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Coolant flow effects on the performance of a conical plug nozzle at Mach numbers from 0 to 2.0Coolant flow effects on performance of conical plug nozzle at Mach numbers from 0 to 2.0
Document ID
19700029435
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chenoweth, F. C. (NASA Lewis Research Center Cleveland, OH, United States)
Jeracki, R. J. (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-2076
E-5552
Report Number: NASA-TM-X-2076
Report Number: E-5552
Accession Number
70N38751
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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