Comparing Airfoils

MH 22 7.2%

AG16

MH 22 7.2% AG16
Thickness (%) 7.175 7.094
Camber (%) 1.803 1.869
Trailing Edge Angle (%) 6.639 6.607
Lower Surface Flatness 17.212 19.899
Leading Edge Radius (%) 1.671 1.794
Maximum Lift (CL) 0.635 0.920
Maximum Lift Angle-of-Attack (deg) 4.500 6.000
Maximum Lift-to-drag (L/D) 64.099 47.750
Lift at Maximum Lift-to-drag 0.579 0.920
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.000 6.000