Comparing Airfoils

NACA 0012-64

AH 85-L-120/17

NACA 0012-64 AH 85-L-120/17
Thickness (%) 11.957 12.091
Camber (%) 0.000 0.000
Trailing Edge Angle (%) 25.786 13.699
Lower Surface Flatness 6.145 5.138
Leading Edge Radius (%) 2.873 1.898
Maximum Lift (CL) 0.961 0.708
Maximum Lift Angle-of-Attack (deg) 15.000 12.000
Maximum Lift-to-drag (L/D) 31.988 27.440
Lift at Maximum Lift-to-drag 0.588 0.446
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 4.000