Comparing Airfoils

US1000ROOT

NACA 63(3)-218

US1000ROOT NACA 63(3)-218
Thickness (%) 18.492 17.963
Camber (%) 0.000 1.106
Trailing Edge Angle (%) 29.951 7.954
Lower Surface Flatness 3.501 4.689
Leading Edge Radius (%) 3.044 3.484
Maximum Lift (CL) 0.929 1.256
Maximum Lift Angle-of-Attack (deg) 13.000 12.500
Maximum Lift-to-drag (L/D) 22.817 36.367
Lift at Maximum Lift-to-drag 0.901 0.906
Angle-of-Attack for Maximum Lift-to-drag (L/D) 10.500 7.000