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Analysis of turbine flow field under low Reynolds number condition

  • Lin Yang*
  • , Tao Feng
  • , Zhengping Zou
  • , Wei Li
  • *此作品的通讯作者
  • Beihang University
  • China Aviation Powerplant Research Institute

科研成果: 期刊稿件文章同行评审

摘要

The flow field in turbine was investigated using three-dimensional numerical simulation method. The flow structures in different altitude were compared and analyzed, to show the effect on flow structure and turbine performance with the decrease of Reynolds number. The results indicate that on the condition of high altitude, the Reynolds number is decreased nearly one order, and the blade loading distribution is changed, large separation is found on blade suction surface, and secondary flow and radial mixing effects enhance obviously, so that the performance is changed worse and the efficiency is dropped rapidly. These factors should be paid more attention to the aerodynamic design of turbine under low Reynolds number condition. Moreover the selection of loading distribution form is also an important factor of the design.

源语言英语
页(从-至)1194-1197
页数4
期刊Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics
31
11
出版状态已出版 - 11月 2005

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