Comparing Airfoils

US1000ROOT

S1016

US1000ROOT S1016
Thickness (%) 18.492 17.480
Camber (%) 0.000 0.000
Trailing Edge Angle (%) 29.951 11.599
Lower Surface Flatness 3.501 3.627
Leading Edge Radius (%) 3.044 3.539
Maximum Lift (CL) 0.929 1.119
Maximum Lift Angle-of-Attack (deg) 13.000 11.500
Maximum Lift-to-drag (L/D) 22.817 33.255
Lift at Maximum Lift-to-drag 0.901 0.981
Angle-of-Attack for Maximum Lift-to-drag (L/D) 10.500 9.500