Comparing Airfoils

I.S.A. 571

AG35

I.S.A. 571 AG35
Thickness (%) 7.326 8.706
Camber (%) 4.319 4.362
Trailing Edge Angle (%) 18.639 14.975
Lower Surface Flatness 54.334 16.180
Leading Edge Radius (%) 2.148 1.977
Maximum Lift (CL) 1.480 1.091
Maximum Lift Angle-of-Attack (deg) 8.500 6.500
Maximum Lift-to-drag (L/D) 61.436 46.302
Lift at Maximum Lift-to-drag 1.223 0.998
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 5.000