Comparing Airfoils

NACA 2424

FX 77-W-270S

NACA 2424 FX 77-W-270S
Thickness (%) 23.878 27.009
Camber (%) 1.993 4.306
Trailing Edge Angle (%) 35.712 54.656
Lower Surface Flatness 4.104 3.642
Leading Edge Radius (%) 7.542 6.132
Maximum Lift (CL) 1.580 1.265
Maximum Lift Angle-of-Attack (deg) 15.000 15.000
Maximum Lift-to-drag (L/D) 36.967 13.056
Lift at Maximum Lift-to-drag 0.949 1.265
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.500 15.000