Comparing Airfoils

D.G.A. 1138

AG35

D.G.A. 1138 AG35
Thickness (%) 6.900 8.706
Camber (%) 4.050 4.362
Trailing Edge Angle (%) 28.009 14.975
Lower Surface Flatness 57.304 16.180
Leading Edge Radius (%) 2.041 1.977
Maximum Lift (CL) 1.122 1.091
Maximum Lift Angle-of-Attack (deg) 7.000 6.500
Maximum Lift-to-drag (L/D) 41.617 46.302
Lift at Maximum Lift-to-drag 1.023 0.998
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 5.000