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Design and testing of a tandem row pump inducerThe design and testing of a tandem row pump inducer having a supercavitating first stage with a 0.60 hub ratio is presented. The second stage tested was a helical impeller with a 0.70 hub ratio. A cubic arc transition was utilized to accomplish the hub change. The first stage had two blades and the free-vortex design approach was empirically modified based on previous experience. The recommended second stage design having four blades and using cambered blade section is presented but the model was not built or tested. The more simple helix was built instead to reduce cost. Data taken included head generation, cavitation observations and unsteady head fluctuations over the 0-100Hz range.
Document ID
19740022808
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Etter, R. J.
(Hydronautics, Inc. Laurel, MD, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1974
Subject Category
Machine Elements And Processes
Report/Patent Number
NASA-CR-120374
TR-7117-1
Report Number: NASA-CR-120374
Report Number: TR-7117-1
Accession Number
74N30921
Funding Number(s)
CONTRACT_GRANT: NAS8-26591
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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