Comparing Airfoils

MH 22 7.2%

AG44ct -02f

MH 22 7.2% AG44ct -02f
Thickness (%) 7.175 7.288
Camber (%) 1.803 1.941
Trailing Edge Angle (%) 6.639 8.068
Lower Surface Flatness 17.212 20.564
Leading Edge Radius (%) 1.671 1.840
Maximum Lift (CL) 0.635 0.996
Maximum Lift Angle-of-Attack (deg) 4.500 7.000
Maximum Lift-to-drag (L/D) 64.099 48.412
Lift at Maximum Lift-to-drag 0.579 0.893
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.000 6.000