Comparing Airfoils

S4061-096-84

DAE-51 AIRFOIL

S4061-096-84 DAE-51 AIRFOIL
Thickness (%) 9.615 9.378
Camber (%) 3.900 4.030
Trailing Edge Angle (%) 4.164 12.202
Lower Surface Flatness 26.965 28.779
Leading Edge Radius (%) 2.108 2.014
Maximum Lift (CL) 1.292 1.292
Maximum Lift Angle-of-Attack (deg) 9.500 7.500
Maximum Lift-to-drag (L/D) 59.390 59.508
Lift at Maximum Lift-to-drag 0.951 1.086
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 5.000