Comparing Airfoils

USA 46 AIRFOIL

AG17

USA 46 AIRFOIL AG17
Thickness (%) 6.535 6.468
Camber (%) 2.162 2.015
Trailing Edge Angle (%) 6.366 6.391
Lower Surface Flatness 39.338 26.078
Leading Edge Radius (%) 1.980 1.749
Maximum Lift (CL) 0.920 0.878
Maximum Lift Angle-of-Attack (deg) 6.000 5.500
Maximum Lift-to-drag (L/D) 56.701 46.949
Lift at Maximum Lift-to-drag 0.739 0.878
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.000 5.500