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April 23, 2019, 01:17 |
sigFpe with RhocentralFoam
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#1 |
New Member
Anon
Join Date: Apr 2019
Posts: 4
Rep Power: 7 |
I posted a week ago, wanted to bring this situation back up. I am receiving the following error in the code below
Code:
forceCoeffs output: Cd = 4.32461766e-05 Cl = -0.001073409762 Cm = 0 Cl(f) = -0.0005367048812 Cl(r) = -0.0005367048812 Mean and max Courant Numbers = 0.0006168517913 0.09999926631 deltaT = 9.556576144e-10 Time = 3.3447378e-07 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 = 8.557600945e-07, Final residual = 2.321937886e-14, No Iterations 2 smoothSolver: Solving for Uy, Initial residual = 1.026404812e-05, Final residual = 5.437169473e-13, No Iterations 2 smoothSolver: Solving for Uz, Initial residual = 1.992196399e-09, Final residual = 6.780166413e-17, No Iterations 2 diagonal: Solving for rhoE, Initial residual = 0, Final residual = 0, No Iterations 0 #0 Foam::error::printStack(Foam::Ostream&) at ??:? #1 Foam::sigFpe::sigHandler(int) at ??:? #2 in "/lib64/libc.so.6" #3 Foam::ePsiThermo<Foam::pureMixture<Foam::sutherlandTransport<Foam::specieThermo<Foam::eConstThermo<Foam::perfectGas> > > > >::calculate() at ??:? #4 Foam::ePsiThermo<Foam::pureMixture<Foam::sutherlandTransport<Foam::specieThermo<Foam::eConstThermo<Foam::perfectGas> > > > >::correct() at ??:? #5 at ??:? #6 __libc_start_main in "/lib64/libc.so.6" #7 at ??:? /tmp/slurmd/job15559167/slurm_script: line 13: 93677 Floating point exceptionrhoCentralFoam Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2.1.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volVectorField; location "0"; object U; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 1 -1 0 0 0 0]; internalField uniform (790 0 0); boundaryField { Atmosphere { type zeroGradient; } Inlet { type fixedValue; value uniform (790 0 0); } Jet { type fixedValue; value uniform (0 0 317); } Outlet { type zeroGradient; } Plate { type fixedValue; value uniform (0 0 0); } Low { type fixedValue; value uniform (0 0 0); } Mid { type fixedValue; value uniform (0 0 0); } High { type fixedValue; value uniform (0 0 0); } } // *********************************************************************** / Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2.1.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volScalarField; location "0"; object p; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [1 -1 -2 0 0 0 0]; internalField uniform 1210; boundaryField { Atmosphere { type zeroGradient; } Inlet { type fixedValue; value uniform 1210; } Jet { type fixedValue; value uniform 160000; } Outlet { type zeroGradient; } Plate { type zeroGradient; } Low { type zeroGradient; } Mid { type zeroGradient; } High { type zeroGradient; } } // *********************************************************************** // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2.1.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class volScalarField; location "0"; object T; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // dimensions [0 0 0 1 0 0 0]; internalField uniform 62; boundaryField { Atmosphere { type zeroGradient; } Inlet { type inletOutlet; inletValue uniform 62; value uniform 62; } Jet { type inletOutlet; inletValue uniform 250; value uniform 250; } Outlet { type zeroGradient; } Plate { type zeroGradient; } Low { type zeroGradient; } Mid { type zeroGradient; } High { type zeroGradient; } } // *********************************************************************** // Code:
/*--------------------------------*- C++ -*----------------------------------*\ | ========= | | | \\ / F ield | OpenFOAM: The Open Source CFD Toolbox | | \\ / O peration | Version: 2.1.1 | | \\ / A nd | Web: www.OpenFOAM.org | | \\/ M anipulation | | \*---------------------------------------------------------------------------*/ FoamFile { version 2.0; format ascii; class polyBoundaryMesh; location "constant/polyMesh"; object boundary; } // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * // 7 ( Jet { type patch; nFaces 8000; startFace 22942400; } Inlet { type patch; nFaces 39200; startFace 22950400; } Outlet { type patch; nFaces 132000; startFace 22989600; } Plate { type wall; nFaces 11200; startFace 23121600; } Low { type wall; nFaces 1600; startFace 23132800; } Mid { type wall; nFaces 1600; startFace 23134400; } High { type wall; nFaces 1600; startFace 23136000; } ) // *********************************************************************** // |
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