Volume 24 Issue 7
Jul.  2009
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TU Bao-feng, HU Jun, ZHAO Yong. Three-dimensional numerical research on stall inception in axial compressor[J]. Journal of Aerospace Power, 2009, 24(7): 1616-1621.
Citation: TU Bao-feng, HU Jun, ZHAO Yong. Three-dimensional numerical research on stall inception in axial compressor[J]. Journal of Aerospace Power, 2009, 24(7): 1616-1621.

Three-dimensional numerical research on stall inception in axial compressor

  • Received Date: 2008-07-09
  • Rev Recd Date: 2008-09-01
  • Publish Date: 2009-07-28
  • A 3-D dynamic stall inception analysis method was developed based on the 3-D unsteady Euler equations and the 3-D actuator-disk model.The stall inception of the first stage of a high compressor was studied using this method.The compressors were designed using 3-D method,showing that the characteristics of the rotor are different in the radial direction,so three different static-to-total pressure ratios of rotor were studied in this paper,and the effects on the stall inception were investigated.The results show that this method can compute the 3-D stall inception of the axial compressor,the 3-D space configuration of stall cell,and also the effects of 3-D characteristic of rotor on the stability.This method is also able to detect the dangerous section of the compressor which is helpful to study the stability in multi-stage compressors.

     

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