Comparing Airfoils

NACA M10 AIRFOIL

AG03 (flat aft bottom)

NACA M10 AIRFOIL AG03 (flat aft bottom)
Thickness (%) 6.185 6.237
Camber (%) 1.905 2.020
Trailing Edge Angle (%) 17.238 9.524
Lower Surface Flatness 40.220 30.019
Leading Edge Radius (%) 1.818 1.749
Maximum Lift (CL) 0.810 0.973
Maximum Lift Angle-of-Attack (deg) 12.500 7.000
Maximum Lift-to-drag (L/D) 30.065 47.611
Lift at Maximum Lift-to-drag 0.483 0.973
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.000 7.000