Comparing Airfoils

S4061-096-84

AH 79-100 A AIRFOIL

S4061-096-84 AH 79-100 A AIRFOIL
Thickness (%) 9.615 9.969
Camber (%) 3.900 3.644
Trailing Edge Angle (%) 4.164 7.194
Lower Surface Flatness 26.965 16.965
Leading Edge Radius (%) 2.108 2.107
Maximum Lift (CL) 1.292 1.227
Maximum Lift Angle-of-Attack (deg) 9.500 6.500
Maximum Lift-to-drag (L/D) 59.390 73.259
Lift at Maximum Lift-to-drag 0.951 1.040
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 4.500