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engineFoam: Renamed engineFoam -> XiEngineFoam and sprayEngineFoam -> engineFoam

Browse Source 
XiEngineFoam is a premixed/partially-premixed combustion engine solver which
exclusively uses the Xi flamelet combustion model.

engineFoam is a general engine solver for inhomogeneous combustion with or
without spray supporting run-time selection of the chemistry-based combustion
model.
This commit is contained in:
Henry Weller
2017-09-19 17:01:54 +01:00
parent 24a06d3bae
commit 50912f87cf
60 changed files with 10 additions and 16 deletions
Download Patch File Download Diff File Expand all files Collapse all files

41
tutorials/combustion/XiEngineFoam/kivaTest/-180/Su Normal file
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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 volScalarField;
location "-180";
object Su;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform 0.4;
boundaryField
{
piston
{
type zeroGradient;
}
liner
{
type zeroGradient;
}
cylinderHead
{
type zeroGradient;
}
}
// ************************************************************************* //

44
tutorials/combustion/XiEngineFoam/kivaTest/-180/T Normal file
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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 volScalarField;
location "-180";
object T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 373;
boundaryField
{
piston
{
type fixedValue;
value uniform 433;
}
liner
{
type fixedValue;
value uniform 373;
}
cylinderHead
{
type fixedValue;
value uniform 383;
}
}
// ************************************************************************* //

44
tutorials/combustion/XiEngineFoam/kivaTest/-180/Tu Normal file
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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 volScalarField;
location "-180";
object Tu;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 1 0 0 0];
internalField uniform 373;
boundaryField
{
piston
{
type fixedValue;
value uniform 433;
}
liner
{
type fixedValue;
value uniform 373;
}
cylinderHead
{
type fixedValue;
value uniform 383;
}
}
// ************************************************************************* //

42
tutorials/combustion/XiEngineFoam/kivaTest/-180/U Normal file
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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 volVectorField;
location "-180";
object U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 1 -1 0 0 0 0];
internalField uniform (0 0 0);
boundaryField
{
piston
{
type movingWallVelocity;
value uniform (0 0 0);
}
liner
{
type noSlip;
}
cylinderHead
{
type noSlip;
}
}
// ************************************************************************* //

41
tutorials/combustion/XiEngineFoam/kivaTest/-180/Xi Normal file
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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 volScalarField;
location "-180";
object Xi;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
piston
{
type zeroGradient;
}
liner
{
type zeroGradient;
}
cylinderHead
{
type zeroGradient;
}
}
// ************************************************************************* //

45
tutorials/combustion/XiEngineFoam/kivaTest/-180/alphat Normal file
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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 volScalarField;
location "-180";
object alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
piston
{
type compressible::alphatWallFunction;
Prt 0.85;
value uniform 0;
}
liner
{
type compressible::alphatWallFunction;
Prt 0.85;
value uniform 0;
}
cylinderHead
{
type compressible::alphatWallFunction;
Prt 0.85;
value uniform 0;
}
}
// ************************************************************************* //

41
tutorials/combustion/XiEngineFoam/kivaTest/-180/b Normal file
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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 volScalarField;
location "-180";
object b;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 1;
boundaryField
{
piston
{
type zeroGradient;
}
liner
{
type zeroGradient;
}
cylinderHead
{
type zeroGradient;
}
}
// ************************************************************************* //

51
tutorials/combustion/XiEngineFoam/kivaTest/-180/epsilon Normal file
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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 volScalarField;
location "-180";
object epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -3 0 0 0 0];
internalField uniform 450;
boundaryField
{
piston
{
type epsilonWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 450;
}
liner
{
type epsilonWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 450;
}
cylinderHead
{
type epsilonWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 450;
}
}
// ************************************************************************* //

42
tutorials/combustion/XiEngineFoam/kivaTest/-180/ft Normal file
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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 volScalarField;
location "-180";
object ft;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0.0623;
boundaryField
{
piston
{
type zeroGradient;
}
liner
{
type zeroGradient;
}
cylinderHead
{
type zeroGradient;
}
}
// ************************************************************************* //

41
tutorials/combustion/XiEngineFoam/kivaTest/-180/fu Normal file
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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 volScalarField;
location "-180";
object fu;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 0 0 0 0 0 0];
internalField uniform 0;
boundaryField
{
piston
{
type zeroGradient;
}
liner
{
type zeroGradient;
}
cylinderHead
{
type zeroGradient;
}
}
// ************************************************************************* //

42
tutorials/combustion/XiEngineFoam/kivaTest/-180/k Normal file
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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 volScalarField;
location "-180";
object k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -2 0 0 0 0];
internalField uniform 4;
boundaryField
{
piston
{
type kqRWallFunction;
value uniform 4;
}
liner
{
type kqRWallFunction;
value uniform 4;
}
cylinderHead
{
type kqRWallFunction;
value uniform 4;
}
}
// ************************************************************************* //

51
tutorials/combustion/XiEngineFoam/kivaTest/-180/nut Normal file
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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 volScalarField;
location "-180";
object nut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [0 2 -1 0 0 0 0];
internalField uniform 0;
boundaryField
{
piston
{
type nutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
liner
{
type nutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
cylinderHead
{
type nutkWallFunction;
Cmu 0.09;
kappa 0.41;
E 9.8;
value uniform 0;
}
}
// ************************************************************************* //

41
tutorials/combustion/XiEngineFoam/kivaTest/-180/p Normal file
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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 volScalarField;
location "-180";
object p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions [1 -1 -2 0 0 0 0];
internalField uniform 100000;
boundaryField
{
piston
{
type zeroGradient;
}
liner
{
type zeroGradient;
}
cylinderHead
{
type zeroGradient;
}
}
// ************************************************************************* //

15
tutorials/combustion/XiEngineFoam/kivaTest/Allclean Executable file
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#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial clean functions
. $WM_PROJECT_DIR/bin/tools/CleanFunctions
mv ./-180 temp180
cleanCase
rm -rf 0 > /dev/null 2>&1
rm -f constant/polyMesh/boundary > /dev/null 2>&1
mv temp180 ./-180
#------------------------------------------------------------------------------

14
tutorials/combustion/XiEngineFoam/kivaTest/Allrun Executable file
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#!/bin/sh
cd ${0%/*} || exit 1 # Run from this directory
# Source tutorial run functions
. $WM_PROJECT_DIR/bin/tools/RunFunctions
# Get application name
application=`getApplication`
runApplication kivaToFoam -file otape17
runApplication $application
#------------------------------------------------------------------------------

93
tutorials/combustion/XiEngineFoam/kivaTest/constant/combustionProperties Normal file
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@ -0,0 +1,93 @@
/*--------------------------------*- 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 combustionProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
laminarFlameSpeedCorrelation Gulders;
fuel IsoOctane;
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;
}
Propane
{
W 0.446;
eta 0.12;
xi 4.95;
alpha 1.77;
beta -0.2;
f 2.3;
}
IsoOctane
{
W 0.4658;
eta -0.326;
xi 4.48;
alpha 1.56;
beta -0.22;
f 2.3;
}
}
ignite yes;
ignitionSites
(
{
location (0.03 0 0.091);
diameter 0.002;
start -15;
duration 20;
strength 4;
}
);
ignitionSphereFraction 1;
ignitionThickness ignitionThickness [0 1 0 0 0 0 0] 0;
ignitionCircleFraction 1;
ignitionKernelArea ignitionKernelArea [0 2 0 0 0 0 0] 0;
// ************************************************************************* //

31
tutorials/combustion/XiEngineFoam/kivaTest/constant/engineGeometry Normal file
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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 engineGeometry;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
engineMesh layered;
conRodLength conRodLength [0 1 0 0 0 0 0] 0.147;
bore bore [0 1 0 0 0 0 0] 0.092;
stroke stroke [0 1 0 0 0 0 0] 0.08423;
clearance clearance [0 1 0 0 0 0 0] 0.00115;
rpm rpm [0 0 -1 0 0 0 0] 1500;
// ************************************************************************* //

96
tutorials/combustion/XiEngineFoam/kivaTest/constant/thermophysicalProperties Normal file
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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 thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
thermoType
{
type heheuPsiThermo;
mixture inhomogeneousMixture;
transport sutherland;
thermo janaf;
equationOfState perfectGas;
specie specie;
energy absoluteEnthalpy;
//energy absoluteInternalEnergy;
}
stoichiometricAirFuelMassRatio stoichiometricAirFuelMassRatio [0 0 0 0 0 0 0] 15.0336;
fuel
{
specie
{
molWeight 114.23;
}
thermodynamics
{
Tlow 298.15;
Thigh 5000;
Tcommon 1000;
highCpCoeffs ( 19.3963 0.0488137 -1.55798e-05 2.17831e-09 -1.08391e-13 -37133.9 -78.8531 );
lowCpCoeffs ( 0.429357 0.0765769 8.41306e-06 -5.86603e-08 2.79414e-11 -30446.4 25.6735 );
}
transport
{
As 1.67212e-06;
Ts 170.672;
}
}
oxidant
{
specie
{
molWeight 28.8504;
}
thermodynamics
{
Tlow 200;
Thigh 6000;
Tcommon 1000;
highCpCoeffs ( 3.10205 0.00123963 -4.17512e-07 6.60292e-11 -3.87448e-15 -985.517 5.35187 );
lowCpCoeffs ( 3.58378 -0.0007269 1.66985e-06 -1.08452e-10 -4.31951e-13 -1050.53 3.11223 );
}
transport
{
As 1.67212e-06;
Ts 170.672;
}
}
burntProducts
{
specie
{
molWeight 28.6068;
}
thermodynamics
{
Tlow 200;
Thigh 6000;
Tcommon 1000;
highCpCoeffs ( 3.12468 0.00178578 -5.94695e-07 9.09801e-11 -5.1246e-15 -11005.8 5.03593 );
lowCpCoeffs ( 3.47612 0.000758205 -3.68739e-07 1.3449e-09 -8.08868e-13 -11071.5 3.3058 );
}
transport
{
As 1.67212e-06;
Ts 170.672;
}
}
// ************************************************************************* //

35
tutorials/combustion/XiEngineFoam/kivaTest/constant/turbulenceProperties Normal file
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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 turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
simulationType RAS;
RAS
{
RASModel kEpsilon;
turbulence on;
printCoeffs on;
kEpsilonCoeffs
{
C3 -0.33;
}
}
// ************************************************************************* //

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tutorials/combustion/XiEngineFoam/kivaTest/otape17 Normal file
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80
tutorials/combustion/XiEngineFoam/kivaTest/system/controlDict Normal file
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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 "system";
object controlDict.1st;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
application XiEngineFoam;
startFrom startTime;
startTime -180;
stopAt endTime;
endTime 60;
deltaT 0.25;
writeControl runTime;
writeInterval 5;
purgeWrite 0;
writeFormat ascii;
writePrecision 6;
writeCompression off;
timeFormat general;
timePrecision 6;
runTimeModifiable true;
adjustTimeStep no;
maxCo 0.2;
maxDeltaT 1;
functions
{
timeStep
{
type coded;
libs ("libutilityFunctionObjects.so");
name setDeltaT;
code
#{
#};
codeExecute
#{
const Time& runTime = mesh().time();
if (runTime.timeToUserTime(runTime.value()) >= -15.0)
{
const_cast<Time&>(runTime).setDeltaT
(
runTime.userTimeToTime(0.025)
);
}
#};
}
}
// ************************************************************************* //

75
tutorials/combustion/XiEngineFoam/kivaTest/system/fvSchemes Normal file
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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 "system";
object fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
ddtSchemes
{
default Euler;
}
gradSchemes
{
default Gauss linear;
}
divSchemes
{
default none;
div(phi,U) Gauss upwind;
div(phi,K) Gauss upwind;
div(phid,p) Gauss upwind;
div(meshPhi,p) Gauss upwind;
div(phiv,p) Gauss upwind;
div(phi,k) Gauss upwind;
div(phi,epsilon) Gauss upwind;
div(phi,R) Gauss upwind;
div(R) Gauss linear;
div(phiXi,Xi) Gauss upwind;
div(phiXi,Su) Gauss upwind;
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;
ea limitedLinear 1;
eau 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;
}
laplacianSchemes
{
default Gauss linear limited corrected 0.5;
}
interpolationSchemes
{
default linear;
}
snGradSchemes
{
default limited corrected 0.5;
}
// ************************************************************************* //

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tutorials/combustion/XiEngineFoam/kivaTest/system/fvSolution Normal file
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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 "system";
object fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
solvers
{
p
{
solver PCG;
preconditioner DIC;
tolerance 1e-06;
relTol 0.1;
}
pFinal
{
$p;
tolerance 1e-06;
relTol 0;
}
rho
{
solver PCG;
preconditioner DIC;
tolerance 1e-05;
relTol 0.1;
}
rhoFinal
{
$rho;
tolerance 1e-05;
relTol 0;
}
"(U|Xi|hau|eau|ft|b|ha|ea|k|epsilon)"
{
solver PBiCGStab;
preconditioner DILU;
tolerance 1e-05;
relTol 0.1;
}
"(U|ft|Xi|hau|eau|b|ha|ea|k|epsilon)Final"
{
$U;
tolerance 1e-05;
relTol 0;
}
}
PIMPLE
{
nCorrectors 2;
nNonOrthogonalCorrectors 1;
momentumPredictor yes;
}
// ************************************************************************* //