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Static performance of an auxiliary inlet ejector nozzle using an afterburning turbojet gas generatorPerformance characteristics of auxiliary inlet ejector nozzle configurations for takeoff, transonic acceleration, and supersonic flight conditions with pressure and temperature profiles
Document ID
19700015497
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Burley, R. R. (NASA Lewis Research Center Cleveland, OH, United States)
Mansour, A. H. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1999
E-5459
Report Number: NASA-TM-X-1999
Report Number: E-5459
Accession Number
70N24802
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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