Comparing Airfoils

GOE 55 AIRFOIL

AG10

GOE 55 AIRFOIL AG10
Thickness (%) 6.150 4.722
Camber (%) 2.027 1.710
Trailing Edge Angle (%) 19.297 12.416
Lower Surface Flatness 53.520 44.647
Leading Edge Radius (%) 2.392 1.708
Maximum Lift (CL) 1.042 0.772
Maximum Lift Angle-of-Attack (deg) 15.000 11.500
Maximum Lift-to-drag (L/D) 26.951 35.304
Lift at Maximum Lift-to-drag 0.525 0.726
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.000 5.000