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Performance in air of 4 inch /10.16-cm/ mean-diameter single stage axial-flow turbine for Reynolds numbers from 4,900 to 188,000Reynolds number effect on single stage axial flow turbine in air
Document ID
19680006759
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Klassen, H. A. (NASA Lewis Research Center Cleveland, OH, United States)
Wong, R. Y. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1968
Subject Category
Auxiliary Systems
Report/Patent Number
NASA-TN-D-4383
Report Number: NASA-TN-D-4383
Accession Number
68N16228
Funding Number(s)
CONTRACT_GRANT: 128-31-02-25-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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