Comparing Airfoils

AG17

AG11

AG17 AG11
Thickness (%) 6.468 5.811
Camber (%) 2.015 2.287
Trailing Edge Angle (%) 6.391 11.524
Lower Surface Flatness 26.078 54.757
Leading Edge Radius (%) 1.749 1.791
Maximum Lift (CL) 0.878 1.016
Maximum Lift Angle-of-Attack (deg) 5.500 7.000
Maximum Lift-to-drag (L/D) 46.949 44.617
Lift at Maximum Lift-to-drag 0.878 0.962
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.500 6.500