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Numerical Simulation of Rotating Stall in a Centrifugal Compressor with Vaned Diffuser

Weiguang Huang Shaojuan Geng Junqiang Zhu Hongwu Zhang

热科学学报(英文版)2007,Vol.16Issue(2):115-120,6.
热科学学报(英文版)2007,Vol.16Issue(2):115-120,6.

Numerical Simulation of Rotating Stall in a Centrifugal Compressor with Vaned Diffuser

Numerical Simulation of Rotating Stall in a Centrifugal Compressor with Vaned Diffuser

Weiguang Huang 1Shaojuan Geng 1Junqiang Zhu 2Hongwu Zhang1

作者信息

  • 1. Institute of Engineering Thermophysics, Chinese Academy of Sciences, P.O. Box 2706, Beijing 100080, China
  • 2. Graduate School of the Chinese Academy of Sciences
  • 折叠

摘要

Abstract

This paper reports a numerical study on the process from normal operating conditions to rotating stall in a centrifugal compressor with vaned diffuser. The purpose is to better understand the flow characteristics near stall point under the interactions between centrifugal impeller and vaned diffuser. Numerical results show that under certain conditions just preceding stall point the tip leakage vortex begins to fluctuate at roughly half of the blade passing frequency. This phenomenon is similar to rotating instability in axial compressors. With the flow rate reduced further the impeller stalls and five stall cells propagating at a frequency of 85 percent of impeller rotation speed are found.

关键词

centrifugal compressor/rotating stall/tip leakage flow/unsteady

Key words

centrifugal compressor/rotating stall/tip leakage flow/unsteady

分类

数理科学

引用本文复制引用

Weiguang Huang,Shaojuan Geng,Junqiang Zhu,Hongwu Zhang..Numerical Simulation of Rotating Stall in a Centrifugal Compressor with Vaned Diffuser[J].热科学学报(英文版),2007,16(2):115-120,6.

基金项目

This work was supported by National Natural Science Forndation of China with project No.50276059. ()

热科学学报(英文版)

OAEISCI

1003-2169

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