中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Unsteady Rotor-Stator Interaction in High Speed Compressor and Turbine Stages

文献类型:期刊论文

作者I. Trebinjac; D. Charbonnier; F. Leboeuf
刊名JOURNAL OF THERMAL SCIENCE
出版日期2005
卷号14期号:4页码:289,297
关键词Unsteady Aerodynamics Rotor Stator Interaction Deterministic Stress
英文摘要The blade row interaction can alter the time-mean flow and therefore be of interest for aerodynamic design analysis. Whereas results within low subsonic turbomachines are quite numerous in the literature, there have been far fewer works which give results of blade row interaction within high speed cases. Two cases are related in this paper. First, the effects of an incoming wake on the rotor flow field of a transonic compressor are analyzed. The blade row interaction proved to be positive regarding the total pressure ratio, but negative regarding the losses. The second case concerns a transonic turbine. Particular emphasis is placed on the assessment of the deterministic correlations included in the Averaged Passage Equation System.
公开日期2013-03-11
源URL[http://ir.etp.ac.cn/handle/311046/53244]  
专题工程热物理研究所_Journal of Thermal Science
推荐引用方式
GB/T 7714
I. Trebinjac,D. Charbonnier,F. Leboeuf. Unsteady Rotor-Stator Interaction in High Speed Compressor and Turbine Stages[J]. JOURNAL OF THERMAL SCIENCE,2005,14(4):289,297.
APA I. Trebinjac,D. Charbonnier,&F. Leboeuf.(2005).Unsteady Rotor-Stator Interaction in High Speed Compressor and Turbine Stages.JOURNAL OF THERMAL SCIENCE,14(4),289,297.
MLA I. Trebinjac,et al."Unsteady Rotor-Stator Interaction in High Speed Compressor and Turbine Stages".JOURNAL OF THERMAL SCIENCE 14.4(2005):289,297.

入库方式: OAI收割

来源:工程热物理研究所

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