Comparing Airfoils

NASA/LANGLEY RC08-64C AIRFOIL

M6 (65%)

NASA/LANGLEY RC08-64C AIRFOIL M6 (65%)
Thickness (%) 8.000 7.806
Camber (%) 1.000 1.437
Trailing Edge Angle (%) 17.558 13.930
Lower Surface Flatness 10.814 12.291
Leading Edge Radius (%) 1.804 1.826
Maximum Lift (CL) 0.711 0.770
Maximum Lift Angle-of-Attack (deg) 12.000 12.500
Maximum Lift-to-drag (L/D) 18.841 36.924
Lift at Maximum Lift-to-drag 0.273 0.562
Angle-of-Attack for Maximum Lift-to-drag (L/D) 1.500 4.500