Comparing Airfoils

N-9

AG35

N-9 AG35
Thickness (%) 8.428 8.706
Camber (%) 4.216 4.362
Trailing Edge Angle (%) 18.356 14.975
Lower Surface Flatness 36.354 16.180
Leading Edge Radius (%) 2.337 1.977
Maximum Lift (CL) 1.183 1.091
Maximum Lift Angle-of-Attack (deg) 7.000 6.500
Maximum Lift-to-drag (L/D) 58.690 46.302
Lift at Maximum Lift-to-drag 1.106 0.998
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.500 5.000