Effect of chordwise location of maximum thickness on the supersonic wave drag of sweptback wings / Kenneth Margolis.

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Bibliographic Details
Main Author:	Margolis, Kenneth
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 1543.
Subjects:	Airplanes > Wings, Swept-back. Drag (Aerodynamics) Aerodynamics, Supersonic.

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Call Number:	Y 3.N 21/5:6/1543
Y 3.N 21/5:6/1543	Available Place a Hold