Comparing Airfoils

D.G.A. 1138

AG38

D.G.A. 1138 AG38
Thickness (%) 6.900 7.030
Camber (%) 4.050 3.523
Trailing Edge Angle (%) 28.009 19.494
Lower Surface Flatness 57.304 23.367
Leading Edge Radius (%) 2.041 1.813
Maximum Lift (CL) 1.122 0.997
Maximum Lift Angle-of-Attack (deg) 7.000 5.500
Maximum Lift-to-drag (L/D) 41.617 37.955
Lift at Maximum Lift-to-drag 1.023 0.997
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.000 5.500