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Experimental performance evaluation of an 8.5 inch /21.59 cm/ mean-diameter axial flow turbine at Reynolds numbers from 18,000 to 177,000Effects of Reynolds number change on performance of axial flow turbine working in argon
Document ID
19680009032
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Kofskey, M. G. (NASA Lewis Research Center Cleveland, OH, United States)
Nusbaum, W. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1968
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TN-D-4432
Report Number: NASA-TN-D-4432
Accession Number
68N18501
Funding Number(s)
CONTRACT_GRANT: 120-27-03-13-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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