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Relationship between the Flow Blockage of Tip Leakage Vortex and its Evolutionary Procedures inside the Rotor Passage of a Subsonic Axial Compressor

DU Hui YU Xianjun ZHANG Zhibo LIU Baojie

热科学学报(英文版)2013,Vol.22Issue(6):522-531,10.
热科学学报(英文版)2013,Vol.22Issue(6):522-531,10.DOI:10.1007/s11630-013-0658-2

Relationship between the Flow Blockage of Tip Leakage Vortex and its Evolutionary Procedures inside the Rotor Passage of a Subsonic Axial Compressor

Relationship between the Flow Blockage of Tip Leakage Vortex and its Evolutionary Procedures inside the Rotor Passage of a Subsonic Axial Compressor

DU Hui 1YU Xianjun 1ZHANG Zhibo 1LIU Baojie1

作者信息

  • 1. National Key Laboratory of Science & Technology on Aero-Engine Aero-Thermodynamics, School of Energy and Power Engineering, Beihang University, Beijing 100191, China
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摘要

关键词

tip leakage vortex/ flow blockage/ unsteady flow/ axial compressor/ turbomachinery

Key words

tip leakage vortex/ flow blockage/ unsteady flow/ axial compressor/ turbomachinery

引用本文复制引用

DU Hui,YU Xianjun,ZHANG Zhibo,LIU Baojie..Relationship between the Flow Blockage of Tip Leakage Vortex and its Evolutionary Procedures inside the Rotor Passage of a Subsonic Axial Compressor[J].热科学学报(英文版),2013,22(6):522-531,10.

基金项目

This work is funded by the National Natural Science Foundation of China,Grant No.51006007,51136003 and 50976009. ()

热科学学报(英文版)

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