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June 7, 2022, 07:37 |
openfoam motorbike benchmark explosion
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Join Date: Jun 2022
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Dear forum,
I'm by no means a knowledgeable openfoam user since I have no clue about CFD in general. However, my intention is to run a scalable openfoam benchmark for which I found this one: https://github.com/do-jason/OpenFOAM...arks/motorbike The benchmark looks good to me (I guess) since I could tune the size of the problem (MCells) and the number of cpus. The problem with it is that the simulation explodes after the first few steps. I've compiled two openfoam version (V2112 and V2106) and tested the 42 MCells setup using 16 cores and 1 TB of RAM. With both openfoam versions I get this log in which the 'sum local' number in the 'time step continuity errors' line diverges extremely quickly leading to a simulation failure: Code:
... Time = 1 smoothSolver: Solving for Ux, Initial residual = 0.287454, Final residual = 0.0159974, No Iterations 22 smoothSolver: Solving for Uy, Initial residual = 0.670437, Final residual = 0.0578161, No Iterations 19 smoothSolver: Solving for Uz, Initial residual = 0.713336, Final residual = 0.0384459, No Iterations 19 GAMG: Solving for p, Initial residual = 1, Final residual = 0.131524, No Iterations 1000 time step continuity errors : sum local = 1.81912e+08, global = 861174, cumulative = 861174 smoothSolver: Solving for omega, Initial residual = 0.113341, Final residual = 0.00964374, No Iterations 4 smoothSolver: Solving for k, Initial residual = 1, Final residual = 0.0804192, No Iterations 4 ExecutionTime = 174.48 s ClockTime = 174 s forceCoeffs forceCoeffs1 execute: Coefficients Cd : 2.2912e+14 (pressure: 2.2912e+14 viscous: 3.724e+07) Cs : 1.5138e+13 (pressure: 1.51381e+13 viscous: -6.80952e+07) Cl : 7.90224e+12 (pressure: 7.90232e+12 viscous: -8.50578e+07) CmRoll : -3.08433e+13 (pressure: -3.08433e+13 viscous: 8.91239e+06) CmPitch : 9.23788e+13 (pressure: 9.23788e+13 viscous: 2.55493e+06) CmYaw : -1.7646e+13 (pressure: -1.7646e+13 viscous: -2.22275e+07) Cd(f) : 8.37169e+13 Cd(r) : 1.45404e+14 Cs(f) : -1.0077e+13 Cs(r) : 2.52151e+13 Cl(f) : 9.63299e+13 Cl(r) : -8.84277e+13 Time = 2 smoothSolver: Solving for Ux, Initial residual = 0.665592, Final residual = 0.0643762, No Iterations 47 smoothSolver: Solving for Uy, Initial residual = 0.610635, Final residual = 0.0404073, No Iterations 58 smoothSolver: Solving for Uz, Initial residual = 0.600655, Final residual = 0.0574642, No Iterations 45 GAMG: Solving for p, Initial residual = 1, Final residual = 0.0199624, No Iterations 1000 time step continuity errors : sum local = 2.39263e+19, global = -7.23625e+16, cumulative = -7.23625e+16 smoothSolver: Solving for omega, Initial residual = 0.107859, Final residual = 0.00710626, No Iterations 4 smoothSolver: Solving for k, Initial residual = 0.381193, Final residual = 0.0353298, No Iterations 3 ExecutionTime = 341 s ClockTime = 341 s forceCoeffs forceCoeffs1 execute: Coefficients Cd : 2.41032e+33 (pressure: 2.41032e+33 viscous: -7.07675e+19) Cs : 5.40342e+33 (pressure: 5.40342e+33 viscous: 2.95738e+20) Cl : 7.57467e+32 (pressure: 7.57467e+32 viscous: -3.32622e+19) CmRoll : -2.66388e+33 (pressure: -2.66388e+33 viscous: -1.76725e+20) CmPitch : 1.04103e+33 (pressure: 1.04103e+33 viscous: -3.59468e+19) CmYaw : 8.57365e+31 (pressure: 8.57365e+31 viscous: 7.09699e+19) Cd(f) : -1.45872e+33 Cd(r) : 3.86904e+33 Cs(f) : 2.78745e+33 Cs(r) : 2.61598e+33 Cl(f) : 1.41977e+33 Cl(r) : -6.62301e+32 Time = 3 [19] #0 Foam::error::printStack(Foam::Ostream&) at ??:? [19] #1 Foam::sigFpe::sigHandler(int) at ??:? [19] #2 ? in /lib/x86_64-linux-gnu/libc.so.6 [19] #3 Foam::GaussSeidelSmoother::smooth(Foam::word const&, Foam::Field<double>&, Foam::lduMatrix const&, Foam::Field<double> const&, Foam::FieldField<Foam::Field, double> const&, Foam::UPtrList<Foam::lduInterfaceField const> const&, unsigned char, int) at ??:? ... Any advise about stabilizing this simulation is greatly appreciated. |
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