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입구 비 균일 유동이 원심압축기의 정상 및 비정상 성능에 미치는 영향

The Effect of Inlet Distorted Flow on Steady and Unsteady Performance of a Centrifugal Compressor

  • 강신형 (서울대학교 기계항공공학부) ;
  • 박재형 (서울대학교 대학원 기계항공공학부)
  • 발행 : 2005.09.01

초록

Effects of inlet distorted flow on performance, stall and surge are experimentally investigated for a high-speed centrifugal compressor. Tested results for the distorted inlet flow cases are compared with the result of the undistorted one. The performance of compressor is slightly deteriorated due to the inlet distortion. The inlet distortion does not affect the number of stall cell and the propagation velocity. It also does not change stall inception flow rate. However, as the distortion increases, stall starts at the higher flow rate for low speed and at the lower flow rate for high speed. For 50,000 rpm stall occurrs as the flow rate decreases, however disappears fur the smaller flow rate. This is due to the interaction of surge and stall. After the stall and surge interact, the number of stall cell decreases.

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참고문헌

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