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The effect of inlet swirl on the rotordynamic shroud forces in a centrifugal pumpThe role played by fluid forces in determining the rotordynamic stability of a centrifugal pump is gaining increasing attention. The present research investigates the contributions to the rotordynamic forces from the discharge-to-suction leakage flows between the front shroud of the rotating impeller and the stationary pump casing. In particular, the dependency of the rotordynamic characteristics of leakage flows on the swirl at the inlet to the leakage path was examined. An inlet guide vane was designed for the experiment so that swirl could be introduced at the leakage flow inlet. The data demonstrates substantial rotordynamic effects and a destabilizing tangential force for small positive whirl ratios; this force decreased with increasing flow rate. The effect of swirl on the rotordynamic forces was found to be destabilizing.
Document ID
19930035363
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ginzburg, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Brennen, C. E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Acosta, A. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Caughey, T. K.
(California Inst. of Technology Pasadena, United States)
Date Acquired
August 15, 2013
Publication Date
June 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ASME PAPER 92-GT-126
Meeting Information
Meeting: ASME, International Gas Turbine and Aeroengine Congress and Exposition
Location: Cologne
Country: Germany
Start Date: June 1, 1992
End Date: June 4, 1992
Sponsors: ASME
Accession Number
93A19360
Funding Number(s)
CONTRACT_GRANT: NAG8-118
Distribution Limits
Public
Copyright
Other

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