High-speed wind-tunnel tests of an NACA 0009-64 airfoil having a 33.4-percent-chord flap with an overhang 20.1 percent of the flap chord / David B. Stevenson and Alfred A. Adler.

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Bibliographic Details
Main Author:	Stevenson, David B.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Adler, Alfred A.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 1417.
Subjects:	Aerofoils. Flaps (Airplanes) Wind tunnel testing. Mach number.

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Call Number:	Y 3.N 21/5:6/1417
Y 3.N 21/5:6/1417	Available Place a Hold