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

doi:10.1007/s11708-007-0063-5

2007, Vol. 1

Issue (4) : 435-440 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

WANG Qikun, CHEN Kangmin

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

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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

Issue Date: 05 December 2007

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]. Front. Energy, 2007, 1(4): 435-440.

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https://academic.hep.com.cn/fie/EN/10.1007/s11708-007-0063-5
https://academic.hep.com.cn/fie/EN/Y2007/V1/I4/435

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