Comparing Airfoils

GOE 610-B MOD. AIRFOIL

GOE 124 (MVA H.4) AIRFOIL

GOE 610-B MOD. AIRFOIL GOE 124 (MVA H.4) AIRFOIL
Thickness (%) 7.638 7.894
Camber (%) 5.651 5.523
Trailing Edge Angle (%) 24.798 16.907
Lower Surface Flatness 12.024 12.274
Leading Edge Radius (%) 2.113 2.374
Maximum Lift (CL) 1.657 1.532
Maximum Lift Angle-of-Attack (deg) 9.000 10.500
Maximum Lift-to-drag (L/D) 54.709 63.804
Lift at Maximum Lift-to-drag 1.390 1.187
Angle-of-Attack for Maximum Lift-to-drag (L/D) 6.500 5.000