Comparing Airfoils

AH 93-156

AH 82-150 F

AH 93-156 AH 82-150 F
Thickness (%) 15.663 14.991
Camber (%) 3.737 3.633
Trailing Edge Angle (%) 13.231 12.352
Lower Surface Flatness 7.505 7.815
Leading Edge Radius (%) 2.571 2.118
Maximum Lift (CL) 1.403 1.189
Maximum Lift Angle-of-Attack (deg) 10.500 11.000
Maximum Lift-to-drag (L/D) 44.716 39.119
Lift at Maximum Lift-to-drag 1.111 0.936
Angle-of-Attack for Maximum Lift-to-drag (L/D) 7.000 4.500