Comparing Airfoils

D.G.A. 1138

AG37

D.G.A. 1138 AG37
Thickness (%) 6.900 7.729
Camber (%) 4.050 3.880
Trailing Edge Angle (%) 28.009 17.198
Lower Surface Flatness 57.304 19.849
Leading Edge Radius (%) 2.041 1.878
Maximum Lift (CL) 1.122 1.069
Maximum Lift Angle-of-Attack (deg) 7.000 6.000
Maximum Lift-to-drag (L/D) 41.617 42.503
Lift at Maximum Lift-to-drag 1.023 1.069
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 6.000