Comparing Airfoils

NACA 0012-34

AH 85-L-120/17

NACA 0012-34 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 5.733 5.138
Leading Edge Radius (%) 2.181 1.898
Maximum Lift (CL) 0.768 0.708
Maximum Lift Angle-of-Attack (deg) 13.500 12.000
Maximum Lift-to-drag (L/D) 32.379 27.440
Lift at Maximum Lift-to-drag 0.523 0.446
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.500 4.000