCoef [ 0 0 0 0 0 0 0 ] 0.62;
XiShapeCoef XiShapeCoef [ 0 0 0 0 0 0 0 ] 1;
uPrimeCoef uPrimeCoef [ 0 0 0 0 0 0 0 ] 1;
GuldersCoeffs
{
Methane
{
W 0.422;
eta 0.15;
xi 5.18;
alpha 2;
beta -0.5;
f 2.3;
}
}
ignite yes;
ignitionProperties
{
diameter 0.03;
start 0;
duration 1;
strength 20;
}
noIgnitionProperties
{
diameter 0;
start 0;
duration 1e-30;
strength 0;
}
ignitionSites
(
{
location (-0.28 0.55 0);
$noIgnitionProperties;
}
);
ignitionSphereFraction 1;
ignitionThickness ignitionThickness [ 0 1 0 0 0 0 0 ] 0.001;
ignitionCircleFraction 0.5;
ignitionKernelArea ignitionKernelArea [ 0 2 0 0 0 0 0 ] 0.001;
// ************************************************************************* //

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/*--------------------------------*- 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 dictionary;
location "constant";
object dynamicMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dynamicFvMesh solidBodyMotionFvMesh;
motionSolverLibs ( "libfvMotionSolvers.so" );
solidBodyMotionFvMeshCoeffs
{
cellZone rotating;
solidBodyMotionFunction rotatingMotion;
rotatingMotionCoeffs
{
origin (0 0 0);
axis (1 0 0);
omega 10;
}
}
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class uniformDimensionedVectorField;
location "constant";
object g;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -2 0 0 0 0];
value ( 0 0 0 );
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: Uhe Open Source CFD Uoolbox |
| \\ / O peration | Tersion: 1.5 |
| \\ / A nd | Web: http://www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertUoMeters 1;
r0 34;
r1 39;
r2 61;
r3 66;
t -10;
u 10;
o 10;
d2r #calc "constant::mathematical::pi/180";
r0CosT #calc "$r0*cos($d2r*($t ))";
r0CosTO #calc "$r0*cos($d2r*($t+$o))";
r0CosU #calc "$r0*cos($d2r*($u ))";
r0CosUO #calc "$r0*cos($d2r*($u+$o))";
r0SinT #calc "$r0*sin($d2r*($t ))";
r0SinTO #calc "$r0*sin($d2r*($t+$o))";
r0SinU #calc "$r0*sin($d2r*($u ))";
r0SinUO #calc "$r0*sin($d2r*($u+$o))";
r1CosT #calc "$r1*cos($d2r*($t ))";
r1CosTO #calc "$r1*cos($d2r*($t+$o))";
r1CosU #calc "$r1*cos($d2r*($u ))";
r1CosUO #calc "$r1*cos($d2r*($u+$o))";
r1SinT #calc "$r1*sin($d2r*($t ))";
r1SinTO #calc "$r1*sin($d2r*($t+$o))";
r1SinU #calc "$r1*sin($d2r*($u ))";
r1SinUO #calc "$r1*sin($d2r*($u+$o))";
r2CosT #calc "$r2*cos($d2r*($t ))";
r2CosTO #calc "$r2*cos($d2r*($t+$o))";
r2CosU #calc "$r2*cos($d2r*($u ))";
r2CosUO #calc "$r2*cos($d2r*($u+$o))";
r2SinT #calc "$r2*sin($d2r*($t ))";
r2SinTO #calc "$r2*sin($d2r*($t+$o))";
r2SinU #calc "$r2*sin($d2r*($u ))";
r2SinUO #calc "$r2*sin($d2r*($u+$o))";
r3CosT #calc "$r3*cos($d2r*($t ))";
r3CosTO #calc "$r3*cos($d2r*($t+$o))";
r3CosU #calc "$r3*cos($d2r*($u ))";
r3CosUO #calc "$r3*cos($d2r*($u+$o))";
r3SinT #calc "$r3*sin($d2r*($t ))";
r3SinTO #calc "$r3*sin($d2r*($t+$o))";
r3SinU #calc "$r3*sin($d2r*($u ))";
r3SinUO #calc "$r3*sin($d2r*($u+$o))";
vertices
(
(-34 $r1CosT $r1SinT )
(-34 $r1CosTO $r1SinTO)
(-34 $r1CosU $r1SinU )
(-30 $r1CosT $r1SinT )
(-30 $r1CosTO $r1SinTO)
(-30 $r1CosU $r1SinU )
(-15 $r0CosT $r0SinT )
(-15 $r0CosTO $r0SinTO)
(-15 $r0CosU $r0SinU )
( 0 $r1CosT $r1SinT )
( 0 $r1CosTO $r1SinTO)
( 0 $r1CosU $r1SinU )
( 12 $r1CosT $r1SinT )
( 12 $r1CosTO $r1SinTO)
( 12 $r1CosU $r1SinU )
( 12 $r1CosUO $r1SinUO)
( 28 $r1CosT $r1SinT )
( 28 $r1CosTO $r1SinTO)
( 28 $r1CosU $r1SinU )
( 28 $r1CosUO $r1SinUO)
( 40 $r1CosT $r1SinT )
( 40 $r1CosTO $r1SinTO)
( 40 $r1CosU $r1SinU )
(-34 $r2CosT $r2SinT )
(-34 $r2CosTO $r2SinTO)
(-34 $r2CosU $r2SinU )
(-30 $r2CosT $r2SinT )
(-30 $r2CosTO $r2SinTO)
(-30 $r2CosU $r2SinU )
(-15 $r3CosT $r3SinT )
(-15 $r3CosTO $r3SinTO)
(-15 $r3CosU $r3SinU )
( 0 $r2CosT $r2SinT )
( 0 $r2CosTO $r2SinTO)
( 0 $r2CosU $r2SinU )
( 12 $r2CosT $r2SinT )
( 12 $r2CosTO $r2SinTO)
( 12 $r2CosU $r2SinU )
( 12 $r2CosUO $r2SinUO)
( 28 $r2CosT $r2SinT )
( 28 $r2CosTO $r2SinTO)
( 28 $r2CosU $r2SinU )
( 28 $r2CosUO $r2SinUO)
( 40 $r2CosT $r2SinT )
( 40 $r2CosTO $r2SinTO)
( 40 $r2CosU $r2SinU )
);
blocks
(
hex ( 0 1 4 3 23 24 27 26) (8 4 22) simpleGrading (1 1 1)
hex ( 1 2 5 4 24 25 28 27) (8 4 22) simpleGrading (1 1 1)
hex ( 3 4 7 6 26 27 30 29) (8 15 22) simpleGrading (1 1 1)
hex ( 4 5 8 7 27 28 31 30) (8 15 22) simpleGrading (1 1 1)
hex ( 6 7 10 9 29 30 33 32) (8 15 22) simpleGrading (1 1 1)
hex ( 7 8 11 10 30 31 34 33) (8 15 22) simpleGrading (1 1 1)
hex ( 9 10 13 12 32 33 36 35) (8 12 22) simpleGrading (1 1 1)
hex (10 11 14 13 33 34 37 36) (8 12 22) simpleGrading (1 1 1)
hex (13 14 18 17 36 37 41 40) (8 16 22) simpleGrading (1 1 1)
hex (14 15 19 18 37 38 42 41) (8 16 22) simpleGrading (1 1 1)
hex (16 17 21 20 39 40 44 43) (8 12 22) simpleGrading (1 1 1)
hex (17 18 22 21 40 41 45 44) (8 12 22) simpleGrading (1 1 1)
);
edges
(
);
defaultPatch
{
name walls;
type wall;
}
boundary
(
coupled0
{
type patch;
faces
(
( 0 3 26 23)
( 3 6 29 26)
( 6 9 32 29)
( 9 12 35 32)
(12 13 36 35)
(13 17 40 36)
(17 16 39 40)
(16 20 43 39)
);
}
coupled1
{
type patch;
faces
(
( 2 5 28 25)
( 5 8 31 28)
( 8 11 34 31)
(11 14 37 34)
(14 15 38 37)
(15 19 42 38)
(19 18 41 42)
(18 22 45 41)
);
}
inlet
{
type patch;
faces
(
(0 1 24 23)
(1 2 25 24)
);
}
outlet
{
type patch;
faces
(
(20 21 44 43)
(21 22 45 44)
);
}
);
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev-OpenCFD.feature-periodicAMIAndXiDyMFoam|
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format binary;
class polyBoundaryMesh;
location "constant/polyMesh";
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
9
(
inlet
{
type patch;
nFaces 274;
startFace 250645;
}
outlet
{
type patch;
nFaces 1280;
startFace 250919;
}
walls
{
type wall;
inGroups 1(wall);
nFaces 10444;
startFace 252199;
}
cyclic0
{
type cyclicSlip;
inGroups 1(cyclicSlip);
nFaces 3206;
startFace 262643;
matchTolerance 0.001;
transform rotational;
neighbourPatch cyclic1;
rotationAxis (1 0 0);
rotationCentre (0 0 0);
}
cyclic1
{
type cyclicSlip;
inGroups 1(cyclicSlip);
nFaces 3206;
startFace 265849;
matchTolerance 0.001;
transform rotational;
neighbourPatch cyclic0;
rotationAxis (1 0 0);
rotationCentre (0 0 0);
}
blade1
{
type wall;
inGroups 1(wall);
nFaces 2614;
startFace 269055;
}
blade2
{
type wall;
inGroups 1(wall);
nFaces 2616;
startFace 271669;
}
ami0
{
type cyclicPeriodicAMI;
inGroups 1(cyclicAMI);
nFaces 1280;
startFace 274285;
matchTolerance 0.001;
transform unknown;
neighbourPatch ami1;
periodicPatch cyclic0;
}
ami1
{
type cyclicPeriodicAMI;
inGroups 1(cyclicAMI);
nFaces 1280;
startFace 275565;
matchTolerance 0.001;
transform unknown;
neighbourPatch ami0;
periodicPatch cyclic0;
}
)
// ************************************************************************* //

View File

@ -0,0 +1,111 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type heheuPsiThermo;
mixture inhomogeneousMixture;
transport sutherland;
thermo janaf;
equationOfState perfectGas;
specie specie;
energy absoluteEnthalpy;
}
stoichiometricAirFuelMassRatio stoichiometricAirFuelMassRatio [ 0 0 0 0 0 0 0 ] 17.1256917852272;
fuel
{
specie
{
nMoles 1;
molWeight 16.0428;
}
thermodynamics
{
Tlow 200;
Thigh 6000;
Tcommon 1000;
highCpCoeffs ( 1.68347900000000e+00 1.02372400000000e-02 -3.87512900000000e-06
6.78558500000000e-10 -4.50342300000000e-14 -1.00807900000000e+04
9.62339500000000e+00 );
lowCpCoeffs ( 7.78741500000000e-01 1.74766800000000e-02 -2.78340900000000e-05
3.04970800000000e-08 -1.22393100000000e-11 -9.82522900000000e+03
1.37221900000000e+01);
}
transport
{
As 1.67212e-06;
Ts 170.672;
}
}
oxidant
{
specie
{
nMoles 1; //9.52305854241338;
molWeight 28.8504;
}
thermodynamics
{
Tlow 200;
Thigh 6000;
Tcommon 1000;
highCpCoeffs ( 3.10621870999231e+00 1.28428498601527e-03 -4.65380802511688e-07
8.15860818565581e-11 -5.44497272650050e-15 -9.95271410040158e+02
-3.84458215280579e+00 );
lowCpCoeffs ( 3.27870489047439e+00 1.34284246978981e-03 -3.17412859038611e-06
4.63345514388486e-09 -2.07961247020324e-12 -1.01725432889533e+03
4.43589451598939e+00 );
}
transport
{
As 1.67212e-06;
Ts 170.672;
}
}
burntProducts
{
specie
{
nMoles 1; //10.5230585424134;
molWeight 27.6333203887463;
}
thermodynamics
{
Tlow 200;
Thigh 6000;
Tcommon 1000;
highCpCoeffs ( 3.12621199152579e+00 1.93235833404466e-03 -7.13659150075058e-07
1.24291624549546e-10 -8.21247028136899e-15 -1.17845644935839e+04
-3.62860244355855e+00 );
lowCpCoeffs ( 3.15477967054864e+00 2.95287447890381e-03 -5.23511418470824e-06
5.99137516254551e-09 -2.40292638317596e-12 -1.18040651744366e+04
4.72596689098416e+00 );
}
transport
{
As 1.67212e-06;
Ts 170.672;
}
}
// ************************************************************************* //

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v 20 -70 -70
v 20 70 -70
v 20 70 70
v 20 -70 70
f 1 2 3
f 1 3 4

View File

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v 12.000000 0.000000 0.000000
v 20.000000 77.274066 20.705524
v 4.000000 79.695576 -6.972459
f 1 2 3

View File

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v 28.000000 0.000000 0.000000
v 20.000000 77.274066 20.705524
v 36.000000 79.695576 -6.972459
f 1 2 3

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View File

@ -0,0 +1,42 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType LES;
LES
{
LESModel kEqn;
delta cubeRootVol;
turbulence on;
printCoeffs on;
oneEqEddyCoeffs
{
Prt 1;
}
cubeRootVolCoeffs
{
deltaCoeff 1;
}
}
// ************************************************************************* //

View File

@ -0,0 +1,53 @@
/*--------------------------------*- 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 dictionary;
location "system";
object controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application pimpleFoam;
startFrom latestTime;
startTime 0;
stopAt endTime;
endTime 0.1;
deltaT 1e-4;
writeControl adjustableRunTime;
writeInterval 2e-3;
purgeWrite 0;
writeFormat binary;
writePrecision 6;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable yes;
adjustTimeStep yes;
maxCo 0.2;
// ************************************************************************* //

View File

@ -0,0 +1,88 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.1.x |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object createPatchDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// This application/dictionary controls:
// - optional: create new patches from boundary faces (either given as
// a set of patches or as a faceSet)
// - always: order faces on coupled patches such that they are opposite. This
// is done for all coupled faces, not just for any patches created.
// - optional: synchronise points on coupled patches.
// - always: remove zero-sized (non-coupled) patches (that were not added)
// 1. Create cyclic:
// - specify where the faces should come from
// - specify the type of cyclic. If a rotational specify the rotationAxis
// and centre to make matching easier
// - always create both halves in one invocation with correct 'neighbourPatch'
// setting.
// - optionally pointSync true to guarantee points to line up.
// 2. Correct incorrect cyclic:
// This will usually fail upon loading:
// "face 0 area does not match neighbour 2 by 0.0100005%"
// " -- possible face ordering problem."
// - in polyMesh/boundary file:
// - loosen matchTolerance of all cyclics to get case to load
// - or change patch type from 'cyclic' to 'patch'
// and regenerate cyclic as above
// Do a synchronisation of coupled points after creation of any patches.
// Note: this does not work with points that are on multiple coupled patches
// with transformations (i.e. cyclics).
pointSync false;//true;
tol 1e-3;
// Patches to create.
patches
(
{
name ami0;
patchInfo
{
type cyclicPeriodicAMI;
inGroups 1(cyclicAMI);
neighbourPatch ami1;
periodicPatch cyclic0;
matchTolerance $tol;
nRotationalTransforms 18;
}
constructFrom patches;
patches (ami);
}
{
name ami1;
patchInfo
{
type cyclicPeriodicAMI;
inGroups 1(cyclicAMI);
neighbourPatch ami0;
periodicPatch cyclic0;
matchTolerance $tol;
nRotationalTransforms 18;
}
constructFrom patches;
patches (ami_slave);
}
);
// ************************************************************************* //

View File

@ -0,0 +1,92 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.1.x |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object createPatchDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// This application/dictionary controls:
// - optional: create new patches from boundary faces (either given as
// a set of patches or as a faceSet)
// - always: order faces on coupled patches such that they are opposite. This
// is done for all coupled faces, not just for any patches created.
// - optional: synchronise points on coupled patches.
// - always: remove zero-sized (non-coupled) patches (that were not added)
// 1. Create cyclic:
// - specify where the faces should come from
// - specify the type of cyclic. If a rotational specify the rotationAxis
// and centre to make matching easier
// - always create both halves in one invocation with correct 'neighbourPatch'
// setting.
// - optionally pointSync true to guarantee points to line up.
// 2. Correct incorrect cyclic:
// This will usually fail upon loading:
// "face 0 area does not match neighbour 2 by 0.0100005%"
// " -- possible face ordering problem."
// - in polyMesh/boundary file:
// - loosen matchTolerance of all cyclics to get case to load
// - or change patch type from 'cyclic' to 'patch'
// and regenerate cyclic as above
// Do a synchronisation of coupled points after creation of any patches.
// Note: this does not work with points that are on multiple coupled patches
// with transformations (i.e. cyclics).
pointSync false;//true;
tol 1e-3;
// Patches to create.
patches
(
{
name cyclic0;
patchInfo
{
type cyclicSlip;
neighbourPatch cyclic1;
transform rotational;
rotationAxis (1 0 0);
rotationCentre (0 0 0);
matchTolerance $tol;
}
constructFrom patches;
patches (coupled0);
}
{
name cyclic1;
patchInfo
{
type cyclicSlip;
neighbourPatch cyclic0;
transform rotational;
rotationAxis (1 0 0);
rotationCentre (0 0 0);
matchTolerance $tol;
}
constructFrom patches;
patches (coupled1);
}
);
// ************************************************************************* //

View File

@ -0,0 +1,32 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object decomposeParDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
numberOfSubdomains 6;
method hierarchical;
hierarchicalCoeffs
{
n ( 6 1 1 );
delta 0.001;
order xyz;
}
preservePatches (cyclic0 cyclic1 ami0 ami1);
// ************************************************************************* //

View File

@ -0,0 +1,81 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default leastSquares;
grad(U) cellLimited Gauss linear 0.99;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phid,p) Gauss limitedLinear 1;
div(phi,K) Gauss limitedLinear 1;
div(phi,k) Gauss limitedLinear 1;
div(phi,epsilon) Gauss limitedLinear 1;
div(phi,R) Gauss limitedLinear 1;
div(R) Gauss linear;
div(phiXi,Xi) Gauss limitedLinear 1;
div(phiXi,Su) Gauss limitedLinear 1;
div(phiSt,b) Gauss limitedLinear01 1;
div(phi,ft_b_ha_hau) Gauss multivariateSelection
{
fu limitedLinear01 1;
ft limitedLinear01 1;
b limitedLinear01 1;
ha limitedLinear 1;
hau limitedLinear 1;
};
div(U) Gauss linear;
div((Su*n)) Gauss linear;
div((U+((Su*Xi)*n))) Gauss linear;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
div(meshPhi,p) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p ;
Phi ;
pcorr ;
}
// ************************************************************************* //

View File

@ -0,0 +1,76 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"(p|Phi|rho)"
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0.1;
minIter 1;
}
"(p|Phi|rho)Final"
{
$p;
tolerance 1e-06;
relTol 0;
minIter 1;
}
pcorr
{
$p;
tolerance 1e-02;
relTol 0;
}
"(U|b|ft|fu|Su|Xi|ha|hau|k|epsilon)"
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0.1;
minIter 1;
}
"(U|b|ft|fu|Su|Xi|ha|hau|k|epsilon)Final"
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
minIter 1;
}
}
PIMPLE
{
nOuterCorrectors 2;
nCorrectors 1;
nNonOrthogonalCorrectors 0;
}
potentialFlow
{
nNonOrthogonalCorrectors 20;
}
// ************************************************************************* //

View File

@ -0,0 +1,23 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object meshQualityDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Include defaults parameters from master dictionary
#include "$WM_PROJECT_DIR/etc/caseDicts/meshQualityDict"
maxNonOrtho 55;
// ************************************************************************* //

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@ -0,0 +1,375 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object snappyHexMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
// Which of the steps to run
castellatedMesh true;
snap true;
addLayers false;
// Geometry. Definition of all surfaces. All surfaces are of class
// searchableSurface.
// Surfaces are used
// - to specify refinement for any mesh cell intersecting it
// - to specify refinement for any mesh cell inside/outside/near
// - to 'snap' the mesh boundary to the surface
geometry
{
ami.obj
{
type triSurfaceMesh;
name ami;
}
blade1.obj
{
type triSurfaceMesh;
name blade1;
}
blade2.obj
{
type triSurfaceMesh;
name blade2;
}
inlet.stl
{
type triSurfaceMesh;
name inlet;
}
outlet.stl
{
type triSurfaceMesh;
name outlet;
}
walls.stl
{
type triSurfaceMesh;
name walls;
}
};
// Settings for the castellatedMesh generation.
castellatedMeshControls
{
// Refinement parameters
// ~~~~~~~~~~~~~~~~~~~~~
// If local number of cells is >= maxLocalCells on any processor
// switches from from refinement followed by balancing
// (current method) to (weighted) balancing before refinement.
maxLocalCells 100000;
// Overall cell limit (approximately). Refinement will stop immediately
// upon reaching this number so a refinement level might not complete.
// Note that this is the number of cells before removing the part which
// is not 'visible' from the keepPoint. The final number of cells might
// actually be a lot less.
maxGlobalCells 2000000;
// The surface refinement loop might spend lots of iterations refining just a
// few cells. This setting will cause refinement to stop if <= minimumRefine
// are selected for refinement. Note: it will at least do one iteration
// (unless the number of cells to refine is 0)
minRefinementCells 0;
// Number of buffer layers between different levels.
// 1 means normal 2:1 refinement restriction, larger means slower
// refinement.
nCellsBetweenLevels 5;
// Explicit feature edge refinement
// ~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~
// Specifies a level for any cell intersected by its edges.
// This is a featureEdgeMesh, read from constant/triSurface for now.
features
(
);
// Surface based refinement
// ~~~~~~~~~~~~~~~~~~~~~~~~
// Specifies two levels for every surface. The first is the minimum level,
// every cell intersecting a surface gets refined up to the minimum level.
// The second level is the maximum level. Cells that 'see' multiple
// intersections where the intersections make an
// angle > resolveFeatureAngle get refined up to the maximum level.
refinementSurfaces
{
ami
{
level (1 1);
cellZone rotating;
faceZone rotating;
faceType baffle;
cellZoneInside insidePoint;
insidePoint (34 50 0);
}
blade1
{
level (1 1);
faceType baffle;
}
blade2
{
level (1 1);
faceType baffle;
}
cooling
{
level (1 1);
patchInfo
{
type patch;
}
}
inlet
{
level (1 1);
patchInfo
{
type patch;
}
}
outlet
{
level (1 1);
patchInfo
{
type patch;
}
}
walls
{
level (1 1);
patchInfo
{
type wall;
inGroups (wall);
}
}
}
resolveFeatureAngle 30;
// Region-wise refinement
// ~~~~~~~~~~~~~~~~~~~~~~
// Specifies refinement level for cells in relation to a surface. One of
// three modes
// - distance. 'levels' specifies per distance to the surface the
// wanted refinement level. The distances need to be specified in
// descending order.
// - inside. 'levels' is only one entry and only the level is used. All
// cells inside the surface get refined up to the level. The surface
// needs to be closed for this to be possible.
// - outside. Same but cells outside.
refinementRegions
{
}
// Mesh selection
// ~~~~~~~~~~~~~~
// After refinement patches get added for all refinementSurfaces and
// all cells intersecting the surfaces get put into these patches. The
// section reachable from the locationInMesh is kept.
// NOTE: This point should never be on a face, always inside a cell, even
// after refinement.
// This is an outside point locationInMesh (-0.033 -0.033 0.0033);
locationInMesh (-15 50 0);
// Whether any faceZones (as specified in the refinementSurfaces)
// are only on the boundary of corresponding cellZones or also allow
// free-standing zone faces. Not used if there are no faceZones.
allowFreeStandingZoneFaces true;
}
// Settings for the snapping.
snapControls
{
//- Number of patch smoothing iterations before finding correspondence
// to surface
nSmoothPatch 3;
//- Relative distance for points to be attracted by surface feature point
// or edge. True distance is this factor times local
// maximum edge length.
tolerance 1.0;
//- Number of mesh displacement relaxation iterations.
nSolveIter 300;
//- Maximum number of snapping relaxation iterations. Should stop
// before upon reaching a correct mesh.
nRelaxIter 5;
// Feature snapping
//- Number of feature edge snapping iterations.
// Leave out altogether to disable.
nFeatureSnapIter 10;
//- Detect (geometric) features by sampling the surface
implicitFeatureSnap true;
//- Use castellatedMeshControls::features
explicitFeatureSnap false;
//- Detect features between multiple surfaces
// (only for explicitFeatureSnap, default = false)
multiRegionFeatureSnap true;
}
// Settings for the layer addition.
addLayersControls
{
// Are the thickness parameters below relative to the undistorted
// size of the refined cell outside layer (true) or absolute sizes (false).
relativeSizes true;
// Per final patch (so not geometry!) the layer information
layers
{
"blade."
{
nSurfaceLayers 2;
}
}
// Expansion factor for layer mesh
expansionRatio 1.0;
// Wanted thickness of final added cell layer. If multiple layers
// is the thickness of the layer furthest away from the wall.
// Relative to undistorted size of cell outside layer.
// See relativeSizes parameter.
finalLayerThickness 0.25;
// Minimum thickness of cell layer. If for any reason layer
// cannot be above minThickness do not add layer.
// See relativeSizes parameter.
minThickness 0.2;
// If points get not extruded do nGrow layers of connected faces that are
// also not grown. This helps convergence of the layer addition process
// close to features.
nGrow 0;
// Advanced settings
// When not to extrude surface. 0 is flat surface, 90 is when two faces
// are perpendicular
featureAngle 30;
// Maximum number of snapping relaxation iterations. Should stop
// before upon reaching a correct mesh.
nRelaxIter 5;
// Number of smoothing iterations of surface normals
nSmoothSurfaceNormals 1;
// Number of smoothing iterations of interior mesh movement direction
nSmoothNormals 3;
// Smooth layer thickness over surface patches
nSmoothThickness 10;
// Stop layer growth on highly warped cells
maxFaceThicknessRatio 0.5;
// Reduce layer growth where ratio thickness to medial
// distance is large
maxThicknessToMedialRatio 0.3;
// Angle used to pick up medial axis points
minMedianAxisAngle 90;
// Create buffer region for new layer terminations
nBufferCellsNoExtrude 0;
// Overall max number of layer addition iterations. The mesher will exit
// if it reaches this number of iterations; possibly with an illegal
// mesh.
nLayerIter 50;
// Max number of iterations after which relaxed meshQuality controls
// get used. Up to nRelaxIter it uses the settings in meshQualityControls,
// after nRelaxIter it uses the values in meshQualityControls::relaxed.
nRelaxedIter 20;
}
// Generic mesh quality settings. At any undoable phase these determine
// where to undo.
meshQualityControls
{
#include "meshQualityDict"
// Optional : some meshing phases allow usage of relaxed rules.
// See e.g. addLayersControls::nRelaxedIter.
relaxed
{
//- Maximum non-orthogonality allowed. Set to 180 to disable.
maxNonOrtho 75;
}
// Advanced
//- Number of error distribution iterations
nSmoothScale 4;
//- amount to scale back displacement at error points
errorReduction 0.75;
}
// Advanced
// Write flags
writeFlags
(
scalarLevels // write volScalarField with cellLevel for postprocessing
layerSets // write cellSets, faceSets of faces in layer
layerFields // write volScalarField for layer coverage
);
// Merge tolerance. Is fraction of overall bounding box of initial mesh.
// Note: the write tolerance needs to be higher than this.
mergeTolerance 1E-6;
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object Su;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform 0.135;
boundaryField
{
"(walls|cylinder)"
{
type zeroGradient;
}
"inlet.*"
{
type fixedValue;
value uniform 0.135;
}
outlet
{
type inletOutlet;
inletValue uniform 0.135;
value uniform 0.135;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,46 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 300;
boundaryField
{
"(walls|cylinder)"
{
type zeroGradient;
}
"inlet.*"
{
type fixedValue;
value uniform 300;
}
outlet
{
type inletOutlet;
inletValue uniform 300;
value uniform 300;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,46 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object Tu;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 300;
boundaryField
{
"(walls|cylinder)"
{
type zeroGradient;
}
"inlet.*"
{
type fixedValue;
value uniform 300;
}
outlet
{
type inletOutlet;
inletValue uniform 300;
value uniform 300;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,62 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volVectorField;
location "0";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (2 0 0);
/*
A=[2 1]
M=[28.8504 16.0428]
AFR=17.1256917852
T=300
p=1e5
R=8314.3
rho=p/R/T.*M
U=[2 NaN]
U(2)=rho(1)*U(1)*A(1)/(rho(2)*A(2))/AFR
*/
boundaryField
{
"(walls|cylinder)"
{
type fixedValue;
value uniform (0 0 0);
}
inletAir
{
type fixedValue;
value uniform (2 0 0);
}
inletFuel
{
type fixedValue;
value uniform (0.42003 0 0);
}
outlet
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,46 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object Xi;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
"(walls|cylinder)"
{
type zeroGradient;
}
"inlet.*"
{
type fixedValue;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,45 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
"(walls|cylinder)"
{
type compressible::alphatWallFunction;
Prt 0.85;
value uniform 0;
}
"inlet.*"
{
type zeroGradient;
}
outlet
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,46 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object b;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
"(walls|cylinder)"
{
type zeroGradient;
}
"inlet.*"
{
type fixedValue;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 1;
value uniform 1;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / 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 100;
boundaryField
{
"(walls|cylinder)"
{
type epsilonWallFunction;
value uniform 100;
}
"inlet.*"
{
type turbulentMixingLengthDissipationRateInlet;
mixingLength 0.001;
value uniform 100;
}
outlet
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,51 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object ft;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
"(walls|cylinder)"
{
type zeroGradient;
}
inletAir
{
type fixedValue;
value uniform 0;
}
inletFuel
{
type fixedValue;
value uniform 1;
}
outlet
{
type inletOutlet;
inletValue uniform 0;
value uniform 0;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / 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 1;
boundaryField
{
"(walls|cylinder)"
{
type kqRWallFunction;
value uniform 1;
}
"inlet.*"
{
type turbulentIntensityKineticEnergyInlet;
intensity 0.04;
value uniform 1;
}
outlet
{
type zeroGradient;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,46 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object mut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
"(walls|cylinder)"
{
type nutkWallFunction;
value uniform 0;
}
"inlet.*"
{
type calculated;
value uniform 0;
}
outlet
{
type calculated;
value uniform 0;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class volScalarField;
location "0";
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 100000;
boundaryField
{
"(walls|cylinder)"
{
type zeroGradient;
}
"inlet.*"
{
type zeroGradient;
}
outlet
{
type fixedValue;
value uniform 100000;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,59 @@
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class pointScalarField;
location "0";
object pointDisplacementy;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
walls
{
type fixedValue;
value $internalField;
}
cylinder
{
type codedFixedValue;
redirectType pointDisplacementy_cylinder;
code
#{
const scalar t = this->db().time().value();
const scalar a = 0.001;
const scalar f = 200;
operator==(a*sin(constant::mathematical::twoPi*f*t));
#};
value $internalField;
}
"inlet.*"
{
type fixedValue;
value $internalField;
}
outlet
{
type fixedValue;
value $internalField;
}
frontAndBack
{
type empty;
}
}
// ************************************************************************* //

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@ -0,0 +1,25 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / 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;
// ************************************************************************* //

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/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object combustionProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
laminarFlameSpeedCorrelation Gulders;
fuel Methane;
Su Su [ 0 1 -1 0 0 0 0 ] 0;
SuModel unstrained;
equivalenceRatio equivalenceRatio [ 0 0 0 0 0 0 0 ] 1;
sigmaExt sigmaExt [ 0 0 -1 0 0 0 0 ] 100000;
XiModel transport;
XiCoef XiCoef [ 0 0 0 0 0 0 0 ] 0.62;
XiShapeCoef XiShapeCoef [ 0 0 0 0 0 0 0 ] 1;
uPrimeCoef uPrimeCoef [ 0 0 0 0 0 0 0 ] 1;
GuldersCoeffs
{
Methane
{
W 0.422;
eta 0.15;
xi 5.18;
alpha 2;
beta -0.5;
f 2.3;
}
}
ignite yes;
ignitionSites
(
{
location (0.006 0 0.0005);
diameter 0.001;
start 0.02;
duration 0.04;
strength 5;
}
);
ignitionSphereFraction 1;
ignitionThickness ignitionThickness [ 0 1 0 0 0 0 0 ] 0.001;
ignitionCircleFraction 0.5;
ignitionKernelArea ignitionKernelArea [ 0 2 0 0 0 0 0 ] 0.001;
// ************************************************************************* //

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@ -0,0 +1,34 @@
/*--------------------------------*- 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 dictionary;
location "constant";
object dynamicMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dynamicFvMesh dynamicMotionSolverFvMesh;
motionSolverLibs ( "libfvMotionSolvers.so" );
solver displacementComponentLaplacian;
displacementComponentLaplacianCoeffs
{
component y;
diffusivity uniform;
applyPointLocation false;
}
// ************************************************************************* //

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@ -0,0 +1,22 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class uniformDimensionedVectorField;
location "constant";
object g;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -2 0 0 0 0];
value ( 0 0 0 );
// ************************************************************************* //

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@ -0,0 +1,156 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
object blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
convertToMeters 0.001;
vertices
(
(-15 -6 0)
(-15 -2 0)
(-15 2 0)
(-15 6 0)
( -6 -6 0)
( -6 -2 0)
( -6 2 0)
( -6 6 0)
( -2.82842712474619 -2.82842712474619 0)
( -3.86370330515627 -1.03527618041008 0)
( -3.86370330515627 1.03527618041008 0)
( -2.82842712474619 2.82842712474619 0)
( 2.82842712474619 -2.82842712474619 0)
( 2.82842712474619 2.82842712474619 0)
( 6 -6 0)
( 6 6 0)
( 50 -6 0)
( 50 6 0)
(-15 -6 1)
(-15 -2 1)
(-15 2 1)
(-15 6 1)
( -6 -6 1)
( -6 -2 1)
( -6 2 1)
( -6 6 1)
( -2.82842712474619 -2.82842712474619 1)
( -3.86370330515627 -1.03527618041008 1)
( -3.86370330515627 1.03527618041008 1)
( -2.82842712474619 2.82842712474619 1)
( 2.82842712474619 -2.82842712474619 1)
( 2.82842712474619 2.82842712474619 1)
( 6 -6 1)
( 6 6 1)
( 50 -6 1)
( 50 6 1)
);
blocks
(
hex ( 0 4 5 1 18 22 23 19) (16 8 1) simpleGrading (1 1 1)
hex ( 1 5 6 2 19 23 24 20) (16 8 1) simpleGrading (1 1 1)
hex ( 2 6 7 3 20 24 25 21) (16 8 1) simpleGrading (1 1 1)
hex ( 4 8 9 5 22 26 27 23) ( 8 8 1) simpleGrading (1 1 1)
hex ( 5 9 10 6 23 27 28 24) ( 8 8 1) simpleGrading (1 1 1)
hex ( 6 10 11 7 24 28 29 25) ( 8 8 1) simpleGrading (1 1 1)
hex ( 4 14 12 8 22 32 30 26) (24 8 1) simpleGrading (1 1 1)
hex (12 14 15 13 30 32 33 31) ( 8 24 1) simpleGrading (1 1 1)
hex (11 13 15 7 29 31 33 25) (24 8 1) simpleGrading (1 1 1)
hex (14 16 17 15 32 34 35 33) (80 24 1) simpleGrading (1 1 1)
);
edges
(
arc 8 9 (-3.46410161513775 2 0)
arc 9 10 (-4 0 0)
arc 10 11 (-3.46410161513775 2 0)
arc 11 13 ( 0 4 0)
arc 13 12 ( 4 0 0)
arc 12 8 ( 0 -4 0)
arc 26 27 (-3.46410161513775 2 1)
arc 27 28 (-4 0 1)
arc 28 29 (-3.46410161513775 2 1)
arc 29 31 ( 0 4 1)
arc 31 30 ( 4 0 1)
arc 30 26 ( 0 -4 1)
);
defaultPatch
{
name frontAndBack;
type empty;
}
boundary
(
inletAir
{
type patch;
faces
(
(0 1 19 18)
(2 3 21 20)
);
}
inletFuel
{
type patch;
faces
(
(1 2 20 19)
);
}
outlet
{
type patch;
faces
(
(16 17 35 34)
);
}
walls
{
type wall;
faces
(
( 0 4 22 18)
( 3 7 25 21)
( 4 14 32 22)
( 7 15 33 25)
(14 16 34 32)
(15 17 35 33)
);
}
cylinder
{
type wall;
faces
(
( 8 9 27 26)
( 9 10 28 27)
(10 11 29 28)
(11 13 31 29)
(13 12 30 31)
(12 8 26 30)
);
}
);
mergePatchPairs
(
);
// ************************************************************************* //

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@ -0,0 +1,61 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: dev-OpenCFD.feature-periodicAMIAndXiDyMFoam|
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class polyBoundaryMesh;
location "constant/polyMesh";
object boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
6
(
inletAir
{
type patch;
nFaces 16;
startFace 5952;
}
inletFuel
{
type patch;
nFaces 8;
startFace 5968;
}
outlet
{
type patch;
nFaces 24;
startFace 5976;
}
walls
{
type wall;
inGroups 1(wall);
nFaces 240;
startFace 6000;
}
cylinder
{
type wall;
inGroups 1(wall);
nFaces 96;
startFace 6240;
}
frontAndBack
{
type empty;
inGroups 1(empty);
nFaces 6144;
startFace 6336;
}
)
// ************************************************************************* //

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@ -0,0 +1,115 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type heheuPsiThermo;
mixture inhomogeneousMixture;
transport sutherland;
thermo janaf;
equationOfState perfectGas;
specie specie;
energy absoluteEnthalpy;
}
stoichiometricAirFuelMassRatio stoichiometricAirFuelMassRatio [ 0 0 0 0 0 0 0 ] 17.1256917852;
fuel
{
specie
{
nMoles 1;
molWeight 16.0428;
}
thermodynamics
{
Tlow 200;
Thigh 6000;
Tcommon 1000;
highCpCoeffs ( 1.68347900000000e+00 1.02372400000000e-02 -3.87512900000000e-06
6.78558500000000e-10 -4.50342300000000e-14 -1.00807900000000e+04
9.62339500000000e+00 );
lowCpCoeffs ( 7.78741500000000e-01 1.74766800000000e-02 -2.78340900000000e-05
3.04970800000000e-08 -1.22393100000000e-11 -9.82522900000000e+03
1.37221900000000e+01);
}
transport
{
As 1.67212e-06;
Ts 170.672;
}
}
oxidant
{
specie
{
nMoles 1;
molWeight 28.8504;
}
thermodynamics
{
Tlow 200;
Thigh 6000;
Tcommon 1000;
highCpCoeffs ( 3.0885497471e+00 1.3043264856e-03 -4.7552447148e-07
8.3493327980e-11 -5.5737056214e-15 -9.8814063549e+02
-4.0547404058e+00 );
lowCpCoeffs ( 3.2806699701e+00 1.3492770106e-03 -3.2517684297e-06
4.7326393524e-09 -2.1155491172e-12 -1.0176130308e+03
4.3881233780e+00 );
}
transport
{
As 1.67212e-06;
Ts 170.672;
}
}
burntProducts
{
specie
{
nMoles 1;
molWeight 27.6333203887;
}
thermodynamics
{
Tlow 200;
Thigh 6000;
Tcommon 1000;
highCpCoeffs ( 3.0233794599e+00 1.9430560990e-03 -6.9382318371e-07
1.1776092714e-10 -7.6289056653e-15 -1.0995628377e+04
-3.0620017962e+00 );
lowCpCoeffs ( 3.2182230144e+00 2.6101069239e-03 -5.0302916124e-06
6.0101629539e-09 -2.4254586430e-12 -1.1068041672e+04
4.2846702447e+00 );
}
transport
{
As 1.67212e-06;
Ts 170.672;
}
}
// ************************************************************************* //

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@ -0,0 +1,30 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "constant";
object turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
RASModel kEpsilon;
turbulence on;
printCoeffs on;
}
// ************************************************************************* //

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@ -0,0 +1,55 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.2.1 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object controlDict.1st;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application XiDyMFoam;
startFrom startTime;
startTime 0;
stopAt endTime;
endTime 0.1;
deltaT 1e-5;
writeControl adjustableRunTime;
writeInterval 1e-3;
purgeWrite 0;
writeFormat ascii;
writePrecision 8;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
adjustTimeStep yes;
maxCo 0.4;
libs ( "libfvMotionSolvers.so" );
// ************************************************************************* //

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@ -0,0 +1,79 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss limitedLinearV 1;
div(phid,p) Gauss limitedLinear 1;
div(phi,K) Gauss limitedLinear 1;
div(phi,k) Gauss limitedLinear 1;
div(phi,epsilon) Gauss limitedLinear 1;
div(phi,R) Gauss limitedLinear 1;
div(R) Gauss linear;
div(phiXi,Xi) Gauss limitedLinear 1;
div(phiXi,Su) Gauss limitedLinear 1;
div(phiSt,b) Gauss limitedLinear01 1;
div(phi,ft_b_ha_hau) Gauss multivariateSelection
{
fu limitedLinear01 1;
ft limitedLinear01 1;
b limitedLinear01 1;
ha limitedLinear 1;
hau limitedLinear 1;
};
div(U) Gauss linear;
div((Su*n)) Gauss linear;
div((U+((Su*Xi)*n))) Gauss linear;
div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
div(meshPhi,p) Gauss linear;
}
laplacianSchemes
{
default Gauss linear corrected;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default corrected;
}
fluxRequired
{
default no;
p ;
pcorr ;
}
// ************************************************************************* //

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@ -0,0 +1,71 @@
/*--------------------------------*- C++ -*----------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: 2.3.0 |
| \\ / A nd | Web: www.OpenFOAM.org |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
FoamFile
{
version 2.0;
format ascii;
class dictionary;
location "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
"(p|rho|cellDisplacementy)"
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0.1;
minIter 1;
}
"(p|rho|cellDisplacementy)Final"
{
$p;
tolerance 1e-06;
relTol 0;
minIter 1;
}
pcorr
{
$p;
tolerance 1e-2;
relTol 0;
}
"(U|b|ft|fu|Su|Xi|ha|hau|k|epsilon)"
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0.1;
minIter 1;
}
"(U|b|ft|fu|Su|Xi|ha|hau|k|epsilon)Final"
{
solver PBiCG;
preconditioner DILU;
tolerance 1e-05;
relTol 0;
minIter 1;
}
}
PIMPLE
{
nOuterCorrectors 2;
nCorrectors 1;
nNonOrthogonalCorrectors 0;
}
// ************************************************************************* //