Comparing Airfoils

FX 60-100 (126) AIRFOIL

AH 79-100 A AIRFOIL

FX 60-100 (126) AIRFOIL AH 79-100 A AIRFOIL
Thickness (%) 10.106 9.969
Camber (%) 3.560 3.644
Trailing Edge Angle (%) 4.182 7.194
Lower Surface Flatness 17.084 16.965
Leading Edge Radius (%) 2.283 2.107
Maximum Lift (CL) 1.418 1.227
Maximum Lift Angle-of-Attack (deg) 7.500 6.500
Maximum Lift-to-drag (L/D) 68.584 73.259
Lift at Maximum Lift-to-drag 0.994 1.040
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.000 4.500