Comparing Airfoils

NASA SC(2)-0012 AIRFOIL

AH 85-L-120/17

NASA SC(2)-0012 AIRFOIL AH 85-L-120/17
Thickness (%) 12.000 12.091
Camber (%) 0.000 0.000
Trailing Edge Angle (%) 27.284 13.699
Lower Surface Flatness 5.608 5.138
Leading Edge Radius (%) 2.790 1.898
Maximum Lift (CL) 0.970 0.708
Maximum Lift Angle-of-Attack (deg) 15.000 12.000
Maximum Lift-to-drag (L/D) 24.003 27.440
Lift at Maximum Lift-to-drag 0.659 0.446
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.500 4.000