Flapping Wing

This flapping wing was calculated using the unsteady vortex panel methodAlan Lai’s Fortran code. It assumes inviscid incompressible potential flow (irrotational). I also have a working Mathematica version of this code, but it is a little lengthy to show here.

Flapping Wing – Fortran 90, rendered in POV-Ray 3.6.1, 4/28/06


2 Responses to “Flapping Wing”

  1. 1 doctsh
    April 9, 2011 at 9:32 am

    Is it possible to create a simulation like this using your model?

    please if possible teach me..


  2. 2 Karim Alame
    December 9, 2011 at 8:00 am

    this is very interesting, is the FORTRAN code available ?

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