Comparing Airfoils

GOE 55 AIRFOIL

AG13

GOE 55 AIRFOIL AG13
Thickness (%) 6.150 5.831
Camber (%) 2.027 1.971
Trailing Edge Angle (%) 19.297 6.130
Lower Surface Flatness 53.520 32.311
Leading Edge Radius (%) 2.392 1.703
Maximum Lift (CL) 1.042 0.861
Maximum Lift Angle-of-Attack (deg) 15.000 5.500
Maximum Lift-to-drag (L/D) 26.951 46.543
Lift at Maximum Lift-to-drag 0.525 0.861
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.000 5.500