[Jerry123]

Hi guys

I'm simulating a 3D shuttlecock with simplefoam solver together with k esilon model. However, when I simulated it with several angle of attack by editing the velocity components and changed the boundary condition to 2 inlets and 2 outlets, the below error messages came out. After that, I turned off the turbulence mode and it worked well. But is there anyone know how to get the results with turbulence model?

#0 Foam::error:rintStack(Foam::Ostream&) at ??:?
#1 Foam::sigFpe::sigHandler(int) at ??:?
#2 ? in "/usr/lib/x86_64-linux-gnu/libc.so.6"
#3 double Foam::sumProd<double>(Foam::UList<double> const&, Foam::UList<double> const&) at ??:?
#4 Foam::PBiCGStab::solve(Foam::Field<double>&, Foam::Field<double> const&, unsigned char) const at ??:?
#5 Foam::fvMatrix<double>::solveSegregated(Foam::dict ionary const&) at ??:?
#6 Foam::fvMatrix<double>::solve(Foam::dictionary const&) at ??:?
#7 Foam::fvMatrix<double>::solve() at ??:?
#8 Foam::SolverPerformance<double> Foam::solve<double>(Foam::tmp<Foam::fvMatrix<doubl e> > const&) at ??:?
#9 Foam::RASModels::kEpsilon<Foam::incompressibleMome ntumTransportModel>::correct() at ??:?
#10 ? in "/opt/openfoam11/platforms/linux64GccDPInt32Opt/bin/foamRun"
#11 ? in "/usr/lib/x86_64-linux-gnu/libc.so.6"
#12 __libc_start_main in "/usr/lib/x86_64-linux-gnu/libc.so.6"
#13 ? in "/opt/openfoam11/platforms/linux64GccDPInt32Opt/bin/foamRun"
Floating point exception