Comparing Airfoils

NACA 64-012A AIRFOIL

AH 85-L-120/17

NACA 64-012A AIRFOIL AH 85-L-120/17
Thickness (%) 11.960 12.091
Camber (%) 0.000 0.000
Trailing Edge Angle (%) 15.240 13.699
Lower Surface Flatness 5.838 5.138
Leading Edge Radius (%) 2.227 1.898
Maximum Lift (CL) 0.852 0.708
Maximum Lift Angle-of-Attack (deg) 14.500 12.000
Maximum Lift-to-drag (L/D) 33.309 27.440
Lift at Maximum Lift-to-drag 0.534 0.446
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.500 4.000