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1954 (2)

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Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10⁶ to 8.0 x 10⁶
Authors: ---
Year: 1954 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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Book
Airfoil section characteristics at high angles of attack
Authors: ---
Year: 1954 Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics,

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