Comparing Airfoils

D.G.A. 1138

AG36

D.G.A. 1138 AG36
Thickness (%) 6.900 8.153
Camber (%) 4.050 4.088
Trailing Edge Angle (%) 28.009 15.259
Lower Surface Flatness 57.304 17.628
Leading Edge Radius (%) 2.041 1.898
Maximum Lift (CL) 1.122 1.027
Maximum Lift Angle-of-Attack (deg) 7.000 5.500
Maximum Lift-to-drag (L/D) 41.617 44.702
Lift at Maximum Lift-to-drag 1.023 1.027
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 5.500