Comparing Airfoils

GOE 795 smoothed

GOE 622 AIRFOIL

GOE 795 smoothed GOE 622 AIRFOIL
Thickness (%) 8.019 7.975
Camber (%) 2.427 2.446
Trailing Edge Angle (%) 16.693 15.363
Lower Surface Flatness 19.316 30.395
Leading Edge Radius (%) 1.881 2.138
Maximum Lift (CL) 0.955 1.174
Maximum Lift Angle-of-Attack (deg) 6.000 8.000
Maximum Lift-to-drag (L/D) 70.761 58.441
Lift at Maximum Lift-to-drag 0.853 1.021
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 6.500