On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream / Herbert S. Ribner.

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Bibliographic Details
Main Author:	Ribner, H. S. (Herbert S.), 1913-
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1950.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 2146.
Subjects:	Airplanes > Wings, Swept-back. Aerodynamics, Supersonic. Rolling (Aerodynamics) Trailing edges (Aerodynamics)

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Holdings details from PASCAL Offsite
Call Number:	Y 3.N 21/5:6/2146
Y 3.N 21/5:6/2146	Available Place a Hold