Comparing Airfoils

GOE 622 AIRFOIL

GOE 565 AIRFOIL

GOE 622 AIRFOIL GOE 565 AIRFOIL
Thickness (%) 7.975 8.356
Camber (%) 2.446 2.776
Trailing Edge Angle (%) 15.363 10.483
Lower Surface Flatness 30.395 37.036
Leading Edge Radius (%) 2.138 2.328
Maximum Lift (CL) 1.174 1.144
Maximum Lift Angle-of-Attack (deg) 8.000 14.000
Maximum Lift-to-drag (L/D) 58.441 55.958
Lift at Maximum Lift-to-drag 1.021 0.615
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.500 2.000