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

2007年第1卷第4期

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《能源前沿（英文）》 >> 2007年第1卷第4期 doi: 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

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

发布日期： 2007-12-05

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摘要

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

关键词

aerodynamic ; investigation ; centrifugal ; de-swirling ; circumferent