Comparing Airfoils

MH 22 7.2%

AG45ct -02f

MH 22 7.2% AG45ct -02f
Thickness (%) 7.175 6.889
Camber (%) 1.803 1.848
Trailing Edge Angle (%) 6.639 7.150
Lower Surface Flatness 17.212 22.411
Leading Edge Radius (%) 1.671 1.802
Maximum Lift (CL) 0.635 0.974
Maximum Lift Angle-of-Attack (deg) 4.500 7.000
Maximum Lift-to-drag (L/D) 64.099 47.183
Lift at Maximum Lift-to-drag 0.579 0.871
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.000 6.000