Evaluation of the effect of a yaw-rate damper on the flying qualities of a light twin-engine airplane

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Created Date
1970
Description

Work performed at Flight Research Center.

N70-32770.

Cover title.

Includes bibliographical references (p. 42).

Creator

Jarvis, Calvin R

Partner
HathiTrust
Contributing Institution
University of Illinois
Publisher
Washington : National Aeronautics and Space Administration : [For sale by the National Technical Information Service, Springfield, Va.]
Subjects
Turbulence
Private flying
Yawing (Aerodynamics)
Airplanes--Handling characteristics
Type
text
Format
Language material
Electronic resource
Language
English
URL
http://catalog.hathitrust.org/Record/011444423
Rights
Public domain. Learn more at http://www.hathitrust.org/access_use
Chicago citation style
Jarvis, Calvin R. Evaluation of the effect of a yaw-rate damper on the flying qualities of a light twin-engine airplane. 1970. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444423. (Accessed April 19, 2024.)
APA citation style
Jarvis, Calvin R, (1970) Evaluation of the effect of a yaw-rate damper on the flying qualities of a light twin-engine airplane. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444423
MLA citation style
Jarvis, Calvin R. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011444423>.
Note: These citations are programmatically generated and may be incomplete.