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

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  • Опубліковано 25 лис 2024

КОМЕНТАРІ • 5

  • @iamSR007
    @iamSR007 7 місяців тому +2

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

  • @aliasady2181
    @aliasady2181 26 днів тому

    Thanks sir . it was helpful

  • @vvise4179
    @vvise4179 2 місяці тому

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

  • @emredemir229
    @emredemir229 6 місяців тому

    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.

  • @ersahguloglu2577
    @ersahguloglu2577 7 місяців тому

    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?