[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:	Aircraft exhaust emissions > United States. Jet engines > United States. F-16 (Jet fighter plane) Aircraft exhaust emissions. Jet engines. Exhaust gases. Mass flow rate. Mach number. Flight tests. Flow characteristics. Pressure measurement. Velocity measurement. Temperature measurement. United States.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:104326
NAS 1.15:104326	Restricted Place a Hold