Comparing Airfoils

USA 46 AIRFOIL

AG16

USA 46 AIRFOIL AG16
Thickness (%) 6.535 7.094
Camber (%) 2.162 1.869
Trailing Edge Angle (%) 6.366 6.607
Lower Surface Flatness 39.338 19.899
Leading Edge Radius (%) 1.980 1.794
Maximum Lift (CL) 0.920 0.920
Maximum Lift Angle-of-Attack (deg) 6.000 6.000
Maximum Lift-to-drag (L/D) 56.701 47.750
Lift at Maximum Lift-to-drag 0.739 0.920
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.000 6.000