Effect of taper ratio on low-speed static and yawing stability derivatives of 45 degree sweptback wings with aspect ratio of 2.61 /

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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Call Number: Y 3.N 21/5:6/1671
Y 3.N 21/5:6/1671 Available Place a Hold

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