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Stalled-Flow and Head-Loss Model for Diffuser PumpsModeling procedure approximates inlet transition zone (blade leading edge to blade throat) of diffuser pump as two-dimensional cascade, properties of which are well known. Model applied to stators as well as rotors. Procedure much faster than previous methods.
Document ID
19830000673
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Meng, S. Y.
(Rockwell International Corp.)
Date Acquired
August 11, 2013
Publication Date
November 1, 1984
Publication Information
Publication: NASA Tech Briefs
Volume: 8
Issue: 2
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
MFS-19748
Accession Number
83B10673
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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