Comparing Airfoils

HQ 3.5/10 AIRFOIL

AH 79-100 A AIRFOIL

HQ 3.5/10 AIRFOIL AH 79-100 A AIRFOIL
Thickness (%) 9.960 9.969
Camber (%) 3.497 3.644
Trailing Edge Angle (%) 7.401 7.194
Lower Surface Flatness 22.913 16.965
Leading Edge Radius (%) 2.034 2.107
Maximum Lift (CL) 1.336 1.227
Maximum Lift Angle-of-Attack (deg) 7.000 6.500
Maximum Lift-to-drag (L/D) 70.130 73.259
Lift at Maximum Lift-to-drag 0.886 1.040
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.000 4.500