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Flow and wall-temperature sensitivity in parallel passages for large inlet to exit density ratios in subsonic flowAnalytical investigation of flow and wall temperature sensitivity in heated passages for large inlet to exit density ratios in subsonic flow of nuclear rocket
Document ID
19680018899
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Reshotko, M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1968
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-4649
Report Number: NASA-TN-D-4649
Accession Number
68N28371
Funding Number(s)
CONTRACT_GRANT: 120-27-04-56-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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