I am looking for data about the Korn airfoil (with single flap), for which an exact potential flow solution can be derived (if I remember this correctly).
Can anyone provide me references to this airfoil and the solution ?! In particular I am interested, if someone could provide me a multiblock structured grid for this test case and maybe a little program that computes the exact solution. I guess that there should be a couple of people who used this test case to validate their basic euler code as well.
I greately appreciate your help.
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