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Simulation of turbine with bypasses

  • Beihang University
  • China Aviation Powerplant Research Institute

科研成果: 期刊稿件文章同行评审

摘要

In this paper, the three-stage high/low pressure turbines, strut passage after turbines, bypass and mixing section are simulated numerically. Flow field structures and corresponding analyses are presented. The results indicate that simulation of multi-assembly is necessary, which is an efficient way to consider components matching. The results also show that the matching of turbine and strut is not perfect, but the flow direction is still close to axial through it. The mixing process is not intensive in the mixing section, and the loss due to mixing is not serious.

源语言英语
页(从-至)39-41
页数3
期刊Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics
27
1
出版状态已出版 - 1月 2006

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