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

Foam::error::printStack(Foam::Ostream&) with simpleFoam -parallel

Register Blogs Community New Posts Updated Threads Search

Like Tree24Likes

Reply
 
LinkBack Thread Tools Search this Thread Display Modes
Old   August 30, 2018, 03:05
Default Foam::error::printStack(Foam::Ostream&)
  #41
New Member
 
Vitor Dal Bó Abella
Join Date: May 2016
Posts: 6
Rep Power: 10
2vdba2 is on a distinguished road
I solved the problem changing from steadyState to Euler (on fvSchemes).


Now it is:


ddtSchemes
{
default Euler;
}
2vdba2 is offline   Reply With Quote

Old   February 9, 2020, 06:15
Post Foam::error::printStack(Foam::Ostream&)
  #42
Member
 
cal
Join Date: Feb 2020
Location: nowhere
Posts: 65
Rep Power: 6
saidc. is on a distinguished road
Hi, I'm getting similar error. I've tried a lot of things but i didn't solve my problem. My solver is interFoam. Just look at deltaT and alpha.water values in error file. How can i fix this? Any suggestion?
(I used SolidWorks 2016, salome 8.4.0, openfoam-7, ubuntu 18.04 and i customized classic laminar/damBreak case.)



boundary

Code:
{
    version     2.0;
    format      ascii;
    class       polyBoundaryMesh;
    location    "constant/polyMesh";
    object      boundary;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

5
(
    leftWall
    {
        type            wall;
        inGroups        List<word> 1(wall);
        nFaces          116;
        startFace       26049;
    }
    rightWall
    {
        type            wall;
        inGroups        List<word> 1(wall);
        nFaces          80;
        startFace       26165;
    }
    lowerWall
    {
        type            wall;
        inGroups        List<word> 1(wall);
        nFaces          136;
        startFace       26245;
    }
    atmosphere
    {
        type            patch;
        nFaces          120;
        startFace       26381;
    }
    defaultFaces
    {
        type            empty;
        inGroups        List<word> 1(empty);
        nFaces          9918;
        startFace       26501;
    }
)

// ************************************************************************* //
alpha.water

Code:
FoamFile
{
    version     2.0;
    format      ascii;
    class       volScalarField;
    object      alpha.water;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [0 0 0 0 0 0 0];

internalField   uniform 0;

boundaryField
{
    leftWall
    {
        type            zeroGradient;
    }

    rightWall
    {
        type            zeroGradient;
    }

    lowerWall
    {
        type            zeroGradient;
    }

    atmosphere
    {
        type            inletOutlet;
        inletValue      uniform 0;
        value           uniform 0;
    }

    defaultFaces
    {
        type            empty;
    }
}
p_rgh

Code:
FoamFile
{
    version     2.0;
    format      ascii;
    class       volScalarField;
    object      p_rgh;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

dimensions      [1 -1 -2 0 0 0 0];

internalField   uniform 0;

boundaryField
{
    leftWall
    {
        type            fixedFluxPressure;
        value           uniform 0;
    }

    rightWall
    {
        type            fixedFluxPressure;
        value           uniform 0;
    }

    lowerWall
    {
        type            fixedFluxPressure;
        value           uniform 0;
    }

    atmosphere
    {
        type            totalPressure;
        p0              uniform 0;
    }

    defaultFaces
    {
        type            empty;
    }
}
U

Code:
FoamFile
{
    version     2.0;
    format      ascii;
    class       volVectorField;
    location    "0";
    object      U;
}
// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //

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

internalField   uniform (0 0 0);

boundaryField
{
    leftWall
    {
        type            noSlip;
    }
    rightWall
    {
        type            noSlip;
    }
    lowerWall
    {
        type            noSlip;
    }
    atmosphere
    {
        type            pressureInletOutletVelocity;
        value           uniform (0 0 0);
    }
    defaultFaces
    {
        type            empty;
    }
}
HERE MY ERROR
Code:
smoothSolver:  Solving for alpha.water, Initial residual = 5.98474e-05, Final residual = 3.88048e-11, No Iterations 2
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -4.44338e-68  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -3.52175e-17  Max(alpha.water) = 1
DICPCG:  Solving for p_rgh, Initial residual = 0.781862, Final residual = 0.0317406, No Iterations 8
time step continuity errors : sum local = 0.000492867, global = -3.45236e-08, cumulative = 0.00744918
DICPCG:  Solving for p_rgh, Initial residual = 0.608476, Final residual = 0.0248548, No Iterations 8
time step continuity errors : sum local = 0.00162432, global = 1.66769e-08, cumulative = 0.0074492
DICPCG:  Solving for p_rgh, Initial residual = 0.618346, Final residual = 9.228e-08, No Iterations 362
time step continuity errors : sum local = 2.749e-08, global = -8.68054e-10, cumulative = 0.0074492
ExecutionTime = 35.66 s  ClockTime = 36 s

Courant Number mean: 0.0396433 max: 17.064
Interface Courant Number mean: 0.00390682 max: 5.60411
deltaT = 7.77403e-100
Time = 0.00119069

smoothSolver:  Solving for alpha.water, Initial residual = 5.84367e-05, Final residual = 3.60982e-11, No Iterations 2
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -4.44162e-68  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -5.0219e-17  Max(alpha.water) = 1
DICPCG:  Solving for p_rgh, Initial residual = 0.779072, Final residual = 0.0316353, No Iterations 8
time step continuity errors : sum local = 7.53892e-05, global = -4.91121e-09, cumulative = 0.00744919
DICPCG:  Solving for p_rgh, Initial residual = 0.607604, Final residual = 0.0248692, No Iterations 8
time step continuity errors : sum local = 0.000248544, global = 2.35874e-09, cumulative = 0.00744919
DICPCG:  Solving for p_rgh, Initial residual = 0.616997, Final residual = 9.84716e-08, No Iterations 362
time step continuity errors : sum local = 4.46598e-09, global = -1.34046e-10, cumulative = 0.00744919
ExecutionTime = 36.11 s  ClockTime = 37 s

Courant Number mean: 0.00599844 max: 2.59439
Interface Courant Number mean: 0.000588719 max: 0.891569
deltaT = 1.49824e-100
Time = 0.00119069

smoothSolver:  Solving for alpha.water, Initial residual = 5.73287e-05, Final residual = 3.53128e-11, No Iterations 2
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -4.43785e-68  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -6.81171e-17  Max(alpha.water) = 1
DICPCG:  Solving for p_rgh, Initial residual = 0.776517, Final residual = 0.0313868, No Iterations 8
time step continuity errors : sum local = 0.00048802, global = -2.93771e-08, cumulative = 0.00744916
DICPCG:  Solving for p_rgh, Initial residual = 0.606532, Final residual = 0.0247253, No Iterations 8
time step continuity errors : sum local = 0.00160604, global = 1.3903e-08, cumulative = 0.00744918
DICPCG:  Solving for p_rgh, Initial residual = 0.615519, Final residual = 9.41518e-08, No Iterations 340
time step continuity errors : sum local = 2.75985e-08, global = -1.00355e-09, cumulative = 0.00744918
ExecutionTime = 36.54 s  ClockTime = 37 s

Courant Number mean: 0.0385174 max: 16.7802
Interface Courant Number mean: 0.00380786 max: 6.09569
deltaT = 4.4643e-102
Time = 0.00119069

smoothSolver:  Solving for alpha.water, Initial residual = 5.61634e-05, Final residual = 3.3963e-11, No Iterations 2
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -4.42924e-68  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -4.35845e-17  Max(alpha.water) = 1
DICPCG:  Solving for p_rgh, Initial residual = 0.773262, Final residual = 0.0307347, No Iterations 8
time step continuity errors : sum local = 7.27895e-05, global = -3.94879e-09, cumulative = 0.00744917
DICPCG:  Solving for p_rgh, Initial residual = 0.604857, Final residual = 0.024329, No Iterations 8
time step continuity errors : sum local = 0.000239488, global = 2.02513e-09, cumulative = 0.00744917
DICPCG:  Solving for p_rgh, Initial residual = 0.613341, Final residual = 9.64352e-08, No Iterations 362
time step continuity errors : sum local = 4.2589e-09, global = -1.19707e-10, cumulative = 0.00744917
ExecutionTime = 36.98 s  ClockTime = 38 s

Courant Number mean: 0.00578662 max: 2.56257
Interface Courant Number mean: 0.000578441 max: 0.973182
deltaT = 8.71061e-103
Time = 0.00119069

smoothSolver:  Solving for alpha.water, Initial residual = 5.49118e-05, Final residual = 3.2171e-11, No Iterations 2
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -4.4112e-68  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -3.96341e-16  Max(alpha.water) = 1
DICPCG:  Solving for p_rgh, Initial residual = 0.770017, Final residual = 0.0299674, No Iterations 8
time step continuity errors : sum local = 0.000454079, global = -2.18559e-08, cumulative = 0.00744915
DICPCG:  Solving for p_rgh, Initial residual = 0.602994, Final residual = 0.0293486, No Iterations 5
time step continuity errors : sum local = 0.00183973, global = 9.67059e-08, cumulative = 0.00744925
DICPCG:  Solving for p_rgh, Initial residual = 0.620295, Final residual = 9.23708e-08, No Iterations 342
time step continuity errors : sum local = 2.46046e-08, global = -9.39872e-11, cumulative = 0.00744925
ExecutionTime = 37.41 s  ClockTime = 38 s

Courant Number mean: 0.0322515 max: 17.5305
Interface Courant Number mean: 0.00359975 max: 6.76509
deltaT = 2.48441e-104
Time = 0.00119069

smoothSolver:  Solving for alpha.water, Initial residual = 4.83567e-05, Final residual = 1.91459e-11, No Iterations 2
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -1.04402e-46  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -2.51392e-17  Max(alpha.water) = 1
DICPCG:  Solving for p_rgh, Initial residual = 0.742106, Final residual = 0.0363213, No Iterations 7
time step continuity errors : sum local = 6.49571e-05, global = -5.59286e-11, cumulative = 0.00744925
DICPCG:  Solving for p_rgh, Initial residual = 0.606875, Final residual = 0.0274085, No Iterations 5
time step continuity errors : sum local = 0.000207145, global = 4.45286e-09, cumulative = 0.00744925
DICPCG:  Solving for p_rgh, Initial residual = 0.619751, Final residual = 9.17399e-08, No Iterations 362
time step continuity errors : sum local = 3.04518e-09, global = -6.90435e-11, cumulative = 0.00744925
ExecutionTime = 37.86 s  ClockTime = 38 s

Courant Number mean: 0.0040732 max: 2.24028
Interface Courant Number mean: 0.000418459 max: 0.609483
deltaT = 5.54488e-105
Time = 0.00119069

smoothSolver:  Solving for alpha.water, Initial residual = 4.76685e-05, Final residual = 2.01965e-11, No Iterations 2
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -9.91398e-47  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -3.04471e-17  Max(alpha.water) = 1
DICPCG:  Solving for p_rgh, Initial residual = 0.744592, Final residual = 0.0363254, No Iterations 5
time step continuity errors : sum local = 0.000498639, global = 1.99994e-08, cumulative = 0.00744927
DICPCG:  Solving for p_rgh, Initial residual = 0.623883, Final residual = 0.0268522, No Iterations 5
time step continuity errors : sum local = 0.00154667, global = -3.01824e-08, cumulative = 0.00744924
DICPCG:  Solving for p_rgh, Initial residual = 0.613925, Final residual = 9.08759e-08, No Iterations 363
time step continuity errors : sum local = 2.22317e-08, global = -4.95163e-10, cumulative = 0.00744924
ExecutionTime = 38.34 s  ClockTime = 39 s

Courant Number mean: 0.0304221 max: 16.379
Interface Courant Number mean: 0.00306763 max: 4.27059
deltaT = 1.69268e-106
Time = 0.00119069

smoothSolver:  Solving for alpha.water, Initial residual = 4.75175e-05, Final residual = 1.99622e-11, No Iterations 2
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -4.24586e-68  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -3.42133e-17  Max(alpha.water) = 1
DICPCG:  Solving for p_rgh, Initial residual = 0.743859, Final residual = 0.0325512, No Iterations 5
time step continuity errors : sum local = 6.12945e-05, global = 4.61408e-09, cumulative = 0.00744925
DICPCG:  Solving for p_rgh, Initial residual = 0.616162, Final residual = 0.0244443, No Iterations 5
time step continuity errors : sum local = 0.000188544, global = -8.24671e-09, cumulative = 0.00744924
DICPCG:  Solving for p_rgh, Initial residual = 0.605392, Final residual = 9.66245e-08, No Iterations 362
time step continuity errors : sum local = 3.08855e-09, global = -3.55315e-11, cumulative = 0.00744924
ExecutionTime = 38.79 s  ClockTime = 39 s

Courant Number mean: 0.0042222 max: 2.28614
Interface Courant Number mean: 0.000412843 max: 0.511151
deltaT = 3.70205e-107
Time = 0.00119069

smoothSolver:  Solving for alpha.water, Initial residual = 4.32103e-05, Final residual = 1.9414e-11, No Iterations 2
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -4.1624e-68  Max(alpha.water) = 1
MULES: Correcting alpha.water
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.0746171  Min(alpha.water) = -2.01258e-17  Max(alpha.water) = 1
#0  Foam::error::printStack(Foam::Ostream&) at ??:?
#1  Foam::sigFpe::sigHandler(int) at ??:?
#2  ? in "/lib/x86_64-linux-gnu/libc.so.6"
#3  double Foam::sumProd<double>(Foam::UList<double> const&, Foam::UList<double> const&) at ??:?
#4  Foam::PCG::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
#5  Foam::fvMatrix<double>::solveSegregated(Foam::dictionary const&) at ??:?
#6  Foam::fvMatrix<double>::solve(Foam::dictionary const&) in "/opt/openfoam7/platforms/linux64GccDPInt32Opt/bin/interFoam"
#7  Foam::fvMatrix<double>::solve() in "/opt/openfoam7/platforms/linux64GccDPInt32Opt/bin/interFoam"
#8  ? in "/opt/openfoam7/platforms/linux64GccDPInt32Opt/bin/interFoam"
#9  __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6"
#10  ? in "/opt/openfoam7/platforms/linux64GccDPInt32Opt/bin/interFoam"
saidc. is offline   Reply With Quote

Old   May 22, 2020, 13:20
Default
  #43
Member
 
Join Date: Apr 2018
Location: UK
Posts: 78
Rep Power: 8
JM27 is on a distinguished road
Hi Said,

Such small values of deltaT are an indication that the velocity is extremely large. Perhaps it would be a good idea to monitor your minimum and maximum values of velocity in the domain.

That said, I'm also having a similar error but I am using compressibleInterFoam, I was wondering IF and HOW you have managed to solve this error?

I look forward to your reply!

Regards,

JM
hogsonik and saidc. like this.
JM27 is offline   Reply With Quote

Old   September 3, 2020, 10:54
Default
  #44
New Member
 
wanghongjie
Join Date: Apr 2020
Posts: 28
Rep Power: 6
wanghongjie is on a distinguished road
Quote:
Originally Posted by mbay101 View Post
Hi everybody,

I m having as it seems the same Probleme . I m using chtMultiRegionSimpleFoam in OP 2.2.0 to simulate a solid Region and a Fluid Region Tempratur Transfer. The Boundary Condition were taking from the OF example HeatTransfert and i did the same with the Files in system. I m using Salome to create my mesh after that i use mappedWall in Boundary to connect the Region.

Code:
#0 Foam::error::printStack(Foam::Ostream&) in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
#1 Foam::sigSegv::sigHandler(int) in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
#2 
at sigaction.c:0
#3 Foam::polyMeshTetDecomposition::findFaceBasePts(Foam::polyMesh const&, double, bool) in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
#4 Foam::polyMesh::tetBasePtIs() const in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/lib/libOpenFOAM.so"
#5 Foam::mappedPatchBase::facePoints(Foam::polyPatch const&) const in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/lib/libmeshTools.so"
#6 Foam::mappedPatchBase::calcMapping() const in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/lib/libmeshTools.so"
#7 void Foam::mappedPatchBase::distribute<double>(Foam::List<double>&) const in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/lib/libfiniteVolume.so"
#8 Foam::compressible::turbulentTemperatureCoupledBaffleMixedFvPatchScalarField::updateCoeffs() in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/lib/libcompressibleTurbulenceModel.so"
#9 Foam::mixedFvPatchField<double>::evaluate(Foam::UPstream::commsTypes) in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/lib/libfiniteVolume.so"
#10 Foam::mixedEnergyFvPatchScalarField::updateCoeffs() in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/lib/libfluidThermophysicalModels.so"
#11 Foam::fvMatrix<double>::fvMatrix(Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&, Foam::dimensionSet const&) in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/bin/chtMultiRegionSimpleFoam"
#12 
in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/bin/chtMultiRegionSimpleFoam"
#13 
in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/bin/chtMultiRegionSimpleFoam"
#14 __libc_start_main in "/lib64/libc.so.6"
#15 
in "/cax/sw/OPENFOAM/LINUX_x86_64/OpenFOAM-2.2.0/platforms/linux64GccDPOpt/bin/chtMultiRegionSimpleFoam"
./solve: line 5: 10011 Segmentation fault (core dumped) chtMultiRegionSimpleFoam
I attached to this message my system and my 0 directory.
Please!! Please!! take a look at them and if you have any idea what so ever that can help me understand the reason then please shared with me.

In working a Project and i don t have any support from my Team. This is my only option for me to get same Tipps and Help.

Thank you!!
best Regards
Did you have a solution? I have the same question, maybe you can help me somewhere.
wanghongjie is offline   Reply With Quote

Old   September 26, 2020, 14:48
Default
  #45
Member
 
Riddhideep Biswas
Join Date: May 2020
Posts: 30
Rep Power: 6
Rid@foam is on a distinguished road
Hello everyone!!
I am trying to run a lagrangian simulation using sprayFoam solver and I am getting an error as shown

#0 Foam::error:rintStack(Foam::Ostream&) at ??:?
#1 Foam::sigFpe::sigHandler(int) at ??:?
#2 ? in "/lib/x86_64-linux-gnu/libc.so.6"
#3 Foam::divide(Foam::Field<double>&, Foam::UList<double> const&, Foam::UList<double> const&) at ??:?
#4 Foam:perator/(Foam::UList<double> const&, Foam::UList<double> const&) at ??:?
#5 ? in "/home/riddhideep/OpenFOAM/OpenFOAM-6/platforms/linux64GccDPInt32Opt/bin/sprayFoam"
#6 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6"
#7 ? in "/home/riddhideep/OpenFOAM/OpenFOAM-6/platforms/linux64GccDPInt32Opt/bin/sprayFoam"
Floating point exception (core dumped)

Below I am attaching all the files I am using in the form of a google drive link.
Please take a look at the files and help me how to get rid of this error.

https://drive.google.com/drive/folde...-3?usp=sharing
Rid@foam is offline   Reply With Quote

Old   September 26, 2020, 15:57
Default Problem in simulating the liquid jet
  #46
New Member
 
CA
Join Date: Sep 2020
Posts: 2
Rep Power: 0
Monika Yadav is on a distinguished road
Hi,

I made a closed geometry in Solidwords and imported it into openfoam (trisurface).I defined the blockmesh such that it encloses the structure.I am using surfacefeatureextract and snappyhexmesh.Runnning the case just for streamline case now using simplefoam. The error is when i convert to FoamToVTK than it says

size 50000 is not in the range of 1872638.
Can anyone suggest?

Thanks
Monika
Monika Yadav is offline   Reply With Quote

Old   March 25, 2021, 06:28
Default Reply to problem simulation liquid jet
  #47
New Member
 
Laurens
Join Date: Jun 2020
Location: Antwerp, Belgium
Posts: 6
Rep Power: 6
LVH_CFD is on a distinguished road
Quote:
Originally Posted by Monika Yadav View Post
Hi,

I made a closed geometry in Solidwords and imported it into openfoam (trisurface).I defined the blockmesh such that it encloses the structure.I am using surfacefeatureextract and snappyhexmesh.Runnning the case just for streamline case now using simplefoam. The error is when i convert to FoamToVTK than it says

size 50000 is not in the range of 1872638.
Can anyone suggest?

Thanks
Monika

Whenever I recieve a message like that it means that I made a change to my mesh after having set initial values. You should check all the files in the 0 directory and make sure that none of them contain a list of cell points with cell points from the old mesh.
My guess is that you ran a simulation, refined the mesh and then not updated your 0 folder.



Hope this helps!
LVH_CFD is offline   Reply With Quote

Old   March 26, 2022, 05:57
Default
  #48
New Member
 
Ali Can
Join Date: Apr 2021
Posts: 28
Rep Power: 5
Ryuzaki is on a distinguished road
Hello dear foamers,

I have a similar problem with simulating in parallel using rhoCentralFoam. I have tried many changes in my setup, but have not been successful. Here is my error notes and checkMesh notes. I also shared my folders.

I'm looking forward to your suggestions, thanks in advance..


Quote:
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: v1812 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
Build : v1812 OPENFOAM=1812
Arch : "LSB;label=32;scalar=64"
Exec : checkMesh
Date : Mar 26 2022
Time : 12:51:38
Host : sariyer
PID : 178429
I/O : uncollated
Case : /okyanus/users/afadil/acf/00B
nProcs : 1
trapFpe: Floating point exception trapping enabled (FOAM_SIGFPE).
fileModificationChecking : Monitoring run-time modified files using timeStampMas ter (fileModificationSkew 10)
allowSystemOperations : Allowing user-supplied system call operations

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

Create mesh for time = 0

Time = 0

Mesh stats
points: 1807047
faces: 5099080
internal faces: 4903916
cells: 1646904
faces per cell: 6.07382
boundary patches: 5
point zones: 0
face zones: 0
cell zones: 0

Overall number of cells of each type:
hexahedra: 1603980
prisms: 8
wedges: 8
pyramids: 0
tet wedges: 0
tetrahedra: 112
polyhedra: 42796
Breakdown of polyhedra by number of faces:
faces number of cells
6 1572
7 2460
8 124
9 37576
10 8
12 1056

Checking topology...
Boundary definition OK.
Cell to face addressing OK.
Point usage OK.
Upper triangular ordering OK.
Face vertices OK.
Number of regions: 1 (OK).

Checking patch topology for multiply connected surfaces...
Patch Faces Points Surface topology
symmetry1 63992 67474 ok (non-closed singly connected)
top 59532 60501 ok (non-closed singly connected)
bottom 68508 69613 ok (non-closed singly connected)
outlet 1566 1726 ok (non-closed singly connected)
inlet 1566 1726 ok (non-closed singly connected)

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

Checking basic cellZone addressing...
No cellZones found.

Checking geometry...
Overall domain bounding box (-0.05 0 -4.33681e-19) (0.126 0.0384 0.0127)
Mesh has 3 geometric (non-empty/wedge) directions (1 1 1)
Mesh has 3 solution (non-empty) directions (1 1 1)
Boundary openness (1.23181e-16 -9.82673e-14 -1.18362e-17) OK.
Max cell openness = 3.25366e-16 OK.
Max aspect ratio = 124.201 OK.
Minimum face area = 1.09571e-10. Maximum face area = 2.6226e-06. Face area magnitudes OK.
Min volume = 1.09571e-14. Max volume = 4.09912e-09. Total volume = 6.10667e -05. Cell volumes OK.
Mesh non-orthogonality Max: 57.5968 average: 13.7674
Non-orthogonality check OK.
Face pyramids OK.
Max skewness = 2.38176 OK.
Coupled point location match (average 0) OK.

Mesh OK.

End
Quote:
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: v1812 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
Build : v1812 OPENFOAM=1812
Arch : "LSB;label=32;scalar=64"
Exec : rhoCentralFoam -parallel -case /okyanus/users/afadil/acf/00B
Date : Mar 26 2022
Time : 12:47:32
Host : s205
PID : 268505
I/O : uncollated
Case : /okyanus/users/afadil/acf/00B
nProcs : 40
Hosts :
(
(s205 40)
)
Pstream initialized with:
floatTransfer : 0
nProcsSimpleSum : 0
commsType : nonBlocking
polling iterations : 0
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

Using LTS
Reading thermophysical properties

Selecting thermodynamics package
{
type hePsiThermo;
mixture pureMixture;
transport sutherland;
thermo janaf;
equationOfState perfectGas;
specie specie;
energy sensibleInternalEnergy;
}

Reading field U

Creating turbulence model

Selecting turbulence model type RAS
Selecting RAS turbulence model kOmegaSST
Selecting patchDistMethod meshWave
RAS
{
RASModel kOmegaSST;
turbulence on;
printCoeffs on;
alphaK1 0.85;
alphaK2 1;
alphaOmega1 0.5;
alphaOmega2 0.856;
gamma1 0.555556;
gamma2 0.44;
beta1 0.075;
beta2 0.0828;
betaStar 0.09;
a1 0.31;
b1 1;
c1 10;
F3 false;
decayControl false;
kInf 0;
omegaInf 0;
}

Creating finite volume options from "system/fvOptions"

Selecting finite volume options type limitTemperature
Source: limitT
- selecting all cells
- selected 1646904 cell(s) with volume 6.10667e-05

Starting time loop

fieldAverage fieldAverage1:
Restarting averaging for fields:
U: starting averaging at time 0
p: starting averaging at time 0

Mean and max Courant Numbers = 0.0014347 0.262613
Flow time scale min/max = 4.28387e-09, 2.03396e-08
Time = 1.125e-09

diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
diagonal: Solving for rhoUx, Initial residual = 0, Final residual = 0, No Iterations 0
diagonal: Solving for rhoUy, Initial residual = 0, Final residual = 0, No Iterations 0
diagonal: Solving for rhoUz, Initial residual = 0, Final residual = 0, No Iterations 0
smoothSolver: Solving for Ux, Initial residual = 1, Final residual = 9.91481e-08, No Iterations 159
smoothSolver: Solving for Uy, Initial residual = 1, Final residual = 9.53803e-08, No Iterations 131
smoothSolver: Solving for Uz, Initial residual = 0.481511, Final residual = 9.73196e-08, No Iterations 111
diagonal: Solving for rhoE, Initial residual = 0, Final residual = 0, No Iterations 0
GAMG: Solving for e, Initial residual = 0.095494, Final residual = 0.000522242, No Iterations 2
GAMG: Solving for omega, Initial residual = 0.017991, Final residual = 8.45975e-05, No Iterations 3
bounding omega, min: -79757.3 max: 3.89408e+09 average: 2.52554e+08
smoothSolver: Solving for k, Initial residual = 1, Final residual = 4.9169e-08, No Iterations 12
ExecutionTime = 2.07 s ClockTime = 3 s

fieldAverage fieldAverage1:
Reading/initialising field UMean
Reading/initialising field pMean
Reading/initialising field UPrime2Mean
Reading/initialising field pPrime2Mean

fieldAverage fieldAverage1 write:
Calculating averages

Mean and max Courant Numbers = 0.00143492 0.261351
Flow time scale min/max = 4.30455e-09, 2.03404e-08
Time = 2.25e-09

diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
diagonal: Solving for rhoUx, Initial residual = 0, Final residual = 0, No Iterations 0
diagonal: Solving for rhoUy, Initial residual = 0, Final residual = 0, No Iterations 0
diagonal: Solving for rhoUz, Initial residual = 0, Final residual = 0, No Iterations 0
smoothSolver: Solving for Ux, Initial residual = 0.000994925, Final residual = 2.68726e-08, No Iterations 1
smoothSolver: Solving for Uy, Initial residual = 0.000364341, Final residual = 7.56062e-08, No Iterations 1
smoothSolver: Solving for Uz, Initial residual = 0.0042112, Final residual = 2.08737e-09, No Iterations 2
diagonal: Solving for rhoE, Initial residual = 0, Final residual = 0, No Iterations 0
GAMG: Solving for e, Initial residual = 0.000137899, Final residual = 1.74764e-09, No Iterations 1
--> FOAM Warning :
From function virtual void Foam::fv:ption::checkApplied() const
in file cfdTools/general/fvOptions/fvOption.C at line 125
Source limitT defined for field e but never used
--> FOAM Warning :
From function virtual void Foam::fv:ption::checkApplied() const
in file cfdTools/general/fvOptions/fvOption.C at line 125
Source limitT defined for field e but never used
GAMG: Solving for omega, Initial residual = 0.000546902, Final residual = 3.751e-07, No Iterations 1
--> FOAM Warning :
From function virtual void Foam::fv:ption::checkApplied() const
in file cfdTools/general/fvOptions/fvOption.C at line 125
Source limitT defined for field e but never used
--> FOAM Warning :
From function virtual void Foam::fv:ption::checkApplied() const
in file cfdTools/general/fvOptions/fvOption.C at line 125
Source limitT defined for field e but never used
smoothSolver: Solving for k, Initial residual = 0.330261, Final residual = 3.36906e-08, No Iterations 5
ExecutionTime = 2.54 s ClockTime = 4 s

fieldAverage fieldAverage1 write:
Calculating averages

Mean and max Courant Numbers = 0.00143609 0.365354
Flow time scale min/max = 3.07921e-09, 2.12312e-08
Time = 3.375e-09

diagonal: Solving for rho, Initial residual = 0, Final residual = 0, No Iterations 0
diagonal: Solving for rhoUx, Initial residual = 0, Final residual = 0, No Iterations 0
diagonal: Solving for rhoUy, Initial residual = 0, Final residual = 0, No Iterations 0
diagonal: Solving for rhoUz, Initial residual = 0, Final residual = 0, No Iterations 0
smoothSolver: Solving for Ux, Initial residual = 0.00117023, Final residual = 4.19306e-08, No Iterations 1
smoothSolver: Solving for Uy, Initial residual = 0.000554007, Final residual = 9.40954e-08, No Iterations 1
smoothSolver: Solving for Uz, Initial residual = 0.00465589, Final residual = 1.67531e-09, No Iterations 2
diagonal: Solving for rhoE, Initial residual = 0, Final residual = 0, No Iterations 0
GAMG: Solving for e, Initial residual = 0.000217566, Final residual = 1.90397e-09, No Iterations 1
--------------------------------------------------------------------------
A process has executed an operation involving a call to the
"fork()" system call to create a child process. Open MPI is currently
operating in a condition that could result in memory corruption or
other system errors; your job may hang, crash, or produce silent
data corruption. The use of fork() (or system() or other calls that
create child processes) is strongly discouraged.

The process that invoked fork was:

Local host: [[45705,1],24] (PID 268529)

If you are *absolutely sure* that your application will successfully
and correctly survive a call to fork(), you may disable this warning
by setting the mpi_warn_on_fork MCA parameter to 0.
--------------------------------------------------------------------------
[s205:268529] *** Process received signal ***
[s205:268529] Signal: Floating point exception (8)
[s205:268529] Signal code: (-6)
[s205:268529] Failing at address: 0xb2c000418f1
[s205:268529] [ 0] /lib64/libc.so.6(+0x362f0)[0x2b7f73d292f0]
[s205:268529] [ 1] /lib64/libc.so.6(gsignal+0x37)[0x2b7f73d29277]
[s205:268529] [ 2] /lib64/libc.so.6(+0x362f0)[0x2b7f73d292f0]
[s205:268529] [ 3] /okyanus/progs/OpenFOAM/OpenFOAM.com-v1812/OpenFOAM-v1812/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so(_ZN4Foam7sumProdIdEEdRKNS_5UListIT_ EES5_+0x25)[0x2b7f72da8f85]
[s205:268529] [ 4] /okyanus/progs/OpenFOAM/OpenFOAM.com-v1812/OpenFOAM-v1812/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so(_ZNK4Foam9PBiCGStab5solveERNS_5Fiel dIdEERKS2_h+0xb4b)[0x2b7f72bfedcb]
[s205:268529] [ 5] /okyanus/progs/OpenFOAM/OpenFOAM.com-v1812/OpenFOAM-v1812/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so(_ZNK4Foam10GAMGSolver18solveCoarses tLevelERNS_5FieldIdEERKS2_+0x1ee)[0x2b7f72c193be]
[s205:268529] [ 6] /okyanus/progs/OpenFOAM/OpenFOAM.com-v1812/OpenFOAM-v1812/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so(_ZNK4Foam10GAMGSolver6VcycleERKNS_7 PtrListINS_9lduMatrix8smootherEEERNS_5FieldIdEERKS 8_S9_S9_S9_S9_S9_RNS1_IS8_EESD_h+0x71b)[0x2b7f72c1ac3b]
[s205:268529] [ 7] /okyanus/progs/OpenFOAM/OpenFOAM.com-v1812/OpenFOAM-v1812/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so(_ZNK4Foam10GAMGSolver5solveERNS_5Fi eldIdEERKS2_h+0x523)[0x2b7f72c1ce33]
[s205:268529] [ 8] /okyanus/progs/OpenFOAM/OpenFOAM.com-v1812/OpenFOAM-v1812/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so(_ZN4Foam8fvMatrixIdE15solveSegr egatedERKNS_10dictionaryE+0x120)[0x2b7f6eec1790]
[s205:268529] [ 9] /okyanus/progs/OpenFOAM/OpenFOAM.com-v1812/OpenFOAM-v1812/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so(_ZN4Foam8fvMatrixIdE24solveSegr egatedOrCoupledERKNS_10dictionaryE+0x27f)[0x2b7f6e9bf87f]
[s205:268529] [10] /okyanus/progs/OpenFOAM/OpenFOAM.com-v1812/OpenFOAM-v1812/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so(_ZNK4Foam6fvMesh5solveERNS_8fvM atrixIdEERKNS_10dictionaryE+0xf)[0x2b7f6e98719f]
[s205:268529] [11] rhoCentralFoam(_ZN4Foam5solveIdEENS_17SolverPerfor manceIT_EERKNS_3tmpINS_8fvMatrixIS2_EEEE+0x45)[0x43ebd5]
[s205:268529] [12] /okyanus/progs/OpenFOAM/OpenFOAM.com-v1812/OpenFOAM-v1812/platforms/linux64GccDPInt32Opt/lib/libcompressibleTurbulenceModels.so(_ZN4Foam13kOmeg aSSTBaseINS_13eddyViscosityINS_8RASModelINS_15Eddy DiffusivityINS_18ThermalDiffusivityINS_27Compressi bleTurbulenceModelINS_11fluidThermoEEEEEEEEEEEE7co rrectEv+0xe10)[0x2b7f71be5890]
[s205:268529] [13] rhoCentralFoam[0x4297dd]
[s205:268529] [14] /lib64/libc.so.6(__libc_start_main+0xf5)[0x2b7f73d15445]
[s205:268529] [15] rhoCentralFoam[0x42ccbe]
[s205:268529] *** End of error message ***
--------------------------------------------------------------------------
mpirun noticed that process rank 24 with PID 268529 on node s205 exited on signal 8 (Floating point exception).
--------------------------------------------------------------------------
Quote:
[24] #0 Foam::error:rintStack(Foam::Ostream&) at ??:?
[24] #1 Foam::sigFpe::sigHandler(int) at ??:?
[24] #2 ? in /lib64/libc.so.6
[24] #3 double Foam::sumProd<double>(Foam::UList<double> const&, Foam::UList<double> const&) at ??:?
[24] #4 Foam::PBiCGStab::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
[24] #5 Foam::GAMGSolver::solveCoarsestLevel(Foam::Field<d ouble>&, Foam::Field<double> const&) const at ??:?
[24] #6 Foam::GAMGSolver::Vcycle(Foam::PtrList<Foam::lduMa trix::smoother> const&, Foam::Field<double>&, Foam::Field<double> const&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::PtrList<Foam::Field<double> >&, Foam::PtrList<Foam::Field<double> >&, unsigned char) const at ??:?
[24] #7 Foam::GAMGSolver::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
[24] #8 Foam::fvMatrix<double>::solveSegregated(Foam::dict ionary const&) at ??:?
[24] #9 Foam::fvMatrix<double>::solveSegregatedOrCoupled(F oam::dictionary const&) at ??:?
[24] #10 Foam::fvMesh::solve(Foam::fvMatrix<double>&, Foam::dictionary const&) const at ??:?
[24] #11 Foam::SolverPerformance<double> Foam::solve<double>(Foam::tmp<Foam::fvMatrix<doubl e> > const&) at ??:?
[24] #12 Foam::kOmegaSSTBase<Foam::eddyViscosity<Foam::RASM odel<Foam::EddyDiffusivity<Foam::ThermalDiffusivit y<Foam::CompressibleTurbulenceModel<Foam::fluidThe rmo> > > > > >::correct() at ??:?
[24] #13 ? at ??:?
[24] #14 __libc_start_main in /lib64/libc.so.6
[24] #15 ? at ??:?
/*---------------------------------------------------------------------------*\
| ========= | |
| \\ / F ield | OpenFOAM: The Open Source CFD Toolbox |
| \\ / O peration | Version: v1812 |
| \\ / A nd | Web: www.OpenFOAM.com |
| \\/ M anipulation | |
\*---------------------------------------------------------------------------*/
Build : v1812 OPENFOAM=1812
Arch : "LSB;label=32;scalar=64"
Exec : reconstructPar -latestTime
Date : Mar 26 2022
Time : 12:47:39
Host : s205
PID : 269361
I/O : uncollated
Case : /okyanus/users/afadil/acf/00B
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

--> FOAM Warning :
From function int main(int, char**)
in file reconstructPar.C at line 242
No times selected
Attached Files
File Type: zip sonic.zip (14.6 KB, 0 views)
Ryuzaki is offline   Reply With Quote

Old   September 21, 2022, 17:14
Default
  #49
New Member
 
openSource_Knight's Avatar
 
Giuseppe
Join Date: Aug 2022
Location: Italia
Posts: 5
Rep Power: 4
openSource_Knight is on a distinguished road
Quote:
Originally Posted by AJAY BHANDARI View Post
Thanks ehsan for your quick reply. But i was able to solve it today.

Actually in my code the variable orl value was wrongly input by me as 1 which made the denominator term zero. thats why sigFpe error was coming.

But i corrected it and solver ran successfully. But thanks for your reply...

hello Ajay, having the same problem, in serial. this is the error message i get
How did you fix?

Quote:
#0 Foam::error:: printStack(Foam::Ostream&) at ??:?
#1 Foam::sigFpe::sigHandler(int) at ??:?
#2 ? in /lib/x86_64-linux-gnu/libpthread.so.0
#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::GAMGSolver::solveCoarsestLevel(Foam::Field<d ouble>&, Foam::Field<double> const&) const at ??:?
#6 Foam::GAMGSolver::Vcycle(Foam::PtrList<Foam::lduMa trix::smoother> const&, Foam::Field<double>&, Foam::Field<double> const&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::PtrList<Foam::Field<double> >&, Foam::PtrList<Foam::Field<double> >&, unsigned char) const at ??:?
#7 Foam::GAMGSolver::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
#8 Foam::fvMatrix<double>::solveSegregated(Foam::dict ionary const&) at ??:?
#9 Foam::fvMatrix<double>::solveSegregatedOrCoupled(F oam::dictionary const&) at ??:?
#10 Foam::fvMesh::solve(Foam::fvMatrix<double>&, Foam::dictionary const&) const at ??:?
#11 ? in /usr/lib/openfoam/openfoam2106/platforms/linux64GccDPInt32Opt/bin/simpleFoam
#12 __libc_start_main in /lib/x86_64-linux-gnu/libc.so.6
#13 ? in /usr/lib/openfoam/openfoam2106/platforms/linux64GccDPInt32Opt/bin/simpleFoam
openSource_Knight is offline   Reply With Quote

Old   January 19, 2023, 08:09
Default
  #50
New Member
 
Join Date: Sep 2022
Posts: 3
Rep Power: 4
CFD- is on a distinguished road
Hi gohome,


Thanks for your suggestion. I am solving compressible flow with Peng Robinson equation of state and Sutherland for viscosity. I got a similar error where initial residual for h was close to 0.99 and floating point exception. I used 0.4 relaxation factor for p, rho, h, U, k, e and it worked!
p { line-height: 115%; margin-bottom: 0.25cm; background: transparent }
CFD- is offline   Reply With Quote

Old   June 22, 2023, 17:19
Default openfom error
  #51
New Member
 
reyhane
Join Date: Mar 2023
Posts: 1
Rep Power: 0
reyhane is on a distinguished road
hi can anyone help me with this error

smoothSolver: Solving for alpha.water, Initial residual = 1.14414e-05, Final residual = 8.06717e-09, No Iterations 1
Phase-1 volume fraction = 0.373702 Min(alpha.water) = -0.0191484 Max(alpha.water) = 1.38326
MULES: Correcting alpha.water
Phase-1 volume fraction = 0.373702 Min(alpha.water) = -0.0191484 Max(alpha.water) = 1.35623
GAMG: Solving for p_rgh, Initial residual = 1, Final residual = 0.0158173, No Iterations 50
time step continuity errors : sum local = 4.82275e-07, global = 3.02594e-07, cumulative = 3.8436e+34
#0 Foam::error:rintStack(Foam::Ostream&) at ??:?
#1 Foam::sigFpe::sigHandler(int) at ??:?
#2 ? in "/lib/x86_64-linux-gnu/libc.so.6"
#3 double Foam::sumProd<double>(Foam::UList<double> const&, Foam::UList<double> const&) at ??:?
#4 Foam::PCG::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
#5 Foam::GAMGSolver::solveCoarsestLevel(Foam::Field<d ouble>&, Foam::Field<double> const&) const at ??:?
#6 Foam::GAMGSolver::Vcycle(Foam::PtrList<Foam::lduMa trix::smoother> const&, Foam::Field<double>&, Foam::Field<double> const&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::Field<double>&, Foam::PtrList<Foam::Field<double> >&, Foam::PtrList<Foam::Field<double> >&, unsigned char) const at ??:?
#7 Foam::GAMGSolver::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
#8 Foam::fvMatrix<double>::solveSegregated(Foam::dict ionary const&) at ??:?
#9 Foam::fvMatrix<double>::solve(Foam::dictionary const&) in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/interFoam"
#10 Foam::fvMatrix<double>::solve() in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/interFoam"
#11 ? in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/interFoam"
#12 ? in "/lib/x86_64-linux-gnu/libc.so.6"
#13 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6"
#14 ? in "/opt/openfoam9/platforms/linux64GccDPInt32Opt/bin/interFoam"
Floating point exception (core dumped)
reyhane is offline   Reply With Quote

Old   September 23, 2023, 04:33
Default error in openfoam
  #52
@ss
New Member
 
shristi
Join Date: Jun 2023
Posts: 26
Rep Power: 3
@ss is on a distinguished road
I am trying to simulate rigid body motion of two cylinder in viv using overset mesh. but i found this error during simulation. Please suggest me some hint to how to handle multi cylinder using overset mesh in viv case.


Thank you in advance...
Mesh Courant Number mean: 0 max: 0
PIMPLE: iteration 1
#0 Foam::error:rintStack(Foam::Ostream&) at ??:?
#1 Foam::sigFpe::sigHandler(int) at ??:?
#2 ? in /lib/x86_64-linux-gnu/libc.so.6
#3 Foam:ILUPreconditioner::calcReciprocalD(Foam::Fi eld<double>&, Foam::lduMatrix const&) at ??:?
#4 Foam:ILUPreconditioner:ILUPreconditioner(Foam: :lduMatrix::solver const&, Foam::dictionary const&) at ??:?
#5 Foam::lduMatrix:reconditioner::addasymMatrixCons tructorToTable<Foam:ILUPreconditioner>::New(Foam ::lduMatrix::solver const&, Foam::dictionary const&) at ??:?
#6 Foam::lduMatrix:reconditioner::New(Foam::lduMatr ix::solver const&, Foam::dictionary const&) at ??:?
#7 Foam::PBiCGStab::scalarSolve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
#8 Foam::PBiCGStab::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
#9 ? at ??:?
#10 Foam::fvMesh::solve(Foam::fvMatrix<Foam::Vector<do uble> >&, Foam::dictionary const&) const at ??:?
#11 ? at ??:?
#12 ? at ??:?
#13 ? in /usr/lib/openfoam/openfoam2206/platforms/linux64GccDPInt32Opt/bin/overPimpleDyMFoam
#14 ? in /lib/x86_64-linux-gnu/libc.so.6
#15 __libc_start_main in /lib/x86_64-linux-gnu/libc.so.6
#16 ? in /usr/lib/openfoam/openfoam2206/platforms/linux64GccDPInt32Opt/bin/overPimpleDyMFoam
Floating point exception (core dumped)
@ss is offline   Reply With Quote

Old   September 23, 2023, 04:35
Default above the error
  #53
@ss
New Member
 
shristi
Join Date: Jun 2023
Posts: 26
Rep Power: 3
@ss is on a distinguished road
Starting time loop

Courant Number mean: 2.77415e-06 max: 0.00125
deltaT = 0.00120048
Time = 0.00120048

forces forces:
rho: rhoInf
Freestream density (rhoInf) set to 1
Not including porosity effects

forces forces:
rho: rhoInf
Freestream density (rhoInf) set to 1
Not including porosity effects

Rigid-body motion of the cylinder1
Centre of rotation: (16 0 0)
Orientation: (1 0 0 0 1 0 0 0 1)
Linear velocity: (0 0 0)
Angular velocity: (0 0 0)
Rigid-body motion of the cylinder2
Centre of rotation: (5.19615 3 0)
Orientation: (1 0 0 0 1 0 0 0 1)
Linear velocity: (0 0 0)
Angular velocity: (0 0 0)
inverseDistance : detected 2 mesh regions
zone:0 nCells:90000 voxels304 304 1) bb-30.0002 -40.0002 -0.500197) (150 40.0002 0.500197)
zone:1 nCells:3000 voxels304 304 1) bb-17.9982 -3.49957 -0.500006) (-14 0.499567 0.500006)
Overset analysis : nCells : 93000
calculated : 92798
interpolated : 170 (interpolated from local:95 mixed local/remote:0 remote:0)
hole : 32

Mesh Courant Number mean: 0 max: 0
PIMPLE: iteration 1
#0 Foam::error:rintStack(Foam::Ostream&) at ??:?
#1 Foam::sigFpe::sigHandler(int) at ??:?
#2 ? in /lib/x86_64-linux-gnu/libc.so.6
#3 Foam:ILUPreconditioner::calcReciprocalD(Foam::Fi eld<double>&, Foam::lduMatrix const&) at ??:?
#4 Foam:ILUPreconditioner:ILUPreconditioner(Foam: :lduMatrix::solver const&, Foam::dictionary const&) at ??:?
#5 Foam::lduMatrix:reconditioner::addasymMatrixCons tructorToTable<Foam:ILUPreconditioner>::New(Foam ::lduMatrix::solver const&, Foam::dictionary const&) at ??:?
@ss is offline   Reply With Quote

Reply


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
SimpleFoam run in Parallel jayrup OpenFOAM 9 July 26, 2019 01:00
Script to Run Parallel Jobs in Rocks Cluster asaha OpenFOAM Running, Solving & CFD 12 July 4, 2012 23:51
Error running simpleFoam in parallel skabilan OpenFOAM Running, Solving & CFD 2 August 29, 2008 10:42
Own boundary condition modified simpleFoam erorr in parallel execution sponiar OpenFOAM Running, Solving & CFD 1 August 27, 2008 10:16
Parallel Computing Classes at San Diego Supercomputer Center Jan. 20-22 Amitava Majumdar Main CFD Forum 0 January 5, 1999 13:00


All times are GMT -4. The time now is 04:43.