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Summary of design and blade-element performance data for 12 axial-flow pump rotor configurationsA collection of noncavitating blade-element performance data for 12 axial-flow pump rotor configurations is presented in tabular form. Rotor design philosophy, test apparatus and procedure, and data reduction and evaluation are discussed. A data storage and recall computer program is described. All but one of the rotor configurations considered were composed of double-circular-arc blade sections and were designed for high inlet relative flow angles. Hub-tip radius ranged from 0.40 to 0.90.
Document ID
19730006255
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Miller, M. J.
(Iowa State Univ. of Sci. and Technol. Cleveland, OH, United States)
Okiishi, T. H.
(Iowa State Univ. of Sci. and Technol. Cleveland, OH, United States)
Serovy, G. K.
(Iowa State Univ. of Sci. and Technol.)
Sandercock, D. M.
(NASA Lewis Research Center)
Britsch, W. R.
(NASA Lewis Research Center)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-7074
E-6624
Report Number: NASA-TN-D-7074
Report Number: E-6624
Accession Number
73N14982
Funding Number(s)
PROJECT: RTOP 502-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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