Aerodyn Design Forum

I'm interested in comparing genuine (measured in a wind tunnel) lift/drag/etc data for any airfol with the data that various computer programs produce.

Can anyone help me find a well-tested airfoil and the test data that goes with it?  I'd prefer an airfoil that's not symetrical (eg: a "wing" section or something that produces lift at AofA=0) - and it would be especially helpful to have tunnel data for angles of 0 through 360 degrees.

Thanks if anyone can help!

Companies do not give out their wind tunnel data eaisly, however, there are lots of NACA reports on the internet if you search for NACA (http://www.pdas.com/avd.htm).  Also he most comprensive list of Airfoils tables in the book, http://www.amazon.com/s?ie=UTF8&search-type=ss&index=books&field-author=A.%20E.%20von%20Doenhoff&page=1

good luck