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Preliminary Altitude Performance Data for the J65-B3 Turbojet Engine at Reynolds Number Indices from 0.2 to 0.8Altitude performance characteristics of the J65-B3 turbojet engine and its components were obtained at engine-inlet conditions corresponding to Reynolds number indices from 0.2 to 0.8 over a range of corrected engine speeds from 70 to 110 percent of rated speed. Engine operational limits up to an altitude of 75,000 feet together with ignition and windmilling characteristics were also obtained. The engine and component data are presented both in graphical and in tabulated form. The operational characteristics are presented in graphical form.
Document ID
20090021720
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Braithwaite, W.M. (NASA Lewis Research Center Cleveland, OH, United States)
Greathouse, W.K. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
August 23, 1954
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-RM-SE54H18
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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