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Pump CFD code validation testsPump CFD code validation tests were accomplished by obtaining nonintrusive flow characteristic data at key locations in generic current liquid rocket engine turbopump configurations. Data were obtained with a laser two-focus (L2F) velocimeter at scaled design flow. Three components were surveyed: a 1970's-designed impeller, a 1990's-designed impeller, and a four-bladed unshrouded inducer. Two-dimensional velocities were measured upstream and downstream of the two impellers. Three-dimensional velocities were measured upstream, downstream, and within the blade row of the unshrouded inducer.
Document ID
19940022094
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Brozowski, L. A.
(Rockwell International Corp. Canoga Park, CA, United States)
Date Acquired
September 6, 2013
Publication Date
December 15, 1993
Subject Category
Mechanical Engineering
Report/Patent Number
RI/RD-93-195
NASA-CR-193939
NAS 1.26:193939
Report Number: RI/RD-93-195
Report Number: NASA-CR-193939
Report Number: NAS 1.26:193939
Accession Number
94N26597
Funding Number(s)
CONTRACT_GRANT: NAS8-38864
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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