Comparing Airfoils

WORTMANN FX 62-K-131 AIRFOIL

AH 88-K-130/20

WORTMANN FX 62-K-131 AIRFOIL AH 88-K-130/20
Thickness (%) 13.088 12.989
Camber (%) 3.889 3.929
Trailing Edge Angle (%) 2.096 9.133
Lower Surface Flatness 11.792 12.560
Leading Edge Radius (%) 2.007 1.922
Maximum Lift (CL) 1.474 1.240
Maximum Lift Angle-of-Attack (deg) 5.500 10.000
Maximum Lift-to-drag (L/D) 35.227 48.839
Lift at Maximum Lift-to-drag 1.304 0.871
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.000 3.000