Comparing Airfoils

FX60-100 10.0% smoothed

AH 79-100 A AIRFOIL

FX60-100 10.0% smoothed AH 79-100 A AIRFOIL
Thickness (%) 9.946 9.969
Camber (%) 3.537 3.644
Trailing Edge Angle (%) 3.416 7.194
Lower Surface Flatness 15.692 16.965
Leading Edge Radius (%) 2.106 2.107
Maximum Lift (CL) 1.387 1.227
Maximum Lift Angle-of-Attack (deg) 8.500 6.500
Maximum Lift-to-drag (L/D) 51.089 73.259
Lift at Maximum Lift-to-drag 0.959 1.040
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.500 4.500