[Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests]
By: [Holzman, Jon K.].
Contributors: NASA Dryden Flight Research Center.
Series: NASA technical memorandum -- 104326.
Publisher: NASA Dryden Flight Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: [Edwards, Calif; Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft exhaust emissions -- United States.; Jet engines -- United States.; F-16 (Jet fighter plane); Jet engines; Exhaust gases.; Mass flow rate.; Mach number.; Flight tests.; Flow characteristics.; Pressure measurement.; Velocity measurement.; Temperature measurement.
Notes: Author and title from microfiche header.

Shipping list no.: 98-0799-M.

"Abstract."

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche : negative. (NASA-TM ; 104326).