Comparing Airfoils

US1000ROOT

NASA SC(2)-0518 AIRFOIL

US1000ROOT NASA SC(2)-0518 AIRFOIL
Thickness (%) 18.492 17.980
Camber (%) 0.000 1.462
Trailing Edge Angle (%) 29.951 18.642
Lower Surface Flatness 3.501 4.180
Leading Edge Radius (%) 3.044 4.871
Maximum Lift (CL) 0.929 1.473
Maximum Lift Angle-of-Attack (deg) 13.000 15.000
Maximum Lift-to-drag (L/D) 22.817 40.333
Lift at Maximum Lift-to-drag 0.901 1.241
Angle-of-Attack for Maximum Lift-to-drag (L/D) 10.500 6.500