Comparing Airfoils

N-9

AG37

N-9 AG37
Thickness (%) 8.428 7.729
Camber (%) 4.216 3.880
Trailing Edge Angle (%) 18.356 17.198
Lower Surface Flatness 36.354 19.849
Leading Edge Radius (%) 2.337 1.878
Maximum Lift (CL) 1.183 1.069
Maximum Lift Angle-of-Attack (deg) 7.000 6.000
Maximum Lift-to-drag (L/D) 58.690 42.503
Lift at Maximum Lift-to-drag 1.106 1.069
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.500 6.000