Comparing Airfoils

AG10

AG08

AG10 AG08
Thickness (%) 4.722 5.828
Camber (%) 1.710 1.802
Trailing Edge Angle (%) 12.416 9.434
Lower Surface Flatness 44.647 28.854
Leading Edge Radius (%) 1.708 1.725
Maximum Lift (CL) 0.772 0.817
Maximum Lift Angle-of-Attack (deg) 11.500 5.500
Maximum Lift-to-drag (L/D) 35.304 43.467
Lift at Maximum Lift-to-drag 0.726 0.817
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 5.500