Comparing Airfoils

MH 22 7.2%

AG455ct -02f rot.

MH 22 7.2% AG455ct -02f rot.
Thickness (%) 7.175 6.457
Camber (%) 1.803 1.831
Trailing Edge Angle (%) 6.639 6.836
Lower Surface Flatness 17.212 25.744
Leading Edge Radius (%) 1.671 1.778
Maximum Lift (CL) 0.635 0.975
Maximum Lift Angle-of-Attack (deg) 4.500 7.000
Maximum Lift-to-drag (L/D) 64.099 46.492
Lift at Maximum Lift-to-drag 0.579 0.975
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.000 7.000