Determination of indicial lift and moment of a two-dimensional ptiching airfoil at subsonic Mach numbers from oscillatory coefficients with numerical calculations for a Mach number of 0.7 / Bernard Mazelsky.

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Bibliographic Details
Main Author:	Mazelsky, Bernard
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 2613.
Subjects:	Airplanes > Wings. Aerofoils. Gust loads. Vibration (Aeronautics) Flutter (Aerodynamics) Mathematical analysis.

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Call Number:	Y 3.N 21/5:6/2613
Y 3.N 21/5:6/2613	Available Place a Hold