Comparing Airfoils

FX 73-170 A

AH 95-160

FX 73-170 A AH 95-160
Thickness (%) 17.078 15.971
Camber (%) 5.635 5.495
Trailing Edge Angle (%) 15.597 15.107
Lower Surface Flatness 11.312 12.717
Leading Edge Radius (%) 2.485 3.003
Maximum Lift (CL) 1.665 1.860
Maximum Lift Angle-of-Attack (deg) 12.000 15.000
Maximum Lift-to-drag (L/D) 40.212 36.960
Lift at Maximum Lift-to-drag 0.635 0.639
Angle-of-Attack for Maximum Lift-to-drag (L/D) -0.500 -0.500