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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Front. Energy ›› 2007, Vol. 1 ›› Issue (4) : 435-440. 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

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