Comparing Airfoils

GOE 622 AIRFOIL

GOE 564 AIRFOIL

GOE 622 AIRFOIL GOE 564 AIRFOIL
Thickness (%) 7.975 8.188
Camber (%) 2.446 2.667
Trailing Edge Angle (%) 15.363 13.561
Lower Surface Flatness 30.395 37.574
Leading Edge Radius (%) 2.138 2.357
Maximum Lift (CL) 1.174 1.119
Maximum Lift Angle-of-Attack (deg) 8.000 14.000
Maximum Lift-to-drag (L/D) 58.441 64.244
Lift at Maximum Lift-to-drag 1.021 0.989
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.500 5.500