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Experimental heat transfer and flow results from an air-cooled plug nozzle systemWall temperature and heat transfer characteristics of air cooled plug nozzle system for afterburning turbojet engine
Document ID
19700032858
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Clark, J. S. (NASA Lewis Research Center Cleveland, OH, United States)
Graber, E. J. (NASA Lewis Research Center Cleveland, OH, United States)
Straight, D. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-52897
Report Number: NASA-TM-X-52897
Accession Number
70N42174
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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