Comparing Airfoils

GOE 795 smoothed

GOE 565 AIRFOIL

GOE 795 smoothed GOE 565 AIRFOIL
Thickness (%) 8.019 8.356
Camber (%) 2.427 2.776
Trailing Edge Angle (%) 16.693 10.483
Lower Surface Flatness 19.316 37.036
Leading Edge Radius (%) 1.881 2.328
Maximum Lift (CL) 0.955 1.144
Maximum Lift Angle-of-Attack (deg) 6.000 14.000
Maximum Lift-to-drag (L/D) 70.761 55.958
Lift at Maximum Lift-to-drag 0.853 0.615
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 2.000