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Experimental investigation of a 10 deg conical turbojet plug nozzle with iris primary and translating shroud at Mach numbers from 0 to 2.0Performance of 10 deg conical turbojet plug nozzle with iris primary and translating shroud for supersonic cruise applications
Document ID
19690004981
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
December 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1709
Report Number: NASA-TM-X-1709
Accession Number
69N14313
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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