Comparing Airfoils

AH 82-150 F

AH 82-150 A

AH 82-150 F AH 82-150 A
Thickness (%) 14.991 14.995
Camber (%) 3.633 3.278
Trailing Edge Angle (%) 12.352 10.121
Lower Surface Flatness 7.815 7.777
Leading Edge Radius (%) 2.118 2.244
Maximum Lift (CL) 1.189 1.265
Maximum Lift Angle-of-Attack (deg) 11.000 12.000
Maximum Lift-to-drag (L/D) 39.119 45.550
Lift at Maximum Lift-to-drag 0.936 0.929
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.500 4.500