Comparing Airfoils

NASA/LANGLEY RC08-64C AIRFOIL

NACA 1408

NASA/LANGLEY RC08-64C AIRFOIL NACA 1408
Thickness (%) 8.000 7.968
Camber (%) 1.000 0.997
Trailing Edge Angle (%) 17.558 14.194
Lower Surface Flatness 10.814 14.251
Leading Edge Radius (%) 1.804 2.178
Maximum Lift (CL) 0.711 0.852
Maximum Lift Angle-of-Attack (deg) 12.000 14.000
Maximum Lift-to-drag (L/D) 18.841 36.547
Lift at Maximum Lift-to-drag 0.273 0.465
Angle-of-Attack for Maximum Lift-to-drag (L/D) 1.500 3.000