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Download Aero Troll - Hegedus Aerodynamics
Transcript
The window will appear as follows. Next, find the leading edge surface distance for the flap using the same method as outlined in the main airfoil section. For the flap, the surface distance to the leading edge is 6.8576. Then, as with the main airfoil, create a break at this location and set the number of points for both the top and bottom segment to 101. 180
