Comparing Airfoils

AH 88-K-130/20

AH 79-K-132/20

AH 88-K-130/20 AH 79-K-132/20
Thickness (%) 12.989 13.198
Camber (%) 3.929 3.679
Trailing Edge Angle (%) 9.133 12.663
Lower Surface Flatness 12.560 10.496
Leading Edge Radius (%) 1.922 2.183
Maximum Lift (CL) 1.240 1.151
Maximum Lift Angle-of-Attack (deg) 10.000 11.500
Maximum Lift-to-drag (L/D) 48.839 45.390
Lift at Maximum Lift-to-drag 0.871 0.984
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.000 6.000