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Calculating Leakage Around Turbopump Inducer ShroudsNew mathematical model for leakage flow around shrouded turbopump inducers yields more realistic analyses from which designers determine best geometry for leakage-flow-reinjection ports. Also, designers use calculated velocity profile at inducer leading edge to determine blade-angle distribution of inducer leading edge.
Document ID
19870000199
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Meng, Sen Yih (Rockwell International Corp.)
Sindir, Munir M. (Rockwell International Corp.)
Date Acquired
August 13, 2013
Publication Date
April 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 4
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
MFS-29106
Accession Number
87B10199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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