High-speed subsonic characteristics of 16 NACA 6-series airfoil sections

Milton D. Van Dyke
naca-tn-2670
Mar 1952


A wind-tunnel investigation has been conducted to determine the high-speed subsonic aerodynamic characteristics of NACA 62-, 64-, 65-, and 66-series airfoil sections having thickness ratios of 6, 8, 10, and 12 percent and an ideal lift coefficient of 0.2 with the uniform-load type (a = 1.0) of mean camber line.

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http://naca.central.cranfield.ac.uk/reports/1952/naca-tn-2670.pdf