Volume 19 Issue 4
Aug.  2004
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LI Chuan-peng, HU Jun. Effects of Rotating Inlet Distortion on a 5-Stage HP-Compressor Stability[J]. Journal of Aerospace Power, 2004, 19(4): 433-437.
Citation: LI Chuan-peng, HU Jun. Effects of Rotating Inlet Distortion on a 5-Stage HP-Compressor Stability[J]. Journal of Aerospace Power, 2004, 19(4): 433-437.

Effects of Rotating Inlet Distortion on a 5-Stage HP-Compressor Stability

  • Received Date: 2003-08-25
  • Rev Recd Date: 2003-11-25
  • Publish Date: 2004-08-28
  • The inlet flow rotating distortion effects in a five-stage HP compressor have been investigated experimentally。For co-rotating distortions,the results exhibited significant loss in stability margin and there were two peaks in surge margin degradation corresponding to two distortion rotating frequencies;For counter rotational distortions,the tests showed minimal loss of stability margin,especially in some cases.The range of stable operations was even enlarged.

     

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