Comparing Airfoils

GOE 602 MOD. AIRFOIL

AH 79-100 A AIRFOIL

GOE 602 MOD. AIRFOIL AH 79-100 A AIRFOIL
Thickness (%) 9.539 9.969
Camber (%) 3.778 3.644
Trailing Edge Angle (%) 11.762 7.194
Lower Surface Flatness 34.941 16.965
Leading Edge Radius (%) 2.307 2.107
Maximum Lift (CL) 1.380 1.227
Maximum Lift Angle-of-Attack (deg) 7.500 6.500
Maximum Lift-to-drag (L/D) 71.727 73.259
Lift at Maximum Lift-to-drag 1.164 1.040
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.500 4.500