Comparing Airfoils

AH 88-K-136/16

AH 79-K-135/20 B

AH 88-K-136/16 AH 79-K-135/20 B
Thickness (%) 13.540 13.486
Camber (%) 3.087 3.052
Trailing Edge Angle (%) 19.630 12.757
Lower Surface Flatness 7.379 8.532
Leading Edge Radius (%) 2.134 2.150
Maximum Lift (CL) 1.049 1.145
Maximum Lift Angle-of-Attack (deg) 14.000 12.500
Maximum Lift-to-drag (L/D) 38.252 38.690
Lift at Maximum Lift-to-drag 0.765 0.711
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 4.000