Comparing Airfoils

US1000ROOT

S1046 17% (Danny Howell)

US1000ROOT S1046 17% (Danny Howell)
Thickness (%) 18.492 16.989
Camber (%) 0.000 0.000
Trailing Edge Angle (%) 29.951 11.801
Lower Surface Flatness 3.501 4.088
Leading Edge Radius (%) 3.044 3.365
Maximum Lift (CL) 0.929 1.054
Maximum Lift Angle-of-Attack (deg) 13.000 15.000
Maximum Lift-to-drag (L/D) 22.817 34.927
Lift at Maximum Lift-to-drag 0.901 0.644
Angle-of-Attack for Maximum Lift-to-drag (L/D) 10.500 6.000