Frontiers in Energy >

2007 , Vol. 1 >Issue 4: 435 - 440

DOI: https://doi.org/10.1007/s11708-007-0063-5

Numerical investigation of aerodynamic performance influenced by circumferentially pre-swirling coming flow on the crossover and de-swirling cascade of a multistage centrifugal compressor

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  • College of Power Engineering, University of Shanghai for Science and Technology, Shanghai 200093, China;

Published date: 05 Dec 2007

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Abstract

Numerical investigation is implemented on aerodynamic performance inside the crossover and de-swirling cascade of a multistage centrifugal compressor. The emphasis is put on the aerodynamic performance influenced by the circumferent

Cite this article

WANG Qikun, CHEN Kangmin . Numerical investigation of aerodynamic performance influenced by circumferentially pre-swirling coming flow on the crossover and de-swirling cascade of a multistage centrifugal compressor[J]. Frontiers in Energy, 2007 , 1(4) : 435 -440 . DOI: 10.1007/s11708-007-0063-5

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