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Influence of Tip Clearance on the Flow Field and Aerodynamic Performance of the Centrifugal Impeller 被引量:5
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作者 高丽敏 席光 王尚锦 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2002年第3期139-144,共6页
This paper studies numerically the influence of the tip clearance on the three dimensional viscous flowfield and performance of the NASA Low Speed Centrifugal Compressor (LSCC) impeller with a vaneless diffuser A thre... This paper studies numerically the influence of the tip clearance on the three dimensional viscous flowfield and performance of the NASA Low Speed Centrifugal Compressor (LSCC) impeller with a vaneless diffuser A three dimensional viscous code developed by the authors is applied with several acceleration methods: local time step, multigrid and residual smoothing The computations were performed under several operating conditions with four different tip clearance sizes(0 0%,50%,100% and 200% design t... 展开更多
关键词 nasa lscc centrifugal impeller performance map tip clearance three dimensional viscous flowfield numerical simulation
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