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Performance of an aerodynamically positioned auxiliary inlet ejector nozzle at Mach numbers from 0 to 2.0Performance of aerodynamically positioned auxiliary inlet ejector nozzle at Mach numbers from 0 to 2.0
Document ID
19700018654
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bresnahan, D. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
E-5536
NASA-TM-X-2023
Report Number: E-5536
Report Number: NASA-TM-X-2023
Accession Number
70N27964
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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