General Aviation Externally Flapped Airfoil
These data are purely theoretical, and were generated using the MCARFA program, a 2D inviscid panel code with and integral boundary layer method. Lift coefficients were crudely corrected for separation, but no corrections were applied to any of the other data. These data are presented for educational purposes only. Basing any aircraft design on these data is not advised.
Last Updated on 4/24/99
By Thomas E. Speer