Comparing Airfoils

GOE 55 AIRFOIL

AG09

GOE 55 AIRFOIL AG09
Thickness (%) 6.150 4.847
Camber (%) 2.027 1.855
Trailing Edge Angle (%) 19.297 9.026
Lower Surface Flatness 53.520 47.830
Leading Edge Radius (%) 2.392 1.675
Maximum Lift (CL) 1.042 0.743
Maximum Lift Angle-of-Attack (deg) 15.000 5.000
Maximum Lift-to-drag (L/D) 26.951 40.390
Lift at Maximum Lift-to-drag 0.525 0.743
Angle-of-Attack for Maximum Lift-to-drag (L/D) 3.000 5.000