Simulating NACA 2412 Airfoil over Varied Angles of Attack in Ansys Fluent with Verification

[@aliasady2181]

Thanks sir . it was helpful

[@iamSR007]

Sir , Thank You. Can you kindly share the files, especially the matlab plot codes and all🥰🥰

[@emredemir229]

Thank you for the very well description. I have a question how you can be sure that the same iteration number is OK for all angles? I am not quite sure that the simulation can be converged with 1000 iterations for 12-14-16 degres.

[@vvise4179]

How did you get the conversion so fast? Can you show us the making of the mesh

[@ersahguloglu2577]

Hey I want to do an analysis for supercritical airfoil. Is this set up options are okay for that or should I change some options if yes what are they? Could you help me with that?