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Showing results 1 to 1 of 1 Search took 0.00 seconds. Search: Posts Made By: Sachchit

Forum: SU2 November 26, 2014, 04:22

Replies: 2 Steady State solution Views: 1,899 Posted By Sachchit Hi Ajinkya, NACA 0012 at Angle of Attack as... Hi Ajinkya, NACA 0012 at Angle of Attack as high as 18 or 20 will have flow separation. This will give rise to wake region behind the airfoil which is unsteady in nature. In this case the steady...

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