Comparing Airfoils

GOE 610-B MOD. AIRFOIL

A18 (original)

GOE 610-B MOD. AIRFOIL A18 (original)
Thickness (%) 7.638 7.287
Camber (%) 5.651 5.021
Trailing Edge Angle (%) 24.798 22.552
Lower Surface Flatness 12.024 20.385
Leading Edge Radius (%) 2.113 2.174
Maximum Lift (CL) 1.657 1.298
Maximum Lift Angle-of-Attack (deg) 9.000 6.000
Maximum Lift-to-drag (L/D) 54.709 54.139
Lift at Maximum Lift-to-drag 1.390 1.298
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.500 6.000