Comparing Airfoils

GOE 279 (DAIMLER X) AIRFOIL

A18 (original)

GOE 279 (DAIMLER X) AIRFOIL A18 (original)
Thickness (%) 7.412 7.287
Camber (%) 4.718 5.021
Trailing Edge Angle (%) 18.981 22.552
Lower Surface Flatness 20.924 20.385
Leading Edge Radius (%) 2.151 2.174
Maximum Lift (CL) 1.408 1.298
Maximum Lift Angle-of-Attack (deg) 14.500 6.000
Maximum Lift-to-drag (L/D) 57.154 54.139
Lift at Maximum Lift-to-drag 1.041 1.298
Angle-of-Attack for Maximum Lift-to-drag (L/D) 4.000 6.000