Comparing Airfoils

S1012

AH 85-L-120/17

S1012 AH 85-L-120/17
Thickness (%) 12.002 12.091
Camber (%) 0.000 0.000
Trailing Edge Angle (%) 9.216 13.699
Lower Surface Flatness 5.314 5.138
Leading Edge Radius (%) 2.676 1.898
Maximum Lift (CL) 0.963 0.708
Maximum Lift Angle-of-Attack (deg) 15.000 12.000
Maximum Lift-to-drag (L/D) 36.583 27.440
Lift at Maximum Lift-to-drag 0.757 0.446
Angle-of-Attack for Maximum Lift-to-drag (L/D) 7.000 4.000