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Investigation of a submerged nozzle on a 1/14.2-scale model of the 260-inch solid rocketFlow characteristics about submerged rocket nozzle model immersed in simulated exhaust gas
Document ID
19670017936
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pelouch, J. J., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Salmi, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TM-X-1388
Report Number: NASA-TM-X-1388
Accession Number
67N27265
Funding Number(s)
CONTRACT_GRANT: 728-00-00-01-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUBMERGED BODY
ROCKET NOZZLE
EXHAUST GAS
FLOW CHARACTERISTICS

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