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#1 |
Member
Tom
Join Date: Apr 2017
Posts: 50
Rep Power: 9 ![]() |
Hi all,
I was wondering if there's any solver in the Openfoam framework that is suited for transonic flows where Mach number is 0.95-1.3; I have tried rhoSimpleFoam with transonic option but it proved to be unreliable and often unexplainably crash. Running transient solvers is not an option as I do not have to computational power required for my problem. I'm simulating an aircraft that's 10m in length and the computational domain is 100m in each direction. |
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#2 |
Senior Member
Klaus
Join Date: Mar 2009
Posts: 287
Rep Power: 23 ![]() |
Hi,
many factors influence stability - it's difficult to help without information: What's your case setup? fvSchemes, fvSolution What kind of mesh do you use? Do you have any idea of the mesh quality? What's the mesh size? What hardware do you use: CPU, GPU, RAM? Klaus |
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Tags |
density based solver, rhosimplefoam, transonic aircraft |
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