Comparing Airfoils

US1000ROOT

NACA 63(3)-018

US1000ROOT NACA 63(3)-018
Thickness (%) 18.492 17.985
Camber (%) 0.000 0.000
Trailing Edge Angle (%) 29.951 6.738
Lower Surface Flatness 3.501 3.718
Leading Edge Radius (%) 3.044 3.262
Maximum Lift (CL) 0.929 1.067
Maximum Lift Angle-of-Attack (deg) 13.000 13.000
Maximum Lift-to-drag (L/D) 22.817 28.900
Lift at Maximum Lift-to-drag 0.901 0.795
Angle-of-Attack for Maximum Lift-to-drag (L/D) 10.500 8.000