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Numerical investigation on effects of bleeding on compressor model

  • Bin Zhao*
  • , Shao Bin Li
  • , Sheng Zhou
  • , Xue Qi Zou
  • , Sheng Qin Huang
  • *Corresponding author for this work
  • Basic Technology Research Center
  • Beihang University
  • China Aviation Powerplant Research Institute

Research output: Contribution to journalArticlepeer-review

Abstract

In order to study the impact of bleeding on compressor performance, this paper sets up a simplified mathematical and physical model, and uses numerical simulation to explore parameters of bleeding rate, bleeding area, the angle and length of bleeding structure in 49 cases. Studies show that due to the effects of the bleeding, the mainstream flow accelerates in the upstream of the bleeding groove, and decelerates in the downstream. There is a certain pattern in the impact of bleeding parameters on mainstream thermal performance. Bleeding rate mainly determines how much the thermodynamic parameters change, and bleeding area mainly affects where the thermodynamic parameters change, while the angle and length of the bleeding structure influence how the internal bleed air flows.

Original languageEnglish
Pages (from-to)620-628
Number of pages9
JournalTuijin Jishu/Journal of Propulsion Technology
Volume34
Issue number5
StatePublished - May 2013

Keywords

  • Bleeding
  • Bleeding area
  • Bleeding rate
  • Bleeding structure
  • Compressor

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