A theoretical method of analyzing the effects of yaw-damper dynamics on the stability of an aircraft equipped with a second-order yaw damper / Albert A. Schy and Ordway B. Gates, Jr.

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Bibliographic Details
Main Author:	Schy, Albert A.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Gates, Ordway B.
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) ; 2857.
Subjects:	Airplanes > Control. Stability of airplanes, Lateral. Yawing (Aerodynamics) Automatic control.

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Holdings details from PASCAL Offsite
Call Number:	Y 3.N 21/5:6/2857
Y 3.N 21/5:6/2857	Available Place a Hold