Comparing Airfoils

GOE 124 (MVA H.4) AIRFOIL

A18 (original)

GOE 124 (MVA H.4) AIRFOIL A18 (original)
Thickness (%) 7.894 7.287
Camber (%) 5.523 5.021
Trailing Edge Angle (%) 16.907 22.552
Lower Surface Flatness 12.274 20.385
Leading Edge Radius (%) 2.374 2.174
Maximum Lift (CL) 1.532 1.298
Maximum Lift Angle-of-Attack (deg) 10.500 6.000
Maximum Lift-to-drag (L/D) 63.804 54.139
Lift at Maximum Lift-to-drag 1.187 1.298
Angle-of-Attack for Maximum Lift-to-drag (L/D) 5.000 6.000