Comparing Airfoils

FX 60-160 AIRFOIL

AH 82-150 A

FX 60-160 AIRFOIL AH 82-150 A
Thickness (%) 15.530 14.995
Camber (%) 3.073 3.278
Trailing Edge Angle (%) 14.110 10.121
Lower Surface Flatness 8.117 7.777
Leading Edge Radius (%) 2.801 2.244
Maximum Lift (CL) 1.442 1.265
Maximum Lift Angle-of-Attack (deg) 15.000 12.000
Maximum Lift-to-drag (L/D) 63.806 45.550
Lift at Maximum Lift-to-drag 1.122 0.929
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.500 4.500