Numerical simulation of the impeller tip clearance effect on centrifugal compressor performance /

This thesis presents the numerical simulation of flow in centrifugal compressors. A three-dimensional Navier-Stokes solver was employed to simulate flow through two centrifugal compressors. The first compressor simulated was the NASA low speed centrifugal compressor (LSCC). The LSCC was selected...

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Bibliographic Details

Main Author:	Hoenninger, Corbett Reed, 1972-
Format:	Thesis eBook
Language:	English
Published:	[Place of publication not identified] : [publisher not identified] ; 2001.
Subjects:	Major aerospace engineering.
Online Access:	Link to OAKTrust copy