Comparing Airfoils

GOE 55 AIRFOIL

AG47ct -02f rot.

GOE 55 AIRFOIL AG47ct -02f rot.
Thickness (%) 6.150 4.983
Camber (%) 2.027 1.302
Trailing Edge Angle (%) 19.297 5.572
Lower Surface Flatness 53.520 30.898
Leading Edge Radius (%) 2.392 1.648
Maximum Lift (CL) 1.042 0.756
Maximum Lift Angle-of-Attack (deg) 15.000 5.500
Maximum Lift-to-drag (L/D) 26.951 43.163
Lift at Maximum Lift-to-drag 0.525 0.756
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.000 5.500