Comparing Airfoils

GOE 795 smoothed

GOE 564 AIRFOIL

GOE 795 smoothed GOE 564 AIRFOIL
Thickness (%) 8.019 8.188
Camber (%) 2.427 2.667
Trailing Edge Angle (%) 16.693 13.561
Lower Surface Flatness 19.316 37.574
Leading Edge Radius (%) 1.881 2.357
Maximum Lift (CL) 0.955 1.119
Maximum Lift Angle-of-Attack (deg) 6.000 14.000
Maximum Lift-to-drag (L/D) 70.761 64.244
Lift at Maximum Lift-to-drag 0.853 0.989
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 5.500