Comparing Airfoils

AG09

AG08

AG09 AG08
Thickness (%) 4.847 5.828
Camber (%) 1.855 1.802
Trailing Edge Angle (%) 9.026 9.434
Lower Surface Flatness 47.830 28.854
Leading Edge Radius (%) 1.675 1.725
Maximum Lift (CL) 0.743 0.817
Maximum Lift Angle-of-Attack (deg) 5.000 5.500
Maximum Lift-to-drag (L/D) 40.390 43.467
Lift at Maximum Lift-to-drag 0.743 0.817
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 5.500