Comparing Airfoils

AH 93-K-132/15

AH 79-K-135/20 B

AH 93-K-132/15 AH 79-K-135/20 B
Thickness (%) 13.215 13.486
Camber (%) 3.515 3.052
Trailing Edge Angle (%) 11.991 12.757
Lower Surface Flatness 9.188 8.532
Leading Edge Radius (%) 2.113 2.150
Maximum Lift (CL) 1.119 1.145
Maximum Lift Angle-of-Attack (deg) 9.500 12.500
Maximum Lift-to-drag (L/D) 40.382 38.690
Lift at Maximum Lift-to-drag 0.984 0.711
Angle-of-Attack for Maximum Lift-to-drag (L/D) 8.000 4.000