CFD Online Logo CFD Online URL
www.cfd-online.com
[Sponsors]
Home > Forums > Software User Forums > OpenFOAM > OpenFOAM Running, Solving & CFD

OpenFOAM (interFoam) crashing while solving k-epsilon model.

Register Blogs Community New Posts Updated Threads Search

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   October 1, 2021, 11:00
Default OpenFOAM (interFoam) crashing while solving k-epsilon model.
  #1
New Member
 
Join Date: Jul 2021
Posts: 16
Rep Power: 5
Legacy is on a distinguished road
Hello! I am new to OpenFOAM so this question might seem dumb. I want to simulate turbulent flow in an open channel. interFoam solves the case without any problems in laminar case but in turbulent condition it diverges. (high Courant Numbers). I get FPE error as something goes to infinity or division by zero.

I think it has something to do with boundary conditions in k, and epsilon but I could not figure it out.

fvSchemes:

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v2106                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    object      fvSchemes;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

ddtSchemes
{
    default         Euler;
}

gradSchemes
{
    default         Gauss linear;
}

divSchemes
{
    div(rhoPhi,U)   Gauss linearUpwind grad(U);
    div(phi,alpha)  Gauss vanLeer;
    div(phirb,alpha) Gauss linear;
    div(((rho*nuEff)*dev2(T(grad(U))))) Gauss linear;
    div(phi,epsilon) Gauss linear;
    div(phi,k) Gauss linear;
}

laplacianSchemes
{
    default         Gauss linear uncorrected;
}

interpolationSchemes
{
    default         linear;
}

snGradSchemes
{
    default         corrected;
}


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

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v2106                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    object      fvSolution;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

solvers
{
    "alpha.water.*"
    {
        nAlphaCorr      2;
        nAlphaSubCycles 1;
        cAlpha          1;

        MULESCorr       yes;
        nLimiterIter    5;

        solver          smoothSolver;
        smoother        symGaussSeidel;
        tolerance       1e-8;
        relTol          0;
    }

    "pcorr.*"
    {
        solver          PCG;
        preconditioner  DIC;
        tolerance       1e-5;
        relTol          0;
    }

    p_rgh
    {
        solver          PCG;
        preconditioner  DIC;
        tolerance       1e-07;
        relTol          0.05;
    }

    p_rghFinal
    {
        $p_rgh;
        relTol          0;
    }

    U
    {
        solver          smoothSolver; //
        smoother        symGaussSeidel;
        relTol          0;
    }

        "(k|epsilon|omega|UFinal|kFinal|epsilonFinal|omegaFinal)"    
    {
        solver           PBiCG;
        preconditioner   DILU;
        tolerance        1e-12;
        relTol           1.0e-2;
        maxIter          100;
    };
}

PIMPLE
{
    momentumPredictor   no;
    nOuterCorrectors    1;
    nCorrectors         3;
    nNonOrthogonalCorrectors 1;
}

relaxationFactors
{

    fields
    {
        "(p)"           0.3;
    }
    equations
    {
        "(U)"           0.7;
        "(k)"           0.3;
        "(epsilon)"     0.8;
        ".*"             1;
    }
}


// ************************************************************************* //
BlockMeshDict

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v2106                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    object      blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

scale   0.1;

x1 4; // mainChannelLength
y1 2; // mainChannelWidth
z1 1; // mainChannelHeight

y2 3; // secondaryChannelLength
x2 1; // secondaryChannelWidth
z2 0.5; // secondaryChannelHeight


// Calculating edge coordinates

xx0 #eval{ 0.5*$x1+0.5*$x2 };
yy0 #eval{ $y1+$y2 };
xx1 #eval{ 0.5*$x1-0.5*$x2 };
zz0 #eval{ $z1-$z2 };

//MeshSiz 0.1; // Mesh Size in 2nd channel (spanwise)
//NcellS1 #eval{ std::floor( $x1/$MeshSiz )}; // Channel 1 number of cells (streamwise)
//NcellS2 #eval{ std::floor ($x2/$MeshSiz) }; // Channel 2 number of cells (spanwise)



vertices
(

//Block1
(0 0 0) // 0
($x1 0 0) // 1
($x1 $y1 0) // 2
(0 $y1 0) // 3
(0 0 $z1) // 4
($x1 0 $z1) // 5
($x1 $y1 $z1) // 6
(0 $y1 $z1) // 7


//Block2
($xx0 $y1 $zz0) //8
($xx0 $yy0 $zz0) //9
($xx1 $yy0 $zz0) //10
($xx1 $y1 $zz0) //11
($xx0 $y1 $z1) //12
($xx0 $yy0 $z1) //13
($xx1 $yy0 $z1) //14
($xx1 $y1 $z1) //15
);

blocks
(
hex (0 1 2 3 4 5 6 7) (320 160 80) simpleGrading (1 1 1) //Channel 1
hex (8 9 10 11 12 13 14 15) (400 80 40) simpleGrading (1 1 1) //Channel 2

);


edges
(
);

boundary
(
    outlet
    {
        type patch;
        faces
        (
            (6 2 1 5)
        );
    }
    inlet
    {
        type patch;
        faces
        (
            (0 4 7 3)
        );
    }
    bottomwall
    {
        type wall;
        faces
        (
            (0 1 2 3)
        );
    }

    leftwall2
    {
        type wall;
        faces
        (
            (8 12 15 11)
        );
    }

    atmosphere
    {
        type patch;
        faces
        (
            (4 5 6 7)

        );
    }
    rightwall
    {
        type wall;
        faces
        (
            (0 1 5 4)

        );
    }
    leftwall
    {
        type wall;
        faces
        (
            (2 6 7 3)

        );
    }

    // Box2

    c2bottom
    {
        type wall;
        faces
        (
            (8 9 10 11)

        );
    }  

     c2atmosphere
    {
        type patch;
        faces
        (
            (12 13 14 15)

        );
    }  

    c2outlet
    {
        type patch;
        faces
        (
            (9 13 14 10)

        );
    }

    c2rightwall
    {
        type wall;
        faces
        (
            (8 9 13 12)

        );
    }

    c2leftwall
    {
        type wall;
        faces
        (
            (11 10 14 15)

        );
    }

);
mergePatchPairs
(

(leftwall leftwall2)
 
);


// ************************************************************************* //
ControlDict

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v2106                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       dictionary;
    object      controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

application     interFoam;

startFrom       startTime;

startTime       0;

stopAt          endTime;

endTime         5;

deltaT          0.001;

writeControl    adjustable;

writeInterval   0.05;

purgeWrite      0;

writeFormat     ascii;

writePrecision  6;

writeCompression off;

timeFormat      general;

timePrecision   6;

runTimeModifiable yes;

adjustTimeStep  yes;

maxCo           1;

maxAlphaCo      1;

maxDeltaT       1;

#sinclude   "sampling"


// ************************************************************************* //
0/k

Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v2106                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       volScalarField;
    object      k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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

internalField   uniform 0.1;

boundaryField
{
    leftwall
    {
        type            kqRWallFunction;
        value           uniform 0.1;
    }

    rightwall
    {
        type            kqRWallFunction;
        value           uniform 0.1;
    }

    bottomwall
    {
        type            kqRWallFunction;
        value           uniform 0.1;
    }

    atmosphere
    {
        type            inletOutlet;
        inletValue      uniform 0.1;
        value           uniform 0.1;
    }

    outlet
    {
        type            inletOutlet;
        inletValue      uniform 0.1;
        value           uniform 0.1;
    }

    inlet
    {
        type            turbulentIntensityKineticEnergyInlet;
        intensity       0.01;
        value           uniform 0.06;
    }

    c2bottom
    {
        type            kqRWallFunction;
        value           uniform 0.1;
    }
    c2atmosphere
    {
        type            inletOutlet;
        inletValue      uniform 0.1;
        value           uniform 0.1;
    }
    c2outlet
    {
        type            inletOutlet;
        inletValue      uniform 0.1;
        value           uniform 0.1;
    }
    c2rightwall
    {
        type            kqRWallFunction;
        value           uniform 0.1;
    }
    c2leftwall
    {
        type            kqRWallFunction;
        value           uniform 0.1;
    }

    defaultFaces
    {
        type            empty;
    }
}


// ************************************************************************* //
0/epsilon
Code:
/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  v2106                                 |
|   \\  /    A nd           | Website:  www.openfoam.com                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       volScalarField;
    object      epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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

internalField   uniform 0.1;

boundaryField
{
    leftwall
    {
        type            epsilonWallFunction;
        value           uniform 0.1;
    }

    rightwall
    {
        type            epsilonWallFunction;
        value           uniform 0.1;
    }

    bottomwall
    {
        type            epsilonWallFunction;
        value           uniform 0.1;
    }

    atmosphere
    {
        type            inletOutlet;
        inletValue      uniform 0.1;
        value           uniform 0.1;
    }

    outlet
    {
        type            inletOutlet;
        inletValue      uniform 0.1;
        value           uniform 0.1;
    }

    inlet
    {
        type            turbulentMixingLengthDissipationRateInlet;
        mixingLength    0.005;
        value           uniform 0.000055;
    }

    c2bottom
    {
        type            epsilonWallFunction;
        value           uniform 0.1;
    }
    c2atmosphere
    {
        type            inletOutlet;
        inletValue      uniform 0.1;
        value           uniform 0.1;
    }
    c2outlet
    {
        type            inletOutlet;
        inletValue      uniform 0.1;
        value           uniform 0.1;
    }
    c2rightwall
    {
        type            epsilonWallFunction;
        value           uniform 0.1;
    }
    c2leftwall
    {
        type            epsilonWallFunction;
        value           uniform 0.1;
    }
    defaultFaces
    {
        type            empty;
    }

}
// ************************************************************************* //
Legacy is offline   Reply With Quote

Old   October 1, 2021, 11:10
Default
  #2
New Member
 
Join Date: Jul 2021
Posts: 16
Rep Power: 5
Legacy is on a distinguished road
When I use adjustable time step, the time step goes to zero: Output here

Code:
PIMPLE: iteration 1
smoothSolver:  Solving for alpha.water, Initial residual = 0.576479, Final residual = 1.69443e-09, No Iterations 3
Phase-1 volume fraction = 0.999932  Min(alpha.water) = 0  Max(alpha.water) = 1.1816
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.999932  Min(alpha.water) = 0  Max(alpha.water) = 1.1686
DICPCG:  Solving for p_rgh, Initial residual = 0.99993, Final residual = 0.0219691, No Iterations 2
DICPCG:  Solving for p_rgh, Initial residual = 2.78473e-38, Final residual = 2.78473e-38, No Iterations 0
time step continuity errors : sum local = 2.34799e+44, global = -8.45321e+43, cumulative = -8.46412e+43
#0  Foam::error::printStack(Foam::Ostream&) at ??:?
#1  Foam::sigFpe::sigHandler(int) at ??:?
#2  ? in /lib64/libc.so.6
#3  Foam::scalarProduct<double, double>::type Foam::sumProd<double>(Foam::UList<double> const&, Foam::UList<double> const&) at ??:?
#4  Foam::PCG::scalarSolve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
#5  Foam::PCG::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
#6  Foam::fvMatrix<double>::solveSegregated(Foam::dictionary const&) at ??:?
#7  Foam::fvMesh::solve(Foam::fvMatrix<double>&, Foam::dictionary const&) const at ??:?
#8  ? at ??:?
#9  __libc_start_main in /lib64/libc.so.6
#10  ? at ??:?
Adjustable time step off:

Code:
Starting time loop

--> FOAM Warning :
    From function void Foam::particle::locate(const Foam::Vector<double> &, const Foam::Vector<double> *, int, bool, const Foam::string &)
    in file particle/particle.C at line 484
    Particle initialised with a location outside of the mesh when tracking from centre (0.0225 0.1975 0.0075) of cell 6324 to position (0.02 0.2 0.005)
Reading set description:
    gauge_1
    gauge_2

Courant Number mean: 0 max: 0
Interface Courant Number mean: 0 max: 0
Time = 0.001

PIMPLE: iteration 1
smoothSolver:  Solving for alpha.water, Initial residual = 0, Final residual = 0, No Iterations 0
Phase-1 volume fraction = 1  Min(alpha.water) = 1  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 1  Min(alpha.water) = 1  Max(alpha.water) = 1
DICPCG:  Solving for p_rgh, Initial residual = 1, Final residual = 0.0480845, No Iterations 38
DICPCG:  Solving for p_rgh, Initial residual = 0.001251, Final residual = 5.07562e-05, No Iterations 24
time step continuity errors : sum local = 8.21433e-05, global = -1.06508e-05, cumulative = -1.06508e-05
DICPCG:  Solving for p_rgh, Initial residual = 0.0181754, Final residual = 0.000821557, No Iterations 38
DICPCG:  Solving for p_rgh, Initial residual = 0.0023616, Final residual = 9.93711e-05, No Iterations 24
time step continuity errors : sum local = 5.54347e-05, global = 7.24914e-06, cumulative = -3.4017e-06
DICPCG:  Solving for p_rgh, Initial residual = 0.00272227, Final residual = 0.00012654, No Iterations 17
DICPCG:  Solving for p_rgh, Initial residual = 0.000127637, Final residual = 8.15941e-08, No Iterations 44
time step continuity errors : sum local = 4.43924e-08, global = -1.19515e-09, cumulative = -3.4029e-06
DILUPBiCG:  Solving for epsilon, Initial residual = 0.432547, Final residual = 0.00151274, No Iterations 2
DILUPBiCG:  Solving for k, Initial residual = 1, Final residual = 0.00501427, No Iterations 2
ExecutionTime = 2 s  ClockTime = 2 s

Courant Number mean: 0.933855 max: 10.6067
Interface Courant Number mean: 0 max: 0
Time = 0.002

PIMPLE: iteration 1
smoothSolver:  Solving for alpha.water, Initial residual = 1, Final residual = 6.31571e-09, No Iterations 3
Phase-1 volume fraction = 1  Min(alpha.water) = 0.999999  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 1  Min(alpha.water) = 0.999999  Max(alpha.water) = 1
DICPCG:  Solving for p_rgh, Initial residual = 0.0257119, Final residual = 0.00127956, No Iterations 41
DICPCG:  Solving for p_rgh, Initial residual = 0.00222235, Final residual = 9.88605e-05, No Iterations 29
time step continuity errors : sum local = 2.89055e-05, global = 4.45382e-06, cumulative = 1.05093e-06
DICPCG:  Solving for p_rgh, Initial residual = 0.0199581, Final residual = 0.00090856, No Iterations 38
DICPCG:  Solving for p_rgh, Initial residual = 0.00437537, Final residual = 0.000210576, No Iterations 28
time step continuity errors : sum local = 1.2806e-05, global = -1.03409e-06, cumulative = 1.68356e-08
DICPCG:  Solving for p_rgh, Initial residual = 0.0306757, Final residual = 0.00131807, No Iterations 16
DICPCG:  Solving for p_rgh, Initial residual = 0.00133985, Final residual = 9.60899e-08, No Iterations 71
time step continuity errors : sum local = 5.49774e-09, global = 2.29314e-10, cumulative = 1.70649e-08
DILUPBiCG:  Solving for epsilon, Initial residual = 0.709524, Final residual = 0.00573007, No Iterations 6
bounding epsilon, min: -0.207824 max: 500.884 average: 9.90857
DILUPBiCG:  Solving for k, Initial residual = 0.796152, Final residual = 0.00556545, No Iterations 6
bounding k, min: -58.4318 max: 204.832 average: 4.33867
ExecutionTime = 2.78 s  ClockTime = 3 s

Courant Number mean: 0.927321 max: 8.9843
Interface Courant Number mean: 0 max: 0
Time = 0.003

PIMPLE: iteration 1
smoothSolver:  Solving for alpha.water, Initial residual = 0.99898, Final residual = 4.47903e-11, No Iterations 6
Phase-1 volume fraction = 0.999898  Min(alpha.water) = 0  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.999887  Min(alpha.water) = -0.0125567  Max(alpha.water) = 1.00597
DICPCG:  Solving for p_rgh, Initial residual = 0.106187, Final residual = 0.00498852, No Iterations 9
DICPCG:  Solving for p_rgh, Initial residual = 0.00227057, Final residual = 9.66437e-05, No Iterations 40
time step continuity errors : sum local = 1.0627e-05, global = 1.00609e-06, cumulative = 1.02316e-06
DICPCG:  Solving for p_rgh, Initial residual = 0.0188761, Final residual = 0.000923598, No Iterations 34
DICPCG:  Solving for p_rgh, Initial residual = 0.000584912, Final residual = 2.85582e-05, No Iterations 27
time step continuity errors : sum local = 5.54231e-06, global = 4.1449e-07, cumulative = 1.43765e-06
DICPCG:  Solving for p_rgh, Initial residual = 0.00464214, Final residual = 0.000228561, No Iterations 8
DICPCG:  Solving for p_rgh, Initial residual = 0.000243947, Final residual = 9.92472e-08, No Iterations 64
time step continuity errors : sum local = 1.81879e-08, global = 3.21452e-10, cumulative = 1.43797e-06
DILUPBiCG:  Solving for epsilon, Initial residual = 0.0321632, Final residual = 0.000107652, No Iterations 1
bounding epsilon, min: -5.00812 max: 311199 average: 135.697
DILUPBiCG:  Solving for k, Initial residual = 0.997182, Final residual = 0.00755244, No Iterations 9
bounding k, min: -3.71915 max: 4283.07 average: 155.914
ExecutionTime = 3.49 s  ClockTime = 3 s

Courant Number mean: 0.923043 max: 9.75704
Interface Courant Number mean: 0.00260689 max: 9.35186
Time = 0.004

PIMPLE: iteration 1
smoothSolver:  Solving for alpha.water, Initial residual = 0.491544, Final residual = 6.08724e-10, No Iterations 4
Phase-1 volume fraction = 0.999951  Min(alpha.water) = 0.582409  Max(alpha.water) = 1.00286
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.999956  Min(alpha.water) = 0.582409  Max(alpha.water) = 1.03078
DICPCG:  Solving for p_rgh, Initial residual = 0.872382, Final residual = 0.0131008, No Iterations 2
DICPCG:  Solving for p_rgh, Initial residual = 0.00083191, Final residual = 3.21955e-05, No Iterations 7
time step continuity errors : sum local = 0.000684782, global = 0.000135832, cumulative = 0.00013727
DICPCG:  Solving for p_rgh, Initial residual = 2.76153e-05, Final residual = 1.21254e-06, No Iterations 43
DICPCG:  Solving for p_rgh, Initial residual = 9.4024e-07, Final residual = 9.41337e-08, No Iterations 24
time step continuity errors : sum local = 1.07063e-05, global = 1.06688e-06, cumulative = 0.000138337
DICPCG:  Solving for p_rgh, Initial residual = 1.0033e-05, Final residual = 4.62191e-07, No Iterations 43
DICPCG:  Solving for p_rgh, Initial residual = 4.45772e-07, Final residual = 9.3462e-08, No Iterations 18
time step continuity errors : sum local = 1.10211e-05, global = -1.91586e-06, cumulative = 0.000136421
DILUPBiCG:  Solving for epsilon, Initial residual = 0.129346, Final residual = 0.00122242, No Iterations 32
bounding epsilon, min: -731.285 max: 2.60303e+07 average: 947816
DILUPBiCG:  Solving for k, Initial residual = 0.785097, Final residual = 0.00508704, No Iterations 26
bounding k, min: -1975.57 max: 20642.1 average: 3522.04
ExecutionTime = 4.21 s  ClockTime = 4 s

Courant Number mean: 0.912524 max: 13.9602
Interface Courant Number mean: 0.00281132 max: 13.9602
Time = 0.005

PIMPLE: iteration 1
smoothSolver:  Solving for alpha.water, Initial residual = 0.538678, Final residual = 2.54492e-09, No Iterations 6
Phase-1 volume fraction = 0.999988  Min(alpha.water) = 0.81784  Max(alpha.water) = 1.0082
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.999989  Min(alpha.water) = 0.797185  Max(alpha.water) = 1.04048
DICPCG:  Solving for p_rgh, Initial residual = 0.999924, Final residual = 0.0407437, No Iterations 4
DICPCG:  Solving for p_rgh, Initial residual = 0.000732188, Final residual = 2.99942e-05, No Iterations 31
time step continuity errors : sum local = 3171.82, global = 98.9218, cumulative = 98.9219
DICPCG:  Solving for p_rgh, Initial residual = 0.999999, Final residual = 0.0496443, No Iterations 20
DICPCG:  Solving for p_rgh, Initial residual = 0.0137463, Final residual = 0.000649829, No Iterations 26
time step continuity errors : sum local = 1.77798e+11, global = -2.06326e+09, cumulative = -2.06326e+09
DICPCG:  Solving for p_rgh, Initial residual = 1, Final residual = 0.0484649, No Iterations 20
DICPCG:  Solving for p_rgh, Initial residual = 0.013821, Final residual = 9.27114e-08, No Iterations 80
time step continuity errors : sum local = 3.35538e+22, global = -1.09243e+21, cumulative = -1.09243e+21
DILUPBiCG:  Solving for epsilon, Initial residual = 1, Final residual = 0.00460737, No Iterations 2
bounding epsilon, min: -3.82187e+43 max: 1.414e+44 average: 9.1937e+39
DILUPBiCG:  Solving for k, Initial residual = 1, Final residual = 0.000613373, No Iterations 3
bounding k, min: -1.30274e+34 max: 3.10203e+34 average: 8.83677e+29
ExecutionTime = 4.84 s  ClockTime = 5 s

Courant Number mean: 2.83494e+29 max: 3.80432e+32
Interface Courant Number mean: 6.81277e+22 max: 1.43842e+27
Time = 0.006

PIMPLE: iteration 1
smoothSolver:  Solving for alpha.water, Initial residual = 0.999997, Final residual = 2.32384e-09, No Iterations 22
Phase-1 volume fraction = 238364  Min(alpha.water) = 0  Max(alpha.water) = 1.81157e+10
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 4.1998e+46  Min(alpha.water) = -8.49254e+66  Max(alpha.water) = 1.07193e+67
DICPCG:  Solving for p_rgh, Initial residual = 1, Final residual = 0.0340628, No Iterations 4
DICPCG:  Solving for p_rgh, Initial residual = 3.21847e-84, Final residual = 3.21847e-84, No Iterations 0
time step continuity errors : sum local = 2.69341e+27, global = 1.21014e+27, cumulative = 1.21014e+27
DICPCG:  Solving for p_rgh, Initial residual = 9.47547e-83, Final residual = 9.47547e-83, No Iterations 0
DICPCG:  Solving for p_rgh, Initial residual = 9.47547e-83, Final residual = 9.47547e-83, No Iterations 0
time step continuity errors : sum local = 7.92964e+28, global = -3.68394e+27, cumulative = -2.47381e+27
DICPCG:  Solving for p_rgh, Initial residual = 1.01454e-82, Final residual = 1.01454e-82, No Iterations 0
DICPCG:  Solving for p_rgh, Initial residual = 1.01454e-82, Final residual = 1.01454e-82, No Iterations 0
time step continuity errors : sum local = 8.49029e+28, global = -6.65261e+27, cumulative = -9.12642e+27
DILUPBiCG:  Solving for epsilon, Initial residual = 0.0817333, Final residual = 0.000213674, No Iterations 26
bounding epsilon, min: -2.62723e+66 max: 9.34649e+66 average: 1.28677e+65
DILUPBiCG:  Solving for k, Initial residual = 1, Final residual = 801874, No Iterations 100
bounding k, min: -2.08023e+79 max: 2.32014e+80 average: 3.38051e+77
ExecutionTime = 5.6 s  ClockTime = 6 s

Courant Number mean: 3.94164e+29 max: 2.82322e+32
Interface Courant Number mean: 2.39755e+27 max: 7.8528e+30
Time = 0.007

PIMPLE: iteration 1
smoothSolver:  Solving for alpha.water, Initial residual = 1, Final residual = 8.55191e-09, No Iterations 30
Phase-1 volume fraction = -6.03994e+74  Min(alpha.water) = -4.49584e+79  Max(alpha.water) = 6.07195e+72
#0  Foam::error::printStack(Foam::Ostream&) at ??:?
#1  Foam::sigFpe::sigHandler(int) at ??:?
#2  ? in /lib64/libc.so.6
#3  ? at ??:?
#4  ? at ??:?
#5  ? at ??:?
#6  __libc_start_main in /lib64/libc.so.6
#7  ? at ??:?
Floating point exception
Legacy is offline   Reply With Quote

Reply

Tags
interfoam, kepsilonmodel, openfoam, turbulence


Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

BB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Trackbacks are Off
Pingbacks are On
Refbacks are On


Similar Threads
Thread Thread Starter Forum Replies Last Post
chtMultiRegionSimpleFoam: maximum number of iterations excedeed. Nkl OpenFOAM Running, Solving & CFD 19 October 10, 2019 03:42
Segmentation fault when using reactingFOAM for Fluids Tommy Floessner OpenFOAM Running, Solving & CFD 4 April 22, 2018 13:30
Cannot run the code properly: very large time step continuity error crst15 OpenFOAM Running, Solving & CFD 9 December 14, 2014 19:17
Moving mesh Niklas Wikstrom (Wikstrom) OpenFOAM Running, Solving & CFD 122 June 15, 2014 07:20
pimpleFoam: turbulence->correct(); is not executed when using residualControl hfs OpenFOAM Running, Solving & CFD 3 October 29, 2013 09:35


All times are GMT -4. The time now is 08:35.