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Performance of convergent and plug nozzles at Mach numbers from 0 to 1.97Boattail and plug area variation effect on convergent and plug nozzle efficiency at Mach 0 to 1.97
Document ID
19700033122
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Harrington, D. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-2112
Report Number: NASA-TM-X-2112
Accession Number
70N42438
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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