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(OpenFOAM) OpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/About.txt

 

Originally copied from from C:\cfd\blueCFD-SingleCore-2.1\OpenFOAM-2.1\tutorials\compressible\rhoSimplecFoam\squareBend
Changed shape and setup

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/case.foam

 

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/CreateMesh.gnumeric

 

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./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound.bat

 

blockMesh.exe
rhoSimplecFoam.exe
paraFoam

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/system/controlDict

 

/*--------------------------------*- 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      controlDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

application     rhoSimplecFoam;

startFrom       startTime;

startTime       0;

stopAt          endTime;

endTime         1;

deltaT          0.01;

writeControl    timeStep;

writeInterval   1;

purgeWrite      0;

writeFormat     ascii;

writePrecision  6;

writeCompression off;

timeFormat      general;

timePrecision   6;

graphFormat     raw;

runTimeModifiable true;


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/system/decomposeParDict

 

/*--------------------------------*- 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      decomposeParDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

numberOfSubdomains 8;

method          hierarchical;

simpleCoeffs
{
    n               (8 1 1);
    delta           0.001;
}

hierarchicalCoeffs
{
    n               (4 2 1);
    delta           0.001;
    order           xyz;
}

manualCoeffs
{
    dataFile        "";
}

distributed     no;

roots           ( );


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/system/fvSchemes

 

/*--------------------------------*- 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             steadyState;
}

gradSchemes
{
    default             Gauss linear;
}

divSchemes
{
    default             none;

    div(phi,U)          Gauss upwind;
    div((muEff*dev2(T(grad(U)))))      Gauss linear;
    div(phi,h)          Gauss upwind;
    div(phi,epsilon)    Gauss upwind;
    div(phi,k)          Gauss upwind;

    div(phid,p)         Gauss upwind;
    div(phi,K)          Gauss upwind;

    //div((phi|interpolate(rho)),p)          Gauss upwind; //NEW
}

laplacianSchemes
{
    default         Gauss linear corrected;
}

interpolationSchemes
{
    default         linear;
    //UD              upwind phid;
}

snGradSchemes
{
    default         corrected;
}

fluxRequired
{
    default         no;
    p;
    pCorr;
}

// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/system/fvSolution

 

/*--------------------------------*- 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-08;
        relTol          0.1;
        smoother        GaussSeidel;
        nPreSweeps      0;
        nPostSweeps     2;
        nFinestSweeps   2;
        cacheAgglomeration true;
        nCellsInCoarsestLevel 20;
        agglomerator    faceAreaPair;
        mergeLevels     1;
    }

    "(U|h|k|epsilon)"
    {
        solver          GAMG;
        tolerance       1e-08;
        relTol          0.1;
        smoother        GaussSeidel;
        nPreSweeps      0;
        nPostSweeps     2;
        nFinestSweeps   2;
        cacheAgglomeration true;
        nCellsInCoarsestLevel 20;
        agglomerator    faceAreaPair;
        mergeLevels     1;
    }
}

SIMPLE
{
    nNonOrthogonalCorrectors 0;
    rhoMin          rhoMin [1 -3 0 0 0] 0.1;
    rhoMax          rhoMax [1 -3 0 0 0] 1.0;
    transonic       yes;
}

relaxationFactors
{
    fields
    {
        p               1;
        rho             1;
    }
    equations
    {
        U               0.9;
        h               0.8;
        k               0.9;
        epsilon         0.9;
pEqn 0.3;
    }
}

// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/RASProperties

 

/*--------------------------------*- 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    "constant";
    object      RASProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

RASModel        kEpsilon;

turbulence      on;

printCoeffs     on;


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/thermophysicalProperties

 

/*--------------------------------*- 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    "constant";
    object      thermophysicalProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

thermoType      hPsiThermo<pureMixture<sutherlandTransport<specieThermo<hConstThermo<perfectGas>>>>>;

mixture
{
    specie
    {
        nMoles      1;
        molWeight   28.9;
    }
    thermodynamics
    {
        Cp          1007;
        Hf          0;
    }
    transport
    {
        As          1.4792e-06;
        Ts          116;
    }
}


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/turbulenceProperties

 

/*--------------------------------*- 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    "constant";
    object      turbulenceProperties;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

simulationType  RASModel;


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/polyMesh/blockMeshDict

 

/*--------------------------------*- 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      blockMeshDict;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

convertToMeters 0.001;

vertices
(
  ( 9.375 0 15 ) // point 0
  ( 12.5 3.125 15 ) // point 1
  ( 15.625 0 15 ) // point 2
  ( 12.5 -3.125 15 ) // point 3
  ( 9.375 0 0 ) // point 4
  ( 12.5 3.125 0 ) // point 5
  ( 15.625 0 0 ) // point 6
  ( 12.5 -3.125 0 ) // point 7
  ( 0 0 0 ) // point 8
  ( 25 43.3012701892219 0 ) // point 9
  ( 25 -43.3012701892219 0 ) // point 10
  ( 0 0 -5 ) // point 11
  ( 25 43.3012701892219 -5 ) // point 12
  ( 25 -43.3012701892219 -5 ) // point 13

  (50 0 0 ) // point 14 //Perhaps needs four vertices per face?
  (50 0 -5 ) // point 15 //Perhaps needs four vertices per face?
);

blocks
(
    hex (4 7 6 5 0 3  2  1 ) inlet  ( 20 20 20)  simpleGrading (1 1 1)
    hex (11 13 15 12 8 10 14 9 ) outlet (20 20 20)  simpleGrading (1 1 1)
);

edges
(
  //Cylinder top
  line 0 1 //Curve these later, e.g. 'arc  0  1  ( 17.678  17.678  25)'
  line 1 2
  line 2 3
  line 3 0
  //Cylinder bottom
  line 4 5
  line 5 6
  line 6 7
  line 7 4
  //Cylinder vertical
  line 0 4
  line 1 5
  line 2 6
  line 3 7
  //Pie top
  line 8 9
  line 9 14
  line 14 10
  line 10 8
  //Pie bottom
  line 11 12
  line 12 15
  line 15 13
  line 13 11
  //Pie vertical
  line 8 11
  line 9 12
  line 10 13
  line 14 15
);

boundary
(
//faces must be traversed clockwise when looking from inside

    // is there no way of defining all my 'defaultFaces' to be 'wall'?
    Default_Boundary_Region
    {
        type wall;
        faces
        (
            //bottom
            ( 11 12 15 13)
        );
    }
    inlet
    {
        type patch;
        faces
        (
            (0 3 2 1)
        );
    }
    outlet
    {
        type patch;
        faces
        (
            (9 14 15 12)
            (10 13 15 14)
        );
    }

    sides
    {
        type symmetryPlane;
        faces
        (
            (8 9 12 11)
            (8 11 13 10)
        );
    }
);

mergePatchPairs
(
);

// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/polyMesh/boundary

 

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.1                                   |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
/*   Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt   *\
|  Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com   |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       polyBoundaryMesh;
    location    "constant/polyMesh";
    object      boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

5
(
    Default_Boundary_Region
    {
        type            wall;
        nFaces          400;
        startFace       45600;
    }
    inlet
    {
        type            patch;
        nFaces          400;
        startFace       46000;
    }
    outlet
    {
        type            patch;
        nFaces          800;
        startFace       46400;
    }
    sides
    {
        type            symmetryPlane;
        nFaces          800;
        startFace       47200;
    }
    defaultFaces
    {
        type            empty;
        nFaces          2400;
        startFace       48000;
    }
)

// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/polyMesh/cellZones

 

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.1                                   |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
/*   Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt   *\
|  Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com   |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       regIOobject;
    location    "constant/polyMesh";
    object      cellZones;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

2
(
inlet
{
    type cellZone;
cellLabels      List<label>
8000
(
0
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
[...]
15956
15957
15958
15959
15960
15961
15962
15963
15964
15965
15966
15967
15968
15969
15970
15971
15972
15973
15974
15975
15976
15977
15978
15979
15980
15981
15982
15983
15984
15985
15986
15987
15988
15989
15990
15991
15992
15993
15994
15995
15996
15997
15998
15999
)
;
}
)

// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/polyMesh/faces

 

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.1                                   |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
/*   Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt   *\
|  Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com   |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       faceList;
    location    "constant/polyMesh";
    object      faces;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //


50400
(
4(1 22 463 442)
4(21 462 463 22)
4(441 442 463 462)
4(2 23 464 443)
4(22 463 464 23)
4(442 443 464 463)
4(3 24 465 444)
4(23 464 465 24)
4(443 444 465 464)
4(4 25 466 445)
4(24 465 466 25)
4(444 445 466 465)
4(5 26 467 446)
4(25 466 467 26)
4(445 446 467 466)
4(6 27 468 447)
4(26 467 468 27)
4(446 447 468 467)
4(7 28 469 448)
4(27 468 469 28)
4(447 448 469 468)
4(8 29 470 449)
4(28 469 470 29)
4(448 449 470 469)
4(9 30 471 450)
4(29 470 471 30)
4(449 450 471 470)
4(10 31 472 451)
4(30 471 472 31)
4(450 451 472 471)
4(11 32 473 452)
4(31 472 473 32)
4(451 452 473 472)
4(12 33 474 453)
4(32 473 474 33)
4(452 453 474 473)
4(13 34 475 454)
4(33 474 475 34)
4(453 454 475 474)
4(14 35 476 455)
4(34 475 476 35)
4(454 455 476 475)
4(15 36 477 456)
4(35 476 477 36)
4(455 456 477 476)
4(16 37 478 457)
4(36 477 478 37)
4(456 457 478 477)
4(17 38 479 458)
4(37 478 479 38)
4(457 458 479 478)
4(18 39 480 459)
4(38 479 480 39)
4(458 459 480 479)
4(19 40 481 460)
4(39 480 481 40)
4(459 460 481 480)
4(40 481 482 41)
4(460 461 482 481)
4(22 43 484 463)
4(42 483 484 43)
4(462 463 484 483)
4(23 44 485 464)
4(43 484 485 44)
4(463 464 485 484)
4(24 45 486 465)
4(44 485 486 45)
4(464 465 486 485)
4(25 46 487 466)
4(45 486 487 46)
4(465 466 487 486)
4(26 47 488 467)
4(46 487 488 47)
4(466 467 488 487)
4(27 48 489 468)
4(47 488 489 48)
4(467 468 489 488)
[...]
4(18392 18393 18414 18413)
4(18413 18414 18435 18434)
4(18434 18435 18456 18455)
4(18455 18456 18477 18476)
4(18476 18477 18498 18497)
4(18497 18498 18519 18518)
4(18099 18100 18121 18120)
4(18120 18121 18142 18141)
4(18141 18142 18163 18162)
4(18162 18163 18184 18183)
4(18183 18184 18205 18204)
4(18204 18205 18226 18225)
4(18225 18226 18247 18246)
4(18246 18247 18268 18267)
4(18267 18268 18289 18288)
4(18288 18289 18310 18309)
4(18309 18310 18331 18330)
4(18330 18331 18352 18351)
4(18351 18352 18373 18372)
4(18372 18373 18394 18393)
4(18393 18394 18415 18414)
4(18414 18415 18436 18435)
4(18435 18436 18457 18456)
4(18456 18457 18478 18477)
4(18477 18478 18499 18498)
4(18498 18499 18520 18519)
4(18100 18101 18122 18121)
4(18121 18122 18143 18142)
4(18142 18143 18164 18163)
4(18163 18164 18185 18184)
4(18184 18185 18206 18205)
4(18205 18206 18227 18226)
4(18226 18227 18248 18247)
4(18247 18248 18269 18268)
4(18268 18269 18290 18289)
4(18289 18290 18311 18310)
4(18310 18311 18332 18331)
4(18331 18332 18353 18352)
4(18352 18353 18374 18373)
4(18373 18374 18395 18394)
4(18394 18395 18416 18415)
4(18415 18416 18437 18436)
4(18436 18437 18458 18457)
4(18457 18458 18479 18478)
4(18478 18479 18500 18499)
4(18499 18500 18521 18520)
)


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/polyMesh/neighbour

 

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.1                                   |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
/*   Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt   *\
|  Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com   |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       labelList;
    note        "nPoints: 18522 nCells: 16000 nFaces: 50400 nInternalFaces: 45600";
    location    "constant/polyMesh";
    object      neighbour;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //


45600
(
1
20
400
2
21
401
3
22
402
4
23
403
5
24
404
6
25
405
7
26
406
8
27
407
9
28
408
10
29
409
11
30
410
12
31
411
13
32
412
14
33
413
15
34
414
16
35
415
17
36
416
18
37
417
19
38
418
39
419
21
40
420
22
41
421
23
42
422
24
43
423
25
44
424
26
45
[...]
15967
15986
15968
15987
15969
15988
15970
15989
15971
15990
15972
15991
15973
15992
15974
15993
15975
15994
15976
15995
15977
15996
15978
15997
15979
15998
15999
15981
15982
15983
15984
15985
15986
15987
15988
15989
15990
15991
15992
15993
15994
15995
15996
15997
15998
15999
)


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/polyMesh/owner

 

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.1                                   |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
/*   Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt   *\
|  Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com   |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       labelList;
    note        "nPoints: 18522 nCells: 16000 nFaces: 50400 nInternalFaces: 45600";
    location    "constant/polyMesh";
    object      owner;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //


50400
(
0
0
0
1
1
1
2
2
2
3
3
3
4
4
4
5
5
5
6
6
6
7
7
7
8
8
8
9
9
9
10
10
10
11
11
11
12
12
12
13
13
13
14
14
14
15
15
15
16
16
16
17
17
17
18
18
18
19
19
20
20
20
21
21
21
22
22
22
23
23
23
24
24
24
25
25
[...]
15897
15917
15937
15957
15977
15997
15618
15638
15658
15678
15698
15718
15738
15758
15778
15798
15818
15838
15858
15878
15898
15918
15938
15958
15978
15998
15619
15639
15659
15679
15699
15719
15739
15759
15779
15799
15819
15839
15859
15879
15899
15919
15939
15959
15979
15999
)


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/polyMesh/points

 

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.1                                   |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
/*   Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt   *\
|  Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com   |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       vectorField;
    location    "constant/polyMesh";
    object      points;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //


18522
(
(0.009375 0 0)
(0.00953125 -0.00015625 0)
(0.0096875 -0.0003125 0)
(0.00984375 -0.00046875 0)
(0.01 -0.000625 0)
(0.01015625 -0.00078125 0)
(0.0103125 -0.0009375 0)
(0.01046875 -0.00109375 0)
(0.010625 -0.00125 0)
(0.01078125 -0.00140625 0)
(0.0109375 -0.0015625 0)
(0.01109375 -0.00171875 0)
(0.01125 -0.001875 0)
(0.01140625 -0.00203125 0)
(0.0115625 -0.0021875 0)
(0.01171875 -0.00234375 0)
(0.011875 -0.0025 0)
(0.01203125 -0.00265625 0)
(0.0121875 -0.0028125 0)
(0.01234375 -0.00296875 0)
(0.0125 -0.003125 0)
(0.00953125 0.00015625 0)
(0.0096875 -1.270323545e-019 0)
(0.00984375 -0.00015625 0)
(0.01 -0.0003125 0)
(0.01015625 -0.00046875 0)
(0.0103125 -0.000625 0)
(0.01046875 -0.00078125 0)
(0.010625 -0.0009375 0)
(0.01078125 -0.00109375 0)
(0.0109375 -0.00125 0)
(0.01109375 -0.00140625 0)
(0.01125 -0.0015625 0)
(0.01140625 -0.00171875 0)
(0.0115625 -0.001875 0)
(0.01171875 -0.00203125 0)
(0.011875 -0.0021875 0)
(0.01203125 -0.00234375 0)
(0.0121875 -0.0025 0)
(0.01234375 -0.00265625 0)
(0.0125 -0.0028125 0)
(0.01265625 -0.00296875 0)
(0.0096875 0.0003125 0)
(0.00984375 0.00015625 0)
(0.01 6.041716606e-020 0)
(0.01015625 -0.00015625 0)
(0.0103125 -0.0003125 0)
(0.01046875 -0.00046875 0)
(0.010625 -0.000625 0)
(0.01078125 -0.00078125 0)
(0.0109375 -0.0009375 0)
(0.01109375 -0.00109375 0)
(0.01125 -0.00125 0)
(0.01140625 -0.00140625 0)
(0.0115625 -0.0015625 0)
(0.01171875 -0.00171875 0)
(0.011875 -0.001875 0)
(0.01203125 -0.00203125 0)
(0.0121875 -0.0021875 0)
(0.01234375 -0.00234375 0)
(0.0125 -0.0025 0)
(0.01265625 -0.00265625 0)
(0.0128125 -0.0028125 0)
(0.00984375 0.00046875 0)
(0.01 0.0003125 0)
(0.01015625 0.00015625 0)
(0.0103125 -6.021839566e-020 0)
(0.01046875 -0.00015625 0)
(0.010625 -0.0003125 0)
(0.01078125 -0.00046875 0)
(0.0109375 -0.000625 0)
(0.01109375 -0.00078125 0)
(0.01125 -0.0009375 0)
(0.01140625 -0.00109375 0)
(0.0115625 -0.00125 0)
(0.01171875 -0.00140625 0)
(0.011875 -0.0015625 0)
[...]
(0.04375 0.002165063509 0)
(0.045 3.593913361e-019 0)
(0.04625 -0.002165063509 0)
(0.0475 -0.004330127019 0)
(0.02375 0.04113620668 0)
(0.025 0.03897114317 0)
(0.02625 0.03680607966 0)
(0.0275 0.03464101615 0)
(0.02875 0.03247595264 0)
(0.03 0.03031088913 0)
(0.03125 0.02814582562 0)
(0.0325 0.02598076211 0)
(0.03375 0.0238156986 0)
(0.035 0.02165063509 0)
(0.03625 0.01948557159 0)
(0.0375 0.01732050808 0)
(0.03875 0.01515544457 0)
(0.04 0.01299038106 0)
(0.04125 0.01082531755 0)
(0.0425 0.008660254038 0)
(0.04375 0.006495190528 0)
(0.045 0.004330127019 0)
(0.04625 0.002165063509 0)
(0.0475 2.840248291e-018 0)
(0.04875 -0.002165063509 0)
(0.025 0.04330127019 0)
(0.02625 0.04113620668 0)
(0.0275 0.03897114317 0)
(0.02875 0.03680607966 0)
(0.03 0.03464101615 0)
(0.03125 0.03247595264 0)
(0.0325 0.03031088913 0)
(0.03375 0.02814582562 0)
(0.035 0.02598076211 0)
(0.03625 0.0238156986 0)
(0.0375 0.02165063509 0)
(0.03875 0.01948557159 0)
(0.04 0.01732050808 0)
(0.04125 0.01515544457 0)
(0.0425 0.01299038106 0)
(0.04375 0.01082531755 0)
(0.045 0.008660254038 0)
(0.04625 0.006495190528 0)
(0.0475 0.004330127019 0)
(0.04875 0.002165063509 0)
(0.05 0 0)
)


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/polyMesh/sets/inlet

 

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.1                                   |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
/*   Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt   *\
|  Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com   |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       cellSet;
    location    "constant/polyMesh/sets";
    object      inlet;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //


8000
(
0
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
[...]
7953
7954
7955
7956
7957
7958
7959
7960
7961
7962
7963
7964
7965
7966
7967
7968
7969
7970
7971
7972
7973
7974
7975
7976
7977
7978
7979
7980
7981
7982
7983
7984
7985
7986
7987
7988
7989
7990
7991
7992
7993
7994
7995
7996
7997
7998
7999
)

// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/constant/polyMesh/sets/outlet

 

/*--------------------------------*- C++ -*----------------------------------*\
| =========                 |                                                 |
| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
|  \\    /   O peration     | Version:  2.1                                   |
|   \\  /    A nd           | Web:      www.OpenFOAM.org                      |
|    \\/     M anipulation  |                                                 |
\*---------------------------------------------------------------------------*/
/*   Windows 32 and 64 bit porting by blueCAPE: http://www.bluecape.com.pt   *\
|  Based on Windows porting (2.0.x v4) by Symscape: http://www.symscape.com   |
\*---------------------------------------------------------------------------*/
FoamFile
{
    version     2.0;
    format      ascii;
    class       cellSet;
    location    "constant/polyMesh/sets";
    object      outlet;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //


8000
(
8000
8001
8002
8003
8004
8005
8006
8007
8008
8009
8010
8011
8012
8013
8014
8015
8016
8017
8018
8019
8020
8021
8022
8023
8024
8025
8026
8027
8028
8029
8030
8031
8032
8033
8034
8035
8036
8037
8038
8039
8040
8041
8042
8043
8044
8045
8046
8047
8048
8049
8050
8051
8052
8053
8054
8055
8056
8057
8058
8059
8060
8061
8062
8063
8064
8065
8066
8067
8068
8069
8070
8071
8072
8073
8074
8075
8076
[...]
15953
15954
15955
15956
15957
15958
15959
15960
15961
15962
15963
15964
15965
15966
15967
15968
15969
15970
15971
15972
15973
15974
15975
15976
15977
15978
15979
15980
15981
15982
15983
15984
15985
15986
15987
15988
15989
15990
15991
15992
15993
15994
15995
15996
15997
15998
15999
)

// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/0/alphat

 

/*--------------------------------*- 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       volScalarField;
    location    "0";
    object      alphat;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
dimensions      [1 -1 -1 0 0 0 0];

internalField   uniform 0;

boundaryField
{
    Default_Boundary_Region
    {
        type            alphatWallFunction;
        Prt             0.85;
        value           uniform 0;
    }
    inlet
    {
        type            calculated;
        value           uniform 0;
    }
    outlet
    {
        type            calculated;
        value           uniform 0;
    }
    //Modified by Richel Bilderbeek
    sides
    {
        type            symmetryPlane;
    }
}


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/0/epsilon

 

/*--------------------------------*- 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       volScalarField;
    location    "0";
    object      epsilon;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [0 2 -3 0 0 0 0];

internalField   uniform 200;

boundaryField
{
    Default_Boundary_Region
    {
        type            compressible::epsilonWallFunction;
        Cmu             0.09;
        kappa           0.41;
        E               9.8;
        value           uniform 200;
    }
    inlet
    {
        type            compressible::turbulentMixingLengthDissipationRateInlet;
        mixingLength    0.005;
        value           uniform 200;
    }
    outlet
    {
        type            inletOutlet;
        inletValue      uniform 200;
        value           uniform 200;
    }
    //Modified by Richel Bilderbeek
    sides
    {
        type            symmetryPlane;
    }
}


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/0/k

 

/*--------------------------------*- 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       volScalarField;
    location    "0";
    object      k;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [0 2 -2 0 0 0 0];

internalField   uniform 1;

boundaryField
{
    Default_Boundary_Region
    {
        type            compressible::kqRWallFunction;
        value           uniform 1;
    }
    inlet
    {
        type            turbulentIntensityKineticEnergyInlet;
        intensity       0.05;
        value           uniform 1;
    }
    outlet
    {
        type            inletOutlet;
        inletValue      uniform 1;
        value           uniform 1;
    }
    //Modified by Richel Bilderbeek
    sides
    {
        type            symmetryPlane;
    }
}


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/0/mut

 

/*--------------------------------*- 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       volScalarField;
    location    "0";
    object      mut;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [1 -1 -1 0 0 0 0];

internalField   uniform 0;

boundaryField
{
    Default_Boundary_Region
    {
        type            mutkWallFunction;
        Cmu             0.09;
        kappa           0.41;
        E               9.8;
        value           uniform 0;
    }
    inlet
    {
        type            calculated;
        value           uniform 0;
    }
    outlet
    {
        type            calculated;
        value           uniform 0;
    }
    //Modified by Richel Bilderbeek
    sides
    {
        type            symmetryPlane;
    }
}


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/0/p

 

/*--------------------------------*- 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       volScalarField;
    object      p;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [1 -1 -2 0 0 0 0];

internalField   uniform 110000;

boundaryField
{
    Default_Boundary_Region
    {
        type            zeroGradient;
    }
    //Modified by Richel Bilderbeek
    sides
    {
        type            symmetryPlane;
    }
    inlet
    {
        //type            zeroGradient;
        type            mixed;
        refValue        uniform 110000;
        refGradient     uniform 0;
        valueFraction   uniform 0.3;
    }
    outlet
    {
        type            fixedValue;
        value           uniform 110000;

        //type            mixed;
        //refValue        uniform 110000;
        //refGradient     uniform 0;
        //valueFraction   uniform 1;
        //type            transonicOutletPressure;
        //U               U;
        //phi             phi;
        //gamma           1.4;
        //psi             psi;
        //pInf            uniform 110000;
    }
}


// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/0/T

 

/*--------------------------------*- 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       volScalarField;
    object      T;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [0 0 0 1 0 0 0];

internalField   uniform 1000;

boundaryField
{
    Default_Boundary_Region
    {
        type            zeroGradient;
    }

    inlet
    {
        type            fixedValue;
        value           uniform 1000;
    }

    outlet
    {
        type            inletOutlet;
        //type            zeroGradient;
        value           uniform 1000;
        inletValue      uniform 1000;
    }
    //Modified by Richel Bilderbeek
    sides
    {
        type            symmetryPlane;
    }
}

// ************************************************************************* //

 

 

 

 

 

./ToolOpenFoamErrorRhosimplecFoamCrashAtTimestep1SimpleNoConvergenceCriteriaFound/0/U

 

/*--------------------------------*- 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       volVectorField;
    object      U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [0 1 -1 0 0 0 0];

internalField   uniform (0 0 0);

boundaryField
{
    Default_Boundary_Region
    {
        type            fixedValue;
        value           uniform (0 0 0);
    }
    inlet
    {
        type            flowRateInletVelocity;
        flowRate        constant 0.5; //0.75;
        value           uniform (0 0 0);
    }
    outlet
    {
        type            inletOutlet;
        value           uniform (0 0 0);
        inletValue      uniform (0 0 0);
    }
//Modified by Richel Bilderbeek
    sides
    {
        type            symmetryPlane;
    }
}


// ************************************************************************* //

 

 

 

 

 

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