Comparing Airfoils

AG17

AG08

AG17 AG08
Thickness (%) 6.468 5.828
Camber (%) 2.015 1.802
Trailing Edge Angle (%) 6.391 9.434
Lower Surface Flatness 26.078 28.854
Leading Edge Radius (%) 1.749 1.725
Maximum Lift (CL) 0.878 0.817
Maximum Lift Angle-of-Attack (deg) 5.500 5.500
Maximum Lift-to-drag (L/D) 46.949 43.467
Lift at Maximum Lift-to-drag 0.878 0.817
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.500 5.500