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Airfoil analysis convergence problem

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Old   August 27, 2014, 09:47
Default Airfoil analysis convergence problem
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mayursindhav is on a distinguished road
Hello friend

I am simulating airfoil NACA0012 tlat 18 degree of attack but it is not converge. Graph is straight.
I am try by reduce courent number(my solution is density based), refine mesh,
Help to come out from this
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