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Static performance of an auxiliary inlet ejector nozzle for supersonic-cruise aircraftStatic performance of an auxiliary inlet ejector nozzle for supersonic-cruise aircraft
Document ID
19680026292
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jones, J. R. (NASA Lewis Research Center Cleveland, OH, United States)
Shrewsbury, G. D. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1653
Report Number: NASA-TM-X-1653
Accession Number
68N35764
Funding Number(s)
CONTRACT_GRANT: 126-15-02-10-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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