Effect of taper ratio on low-speed static and yawing stability derivatives of 45 degree sweptback wings with aspect ratio of 2.61 / William Letko and John W. Cowan.

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Bibliographic Details
Main Author:	Letko, William
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Cowan, John W.
Other title:	Technical report archive and image library.
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) ; 1671.
Subjects:	Airplanes > Models > Wings. Airplanes > Wings, Swept-back. Stability of airplanes. Yawing (Aerodynamics) Wind tunnel testing.

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Holdings details from PASCAL Offsite
Call Number:	Y 3.N 21/5:6/1671
Y 3.N 21/5:6/1671	Available Place a Hold