Comparing Airfoils

AH 88-K-130/20

AH 63-K-127/24

AH 88-K-130/20 AH 63-K-127/24
Thickness (%) 12.989 12.704
Camber (%) 3.929 3.761
Trailing Edge Angle (%) 9.133 11.288
Lower Surface Flatness 12.560 12.628
Leading Edge Radius (%) 1.922 1.990
Maximum Lift (CL) 1.240 1.198
Maximum Lift Angle-of-Attack (deg) 10.000 10.500
Maximum Lift-to-drag (L/D) 48.839 47.838
Lift at Maximum Lift-to-drag 0.871 1.036
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.000 5.500