[Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests] [microform] / [Holzman, Jon K.]

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Bibliographic Details
Main Author: Holzman, Jon K.
Corporate Author: NASA Dryden Flight Research Center
Format: Government Document Microfilm Book
Language:English
Published: [Edwards, Calif.] : [Springfield, Va.] : [NASA Dryden Flight Research Center] ; [National Technical Information Service, distributor], [1996]
Series:NASA technical memorandum ; 104326.
Subjects:

MARC

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650 7 |a Jet engines.  |2 nasat. 
650 7 |a Exhaust gases.  |2 nasat. 
650 7 |a Mass flow rate.  |2 nasat. 
650 7 |a Mach number.  |2 nasat. 
650 7 |a Flight tests.  |2 nasat. 
650 7 |a Flow characteristics.  |2 nasat. 
650 7 |a Pressure measurement.  |2 nasat. 
650 7 |a Velocity measurement.  |2 nasat. 
650 7 |a Temperature measurement.  |2 nasat. 
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