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Experimental investigation of a 10 deg conical turbojet plug nozzle with translating primary and secondary shrouds at Mach numbers from 0 to 2.0Static tests of nozzle efficiency and pumping characteristics of conical turbojet plug nozzle with translating primary and secondary shrouds at Mach 0 to 2.0
Document ID
19690012286
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
April 1, 1969
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1777
Report Number: NASA-TM-X-1777
Accession Number
69N21648
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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