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Turbulent flow around a cylinder with pimpleFoam

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Old   May 18, 2020, 08:34
Post Turbulent flow around a cylinder with pimpleFoam
  #1
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nazim
Join Date: Nov 2018
Location: France
Posts: 4
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Hello everyone,

I have a problem of stability when trying to simulate the flow around a cylinder of about Re=20000.

I tried to introduce relaxation in U,k and omega but it only delays the crash of my simulation. I thought about introducing upwind schemes but I'm not sure to which extent exactly and if it's strictly necessary

Here are my files

controlDict

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1912                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    location    "system";
    object      controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

application     pimpleFoam;

startFrom       latestTime;

startTime       0;

stopAt          endTime;

endTime         300;

deltaT          4.5e-03;

//writeControl    adjustable;
writeControl    timeStep;

//writeInterval   0.1;
writeInterval   100;

purgeWrite      0;

writeFormat     ascii;

writePrecision  6;

writeCompression off;

timeFormat      general;

timePrecision   6;

runTimeModifiable yes;    // permet de changer le controlDict en temps reel

adjustTimeStep  yes;

maxCo           0.9;

//stopAt		writeNow;  // permet de stopper la simulation 


// ************************************************************************* //
fvSchemes

Code:
/*--------------------------------*- 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;
    location    "system";
    object      fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

ddtSchemes
{
    default         Euler;
}

gradSchemes
{
    default         Gauss linear;
    grad(p)         Gauss linear;
    grad(U)         Gauss linear;
}

divSchemes
{
    default          none;
    div(phi,U)       Gauss limitedLinearV 1;
    div(phi,k)       Gauss limitedLinear 1;
    div(phi,epsilon) Gauss limitedLinear 1;
    div(phi,omega)       Gauss limitedLinear 1;   // ajouté en debug
    div(phi,R)       Gauss limitedLinear 1;
    div(R)           Gauss linear;
    div(phi,nuTilda) Gauss limitedLinear 1;
    div((nuEff*dev2(T(grad(U))))) Gauss linear;
}

laplacianSchemes
{
    default         none;
    laplacian(nuEff,U) Gauss linear corrected;
    laplacian((1|A(U)),p) Gauss linear corrected; // for older versions
    laplacian(rAUf,p)  Gauss linear corrected;
    laplacian(DkEff,k) Gauss linear corrected;
    laplacian(DepsilonEff,epsilon) Gauss linear corrected;     
    laplacian(DomegaEff,omega)  Gauss linear corrected; // ajouté en debug
    laplacian(DREff,R) Gauss linear corrected;
    laplacian(DnuTildaEff,nuTilda) Gauss linear corrected;
}

interpolationSchemes
{
    default         linear;
    interpolate(U)  linear;
}

snGradSchemes
{
    default         corrected;
}

fluxRequired
{
    default         no;
    p               ;
}

wallDist
{
    method meshWave;
}

// ************************************************************************* //
fvSolution

Code:
/*--------------------------------*- 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;
    location    "system";
    object      fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

solvers
{
    p
    {
        solver          GAMG;
        tolerance       1e-06;
        relTol          0.01;
        smoother        GaussSeidel;
        cacheAgglomeration true;
        nCellsInCoarsestLevel 10;
        agglomerator    faceAreaPair;
        mergeLevels     1;
    }

    pFinal
    {
        solver          GAMG;
        tolerance       1e-06;
        relTol          0;
        smoother        GaussSeidel;
        cacheAgglomeration true;
        nCellsInCoarsestLevel 10;
        agglomerator    faceAreaPair;
        mergeLevels     1;
    }

    "(U|k|epsilon|omega)"				// j'ai ajoute omega dedans
    {
        solver          PBiCG;
        preconditioner  DILU;
        tolerance       1e-05;
        relTol          0.1;
    }

    "(U|k|epsilon|omega)Final"				// j'ai ajoute omega dedans
    {
        $U;
        tolerance       1e-05;
        relTol          0;
    }

omegaFinal
    {
        solver          GAMG;
        tolerance       1e-06;
        relTol          0;
        smoother        GaussSeidel;
        cacheAgglomeration true;
        nCellsInCoarsestLevel 10;
        agglomerator    faceAreaPair;
        mergeLevels     1;
    }

}

PIMPLE
{
    nOuterCorrectors 5;
    nCorrectors     2;
    nNonOrthogonalCorrectors 0;
    pRefCell        0;
    pRefValue       0;
}

relaxationFactors
{
    fields
    {
    }
    equations
    {
        "U.*"           0.8;    //intialement 0.9
        "k.*"           0.8;	// initalement 1
        "epsilon.*"     0.8;	// initialement 1
    }
}


// ************************************************************************* //
transportproperties

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1912                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    location    "constant";
    object      transportProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

transportModel  Newtonian;

nu              1e-02;

// ************************************************************************* //
turbulent model

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1912                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    location    "constant";
    object      turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

simulationType RAS;

RAS
{
    RASModel        kOmegaSST;				// c'etait Launder and sharma avant ca

    turbulence      on;

    printCoeffs     on;
}

// ************************************************************************* //
INITIAL CONDITIONS: (but as I am writing this I will change these one by the ones from the results of simpleFoam simulation, maybe it will increase the convergence and stability)

U

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1912                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       volVectorField;
    location    "0";
    object      U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [0 1 -1 0 0 0 0];


internalField   uniform (10 0 0);

boundaryField
{
    defaultFaces
    {
        type            noSlip;
    }
    upperWall
    {
        type            noSlip;
    }
    close
    {
        type            empty;
    }
    deep
    {
        type            empty;
    }
    inlet
    {
        type            fixedValue;
        value           uniform (10 0 0);
    }
    lowerWall
    {
        type            noSlip;
    }
    cylinder
    {
        type            noSlip;
    }
    outlet
    {
        type            zeroGradient;
    }
}


// ************************************************************************* //
P

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1912                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       volScalarField;
    location    "0";
    object      p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [0 2 -2 0 0 0 0];


internalField   uniform 0;

boundaryField
{
    defaultFaces
    {
        type            zeroGradient;
    }
    upperWall
    {
        type            zeroGradient;
    }
    close
    {
        type            empty;
    }
    deep
    {
        type            empty;
    }
    inlet
    {
        type            zeroGradient;
    }
    lowerWall
    {
        type            zeroGradient;
    }
    cylinder
    {
        type            zeroGradient;
    }
    outlet
    {
        type            fixedValue;
        value           uniform 0;
    }
}


// ************************************************************************* //
omega

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1912                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       volScalarField;
    location    "0";
    object      omega;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [0 0 -1 0 0 0 0];


internalField   uniform 15.97;

boundaryField
{
    defaultFaces
    {
        type            omegaWallFunction;
        value           nonuniform 0();
    }
    upperWall
    {
        type            omegaWallFunction;
        value           uniform 15.97;
    }
    close
    {
        type            empty;
    }
    deep
    {
        type            empty;
    }
    inlet
    {
        type            fixedValue;
        value           uniform 15.97;
    }
    lowerWall
    {
        type            omegaWallFunction;
        value           uniform 15.97;
    }
    cylinder
    {
        type            omegaWallFunction;
        value           uniform 15.97;
    }
    outlet
    {
        type            zeroGradient;
    }
}


// ************************************************************************* //
nut

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1912                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     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
{
    defaultFaces
    {
        type            nutkWallFunction;
        value           nonuniform 0();
    }
    upperWall
    {
        type            nutkWallFunction;
        value           uniform 0;
    }
    close
    {
        type            empty;
    }
    deep
    {
        type            empty;
    }
    inlet
    {
        type            calculated;
        value           uniform 0;
    }
    lowerWall
    {
        type            nutkWallFunction;
        value           uniform 0;
    }
    cylinder
    {
        type            nutkWallFunction;
        value           uniform 0;
    }
    outlet
    {
        type            calculated;
        value           uniform 0;
    }
}


// ************************************************************************* //
k

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1912                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       volScalarField;
    location    "0";
    object      k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [0 2 -2 0 0 0 0];


internalField   uniform 0.00015;

boundaryField
{
    defaultFaces
    {
        type            kqRWallFunction;
        value           nonuniform 0();
    }
    upperWall
    {
        type            kqRWallFunction;
        value           uniform 0.00015;
    }
    close
    {
        type            empty;
    }
    deep
    {
        type            empty;
    }
    inlet
    {
        type            fixedValue;
        value           uniform 0.00015;
    }
    lowerWall
    {
        type            kqRWallFunction;
        value           uniform 0.00015;
    }
    cylinder
    {
        type            kqRWallFunction;
        value           uniform 0.00015;
    }
    outlet
    {
        type            zeroGradient;
    }
}


// ************************************************************************* //
epsilon

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1912                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       volScalarField;
    location    "0";
    object      epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [0 2 -3 0 0 0 0];


internalField   uniform 0.001;

boundaryField
{
    defaultFaces
    {
        type            epsilonWallFunction;
        value           nonuniform 0();
    }
    upperWall
    {
        type            epsilonWallFunction;
        value           uniform 0.001;
    }
    close
    {
        type            empty;
    }
    deep
    {
        type            empty;
    }
    inlet
    {
        type            fixedValue;
        value           uniform 0.001;
    }
    lowerWall
    {
        type            epsilonWallFunction;
        value           uniform 0.001;
    }
    cylinder
    {
        type            epsilonWallFunction;
        value           uniform 0.001;
    }
    outlet
    {
        type            zeroGradient;
    }
}


// ************************************************************************* //
I had several problems of many kind (mesh file conversion and so on) before that the program accepts to run and that's why I'm asking because I don't have much time to try many solutions which won't work.

I have to tell you however that checkMesh tells me of an aspect ratio about 2000 which I don't have at all on my mesh. every other mesh parameters are ok. I have read that checkMesh sometimes give wrong conclusions.

Thanks in advance for you help
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Old   May 18, 2020, 17:56
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  #2
HPE
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Hi,

- Could you please share the output of `checkMesh -allGeometry -allTopology`?
- Could you please attach a log file or some sort of info to provide insight for the numerical instabilities you concern?

Thanks
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Old   May 19, 2020, 07:58
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nazim
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thanks for the quick reply, in fact I have solved the problem now (but I will keep this the post) by setting the relaxation to a higher value in U and introducing it for k and omega as well as setting a CrankNicolson scheme for the time discretization and I set the nonorthogonal correctors to 3, because my cells are not orthogonal everywhere. I think that's all I have changed.

But there is another thing I have done, that is to run a simulation with simpleFoam first and then to inject the steady solution (I didn't verify if it was very well converged though) to my 0 folder as initial conditions, I has probably lowered the sharpness of the gradient comparing to my previous case (all velocities set as zero if I remember well).

I will however try to run again the failed simulation to see what was inside the log file but as I remember I simply have seen all the quantities exploding.

You will find attached the images of the "failed" simulation (the new one I have done is working correctly) as well as the mesh in the critical zone, it may already give you an insight of why it diverged.

The "checkMesh -allGeometry -allTopology" gives the following results.

command line : checkMesh -allGeometry -allTopology

Code:
/*---------------------------------------------------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v1912                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
Build  : _f3950763fe-20191219 OPENFOAM=1912
Arch   : "LSB;label=32;scalar=64"
Exec   : checkMesh -allGeometry -allTopology
Date   : May 19 2020
Time   : 23:36:02
Host   : Jmx-MSI
PID    : 4610
I/O    : uncollated
Case   : /mnt/d/Openfoam_mysim/Steady
nProcs : 1
trapFpe: Floating point exception trapping enabled (FOAM_SIGFPE).
fileModificationChecking : Monitoring run-time modified files using timeStampMaster (fileModificationSkew 10)
allowSystemOperations : Allowing user-supplied system call operations

// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
Create time

Create mesh for time = 0

Enabling all (cell, face, edge, point) topology checks.

Enabling all geometry checks.

Time = 0

Mesh stats
    points:           301648
    internal points:  0
    edges:            752316
    internal edges:   149020
    internal edges using one boundary point:   0
    internal edges using two boundary points:  149020
    faces:            600590
    internal faces:   298942
    cells:            149922
    faces per cell:   6
    boundary patches: 8
    point zones:      0
    face zones:       0
    cell zones:       0

Overall number of cells of each type:
    hexahedra:     149922
    prisms:        0
    wedges:        0
    pyramids:      0
    tet wedges:    0
    tetrahedra:    0
    polyhedra:     0

Checking topology...
    Boundary definition OK.
    Cell to face addressing OK.
    Point usage OK.
    Upper triangular ordering OK.
    Face vertices OK.
    Topological cell zip-up check OK.
    Face-face connectivity OK.
  <<Writing 4 cells with two non-boundary faces to set twoInternalFacesCells
    Number of regions: 1 (OK).

Checking patch topology for multiply connected surfaces...
    Patch               Faces    Points   Surface topology                   Bounding box
    defaultFaces        0        0        ok (empty)                        
    close               149922   150824   ok (non-closed singly connected)   (-143 0 -10) (300 45 -10)
    deep                149922   150824   ok (non-closed singly connected)   (-143 0 -30) (300 45 -30)
    outlet              217      436      ok (non-closed singly connected)   (300 0 -30) (300 45 -10)
    lowerWall           552      1106     ok (non-closed singly connected)   (-143 0 -30) (300 0 -10)
    cylinder            326      652      ok (non-closed singly connected)   (-9.99901 12.5001 -30) (9.99968 32.4999 -10)
    upperWall           552      1106     ok (non-closed singly connected)   (-143 45 -30) (300 45 -10)
    inlet               157      316      ok (non-closed singly connected)   (-143 0 -30) (-143 45 -10)

Checking faceZone topology for multiply connected surfaces...
    No faceZones found.

Checking basic cellZone addressing...
    No cellZones found.

Checking geometry...
    Overall domain bounding box (-143 0 -30) (300 45 -10)
    Mesh has 2 geometric (non-empty/wedge) directions (1 1 0)
    Mesh has 2 solution (non-empty) directions (1 1 0)
    All edges aligned with or perpendicular to non-empty directions.
    Boundary openness (9.70778e-18 1.23123e-17 3.32786e-16) OK.
    Max cell openness = 4.22476e-15 OK.
    Max aspect ratio = 235.434 OK.
    Minimum face area = 0.000347332. Maximum face area = 52.0974.  Face area magnitudes OK.
    Min volume = 0.00694665. Max volume = 26.1673.  Total volume = 392417.  Cell volumes OK.
    Mesh non-orthogonality Max: 44.0317 average: 11.3073
    Non-orthogonality check OK.
    Face pyramids OK.
    Max skewness = 0.604515 OK.
    Coupled point location match (average 0) OK.
    Face tets OK.
    Min/max edge length = 0.00263115 20 OK.
    All angles in faces OK.
    Face flatness (1 = flat, 0 = butterfly) : min = 1  average = 1
    All face flatness OK.
    Cell determinant (wellposedness) : minimum: 7.22331e-05 average: 0.194798
 ***Cells with small determinant (< 0.001) found, number of cells: 1103
  <<Writing 1103 under-determined cells to set underdeterminedCells
    Concave cell check OK.
    Face interpolation weight : minimum: 0.33587 average: 0.492874
    Face interpolation weight check OK.
    Face volume ratio : minimum: 0.501818 average: 0.972636
    Face volume ratio check OK.

Failed 1 mesh checks.

End

Here are the new fvSchemes and fvSolutions that allowed me to get correct results

fvSchemes
Code:
/*--------------------------------*- 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;
    location    "system";
    object      fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

ddtSchemes
{
    default         CrankNicolson  0.5;	 // initially Euler;
    ddt(phi)	    CrankNicolson  0.5;
}

gradSchemes
{
    default         Gauss linear;
    grad(p)         Gauss linear;
    grad(U)         Gauss linear;
}

divSchemes
{
    default          none;
    div(phi,U)       Gauss limitedLinearV 1;
    div(phi,k)       Gauss limitedLinear 1;
    div(phi,epsilon) Gauss limitedLinear 1;
    div(phi,omega)       Gauss limitedLinear 1;   // ajouté en debug
    div(phi,R)       Gauss limitedLinear 1;
    div(R)           Gauss linear;
    div(phi,nuTilda) Gauss limitedLinear 1;
    div((nuEff*dev2(T(grad(U))))) Gauss linear;
}

laplacianSchemes
{
    default         none;
    laplacian(nuEff,U) Gauss linear corrected;
    laplacian((1|A(U)),p) Gauss linear corrected; // for older versions
    laplacian(rAUf,p)  Gauss linear corrected;
    laplacian(DkEff,k) Gauss linear corrected;
    laplacian(DepsilonEff,epsilon) Gauss linear corrected;     
    laplacian(DomegaEff,omega)  Gauss linear corrected; // ajouté en debug
    laplacian(DREff,R) Gauss linear corrected;
    laplacian(DnuTildaEff,nuTilda) Gauss linear corrected;
}

interpolationSchemes
{
    default         linear;
    interpolate(U)  linear;
}

snGradSchemes
{
    default         corrected;
}

fluxRequired
{
    default         no;
    p               ;
}

wallDist
{
    method meshWave;
}

// ************************************************************************* //
fvSolution
Code:
/*--------------------------------*- 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;
    location    "system";
    object      fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

solvers
{
    p
    {
        solver          GAMG;
        tolerance       1e-06;
        relTol          0.01;
        smoother        GaussSeidel;
        cacheAgglomeration true;
        nCellsInCoarsestLevel 10;
        agglomerator    faceAreaPair;
        mergeLevels     1;
    }

    pFinal
    {
        solver          GAMG;
        tolerance       1e-06;
        relTol          0;
        smoother        GaussSeidel;
        cacheAgglomeration true;
        nCellsInCoarsestLevel 10;
        agglomerator    faceAreaPair;
        mergeLevels     1;
    }

    "(U|k|epsilon|omega)"				// j'ai ajouté omega dedans
    {
        solver          PBiCG;
        preconditioner  DILU;
        tolerance       1e-05;
        relTol          0.1;
    }

    "(U|k|epsilon|omega)Final"				// j'ai ajoute omega dedans
    {
        $U;
        tolerance       1e-05;
        relTol          0;
    }

omegaFinal
    {
        solver          GAMG;
        tolerance       1e-06;
        relTol          0;
        smoother        GaussSeidel;
        cacheAgglomeration true;
        nCellsInCoarsestLevel 10;
        agglomerator    faceAreaPair;
        mergeLevels     1;
    }

}

PIMPLE
{
    nOuterCorrectors 5;
    nCorrectors     2;
    nNonOrthogonalCorrectors 3;
    pRefCell        0;
    pRefValue       0;
}

relaxationFactors
{
    fields
    {
    }
    equations
    {
        "U.*"           0.7;    //intialement 0.9
        "k.*"           0.7;	// initalement 1
        "epsilon.*"     0.7;	// initialement 1
    }
}


// ************************************************************************* //
Attached Images
File Type: jpg vortex0.JPG (38.7 KB, 30 views)
File Type: jpg vortex1.JPG (45.9 KB, 21 views)
File Type: jpg vortex2.JPG (47.7 KB, 27 views)
File Type: jpg mesh_cylinder.jpg (112.0 KB, 17 views)
File Type: jpg mesh_cylinder_bis.jpg (136.0 KB, 24 views)
Last edited by Nazim; May 19, 2020 at 19:43.
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