Comparing Airfoils

AG10

AG09

AG10 AG09
Thickness (%) 4.722 4.847
Camber (%) 1.710 1.855
Trailing Edge Angle (%) 12.416 9.026
Lower Surface Flatness 44.647 47.830
Leading Edge Radius (%) 1.708 1.675
Maximum Lift (CL) 0.772 0.743
Maximum Lift Angle-of-Attack (deg) 11.500 5.000
Maximum Lift-to-drag (L/D) 35.304 40.390
Lift at Maximum Lift-to-drag 0.726 0.743
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 5.000