Published June 1992 | Version Published
Discussion Paper Open

The Effect of Inlet Swirl on the Rotordynamic Shroud Forces in a Centrifugal Pump

Abstract

The 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.

Additional Information

The assistance provided by F. Zhuang, A. Bhattacharyya, F. Rahman and Sandor Nagy with the experimental program is greatly appreciated. We would also like to thank NASA George Marshall Space Flight Center for support under Grant NAG8-118.

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Published - ASME_92-GT-126.pdf

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ASME_92-GT-126.pdf

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Identifiers

Eprint ID
28669
Resolver ID
CaltechAUTHORS:20120105-103828941

Funding

NASA
NAG8-118

Dates

Created
2012-01-05
Created from EPrint's datestamp field
Updated
2019-10-03
Created from EPrint's last_modified field

Caltech Custom Metadata

Other Numbering System Name
ASME Papers
Other Numbering System Identifier
92-GT-126