Effect of various parameters including Mach number on the single-degree-of-freedom flutter of a control surface in potential flow / Harry L. Runyan.

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Bibliographic Details
Main Author:	Runyan, Harry L.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1951.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 2551.
Subjects:	Airplanes > Control surfaces. Flutter (Aerodynamics) Vibration (Aeronautics)

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Call Number:	Y 3.N 21/5:6/2551
Y 3.N 21/5:6/2551	Available Place a Hold