How to get better convergence - High speed flows
Hi
I have been simulating flows of 295.16m/s over an airfoil. I have been using SA and k-epsilon turbulence models. Once angle of attack exceeds 5+. convergence does not occur. I cannot get my head round what has to be done to values in the solution controls section. How can I increase change of convergence? Thanks for any response |
try to decrease urf factors
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