|October 14, 2007, 00:39||
NLF0416 at M=0.69, cann't get convergence
I want to make a computation of NLF0416 airfoil with SST k-omega model in FLUENT.
The far field boundary conditions is as follows,
M=0.69 Re=4.0e6 Tu=0.3% Rt=5
But I can not get a converged solution, even I set the Courant No. as 1.0
I hope someone can help me. There are the 'cas' file and the grid 'gg' file.
I hope someone can have a trial with my grid and my 'cas' file in FLUENT and tell me what is the problem with my computation.
Thanks a lot!!!
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