Comparing Airfoils

I.S.A. 571

AG36

I.S.A. 571 AG36
Thickness (%) 7.326 8.153
Camber (%) 4.319 4.088
Trailing Edge Angle (%) 18.639 15.259
Lower Surface Flatness 54.334 17.628
Leading Edge Radius (%) 2.148 1.898
Maximum Lift (CL) 1.480 1.027
Maximum Lift Angle-of-Attack (deg) 8.500 5.500
Maximum Lift-to-drag (L/D) 61.436 44.702
Lift at Maximum Lift-to-drag 1.223 1.027
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 5.500