Comparing Airfoils

AG11

AG08

AG11 AG08
Thickness (%) 5.811 5.828
Camber (%) 2.287 1.802
Trailing Edge Angle (%) 11.524 9.434
Lower Surface Flatness 54.757 28.854
Leading Edge Radius (%) 1.791 1.725
Maximum Lift (CL) 1.016 0.817
Maximum Lift Angle-of-Attack (deg) 7.000 5.500
Maximum Lift-to-drag (L/D) 44.617 43.467
Lift at Maximum Lift-to-drag 0.962 0.817
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.500 5.500