Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests /

Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests /

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Bibliographic Details
Main Authors: Holzman, Jon K. (Author), Webb, Lannie D. (Author), Burcham, Frank W. (Author)
Corporate Author: United States. National Aeronautics and Space Administration (sponsoring body.)
Format: Government Document Electronic eBook
Language:English
Published: Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, November 1996.
Series:NASA technical memorandum ; 104326.
Subjects:
Acoustic measurement.
Aircraft noise.
Engine noise.
Exhaust gases.
Jet engines.
Online Access:CONNECT
Description
Item Description:Title from title screen (viewed April 5, 2016).
"November 1996."
"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
Physical Description:1 online resource (iv, 26 pages) : illustrations.
Bibliography:Includes bibliographical references (page 26).

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