Comparing Airfoils

US1000ROOT

NACA 0018

US1000ROOT NACA 0018
Thickness (%) 18.492 17.931
Camber (%) 0.000 0.000
Trailing Edge Angle (%) 29.951 31.106
Lower Surface Flatness 3.501 4.409
Leading Edge Radius (%) 3.044 4.839
Maximum Lift (CL) 0.929 1.077
Maximum Lift Angle-of-Attack (deg) 13.000 15.000
Maximum Lift-to-drag (L/D) 22.817 34.864
Lift at Maximum Lift-to-drag 0.901 0.686
Angle-of-Attack for Maximum Lift-to-drag (L/D) 10.500 5.500