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Preliminary Internal Performance Data for a Variable-Ejector Assembly on the XJ79-GE-1 Turbojet Engine: Afterburning Configurations - IIInternal performance of an XJ79-GE-1 variable ejector was experimentally determined with the primary nozzle in two representative after-burning positions. Jet-thrust and air-handling data were obtained in quiescent air for 4 selected ejector configurations over a wide range of secondary to primary airflow ratios and primary-nozzle pressure ratios. The experimental ejector data are presented in both graphical and tabulated form.
Document ID
20050019281
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Bloomer, Harry E.
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Groesbeck, Donald E.
(National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 22, 2013
Publication Date
July 30, 1957
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-RM-E57F25
Report Number: NACA-RM-E57F25
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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