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
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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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