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Effect of exit area variation on the performance of an auxiliary inlet ejector nozzle at Mach numbers from 0 to 1.27Auxiliary inlet ejector nozzle designed for supersonic cruise aircraft
Document ID
19710009388
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Blaha, B. J. (NASA Lewis Research Center Cleveland, OH, United States)
Johns, A. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-2182
E-5945
Report Number: NASA-TM-X-2182
Report Number: E-5945
Accession Number
71N18863
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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