Comparing Airfoils

GOE 610-B MOD. AIRFOIL

AH-6-40-7 AIRFOIL

GOE 610-B MOD. AIRFOIL AH-6-40-7 AIRFOIL
Thickness (%) 7.638 6.808
Camber (%) 5.651 5.523
Trailing Edge Angle (%) 24.798 22.022
Lower Surface Flatness 12.024 9.454
Leading Edge Radius (%) 2.113 2.104
Maximum Lift (CL) 1.657 1.749
Maximum Lift Angle-of-Attack (deg) 9.000 9.000
Maximum Lift-to-drag (L/D) 54.709 55.957
Lift at Maximum Lift-to-drag 1.390 1.443
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.500 6.000