Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests / Jon K. Holzman, Lannie D. Webb, and Frank W. Burcham, Jr.
- Physical Description: 1 online resource (iv, 26 pages) : illustrations.
- Publisher: Edwards, California. : National Aeronautics and Space Administration, Dryden Flight Research Center, November 1996.
Title from title screen (viewed April 5, 2016).
"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
|Bibliography, etc. Note:||
Includes bibliographical references (page 26).
|Funding Information Note:||
Sponsored by the National Aeronautics and Space Administration WU 505-68-10 H-2122
Search for related items by series