Comparing Airfoils

HT22

AG10

HT22 AG10
Thickness (%) 5.077 4.722
Camber (%) 1.069 1.710
Trailing Edge Angle (%) 7.603 12.416
Lower Surface Flatness 24.462 44.647
Leading Edge Radius (%) 1.728 1.708
Maximum Lift (CL) 0.766 0.772
Maximum Lift Angle-of-Attack (deg) 12.500 11.500
Maximum Lift-to-drag (L/D) 37.763 35.304
Lift at Maximum Lift-to-drag 0.648 0.726
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 5.000