Low-speed characteristics of four cambered, 10-percent-thick NACA airfoil sections

George B. McCullough, William M. Haire
Aug 1950

A two-dimensional low-speed investigation was made of four thin, cambered airfoil sections. The airfoil sections were the NACA 64A310, a = 1.0; the 64A810, a = 0.8 (modified); and the NACA 0010 cambered to the same two mean lines.

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