|July 26, 2012, 09:43||
Running nacaAirfoil tutorial with sonicFoam
Join Date: May 2011
Posts: 4Rep Power: 4
as stated in title,running such tutorial goes nowhere,that is,no convergence at all,unstable coefficients ...I wonder if there is any setting-up problem or so.
I have also tried a naca study at high subsonic regime (about M=0.6) but drives to the same conclusions (also using sonicFoam).Is there any better solver to use for these range?
I would appreciate any lifeboat in this turbulent sea
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