Comparing Airfoils

GOE 55 AIRFOIL

AG14

GOE 55 AIRFOIL AG14
Thickness (%) 6.150 5.370
Camber (%) 2.027 2.104
Trailing Edge Angle (%) 19.297 5.985
Lower Surface Flatness 53.520 39.632
Leading Edge Radius (%) 2.392 1.678
Maximum Lift (CL) 1.042 0.920
Maximum Lift Angle-of-Attack (deg) 15.000 6.000
Maximum Lift-to-drag (L/D) 26.951 48.257
Lift at Maximum Lift-to-drag 0.525 0.920
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.000 6.000