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Blade-element performance of two-stage axial-flow pump with tandem-row inlet stageBlade element performance of two-stage axial-flow pump with tandem-row inlet stage
Document ID
19670016515
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Crouse, J. E. (NASA Lewis Research Center Cleveland, OH, United States)
Sandercock, D. M. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1967
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-TN-D-3962
Report Number: NASA-TN-D-3962
Accession Number
67N25844
Funding Number(s)
CONTRACT_GRANT: 128-31-06-28-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
INLET
ROTOR BLADE
AXIAL FLOW
PUMP

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