Comparing Airfoils

GOE 122 (MVA H.2) AIRFOIL

AG38

GOE 122 (MVA H.2) AIRFOIL AG38
Thickness (%) 7.298 7.030
Camber (%) 4.053 3.523
Trailing Edge Angle (%) 13.444 19.494
Lower Surface Flatness 30.736 23.367
Leading Edge Radius (%) 2.033 1.813
Maximum Lift (CL) 1.180 0.997
Maximum Lift Angle-of-Attack (deg) 14.000 5.500
Maximum Lift-to-drag (L/D) 53.711 37.955
Lift at Maximum Lift-to-drag 0.675 0.997
Angle-of-Attack for Maximum Lift-to-drag (L/D) 2.500 5.500