April 7, 2017, 16:09
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rhoCentralFoam inviscid airfoil issue (Foam::error::printStack(Foam::Ostream&) at ??)
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#1
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New Member
Join Date: Mar 2017
Posts: 1
Rep Power: 0
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Hi everyone
I am attempting to solve a few inviscid compressible flow cases for a few different angles of attack on a simple NACA0012 airfoil using OpenFOAM 4.1.
The errors I get are as shown below:
Quote:
#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::tmp<Foam::GeometricField<Foam::Vector<double >, Foam::fvsPatchField, Foam::surfaceMesh> > Foam: perator/<Foam::Vector<double>, Foam::fvsPatchField, Foam::surfaceMesh>(Foam::GeometricField<Foam::Vect or<double>, Foam::fvsPatchField, Foam::surfaceMesh> const&, Foam::GeometricField<double, Foam::fvsPatchField, Foam::surfaceMesh> const&) at ??:?
#4 ? at ??:?
#5 __libc_start_main in "/lib/x86_64-linux-gnu/libc.so.6"
#6 ? at ??:?
Floating point exception (core dumped)
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I have attached a picture of the geometry and provided a dropbox link to the entire case file, including logs for checkMesh and rhoCentralFoam. I think that I may have an issue with my boundary conditions as well as I have not specified temperature BCs before.
https://www.dropbox.com/sh/98k3efcdx...Z4yMdTG_a?dl=0
Any help with my issue here would be very useful as I am new to OF and have just attempted using Helyx to fix my issue, but cannot control the solver it uses.
Cheers
kmkb21
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