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Effects of Blade Back Sweep Angle on the Performance and Flow Field in a Centrifugal Compressor

블레이드 후향각이 원심압축기의 성능과 유동에 미치는 영향

  • 정요한 (포항공과대학교 기계공학과 대학원) ;
  • 백제현 (포항공과대학교 기계공학과) ;
  • 박준영 (한국기계연구원) ;
  • 최민석 (명지대학교 기계공학과)
  • Received : 2012.10.28
  • Accepted : 2013.03.21
  • Published : 2013.04.01

Abstract

This paper presents a numerical investigation of the influence of the blade back sweep angle on the performance and flow characteristics in a centrifugal compressor with a vaneless diffuser. Five impellers with different back sweep angles were tested in the flow simulations. It was found that a low back sweep angle could improve the total-to-total pressure ratio and the work coefficient over whole operating ranges. However, the flow field in an impeller with a low back sweep angle produced a more non-uniform velocity distribution at the impeller exit because the wake region was significantly increased. As a consequence, the impeller with a low back sweep angle caused a low diffuser performance.

Keywords

References

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