Comparing Airfoils

AG17

AG16

AG17 AG16
Thickness (%) 6.468 7.094
Camber (%) 2.015 1.869
Trailing Edge Angle (%) 6.391 6.607
Lower Surface Flatness 26.078 19.899
Leading Edge Radius (%) 1.749 1.794
Maximum Lift (CL) 0.878 0.920
Maximum Lift Angle-of-Attack (deg) 5.500 6.000
Maximum Lift-to-drag (L/D) 46.949 47.750
Lift at Maximum Lift-to-drag 0.878 0.920
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.500 6.000