Method of determining reduction in elevator effectiveness when engine is mounted on aft fuselage of aircraft /
James R. Atchison.

Description

Main Author

Atchison, James R.

Related Names

Air Force Flight Dynamics Laboratory (U.S.)
United States. Air Force.
United States. Air Force.

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961.

Subjects

Airplanes > Airplanes / Fuselage.
Airplanes > Airplanes / Turbojet engines > Airplanes / Turbojet engines / Control systems.

Note

"The report was initiated by the Stability and Control Branch, Flight Dynamics Divisoin, Directorate of Defense and Transport Systems Engineering, Aeronautical Systems Division, under System 659A."
"The courtesy of the Ronald Press Company and the McGraw-Hill Book Company, Inc., in granting permission to use their material in this technical report is gratefully acknowledged."
"July 1961."

Physical Description

vi, 11 pages : illustrations, figures, tables ; 28 cm.

Locate a Print Version

Find in a library

Viewability