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Study of cavitating inducer instabilitiesAn analytic and experimental investigation into the causes and mechanisms of cavitating inducer instabilities was conducted. Hydrofoil cascade tests were performed, during which cavity sizes were measured. The measured data were used, along with inducer data and potential flow predictions, to refine an analysis for the prediction of inducer blade suction surface cavitation cavity volume. Cavity volume predictions were incorporated into a linearized system model, and instability predictions for an inducer water test loop were generated. Inducer tests were conducted and instability predictions correlated favorably with measured instability data.
Document ID
19730004572
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Young, W. E.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Murphy, R.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Reddecliff, J. M.
(Pratt and Whitney Aircraft West Palm Beach, FL, United States)
Date Acquired
September 2, 2013
Publication Date
August 31, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-123939
PWA-FR-5131
Accession Number
73N13299
Funding Number(s)
CONTRACT_GRANT: NAS8-27625
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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