中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Three Dimensional Numerical Analysis of Flow within an Isolated Rotor with Stepped Blades

文献类型:期刊论文

作者Shervin Sammak; Masoud Boroom
刊名JOURNAL OF THERMAL SCIENCE
出版日期2012
卷号21页码:420,427
关键词Compressor Performance Efficiency Stable Operational Margin Stepped Airfoil Surge Improvement
英文摘要Every compressor works in a limited operational range. Surge as one of the sources of this limitation has been studied for many years. In this research, an isolated blade row of compressor rotor is numerically modeled and solved. In order to improve operational limit and postpone the surge occurrence, a stepped blade of RAF6E with higher stall angle of attack is used to investigate the near stall flow behavior. In this study, several location of step on blades are tried and the results are compared with the case with no step on blades. It is shown that, as the step moves toward the leading edge of blades, the effect of delay on surge is reduced and even efficiency is also decreased significantly. By moving the step towards the trailing edge, surge is delayed due to the reattachment of flow after the step. Efficiency is also decreased but not in the order of the previous case.
公开日期2013-01-31
源URL[http://ir.etp.ac.cn/handle/311046/51874]  
专题工程热物理研究所_Journal of Thermal Science
推荐引用方式
GB/T 7714
Shervin Sammak,Masoud Boroom. Three Dimensional Numerical Analysis of Flow within an Isolated Rotor with Stepped Blades[J]. JOURNAL OF THERMAL SCIENCE,2012,21:420,427.
APA Shervin Sammak,&Masoud Boroom.(2012).Three Dimensional Numerical Analysis of Flow within an Isolated Rotor with Stepped Blades.JOURNAL OF THERMAL SCIENCE,21,420,427.
MLA Shervin Sammak,et al."Three Dimensional Numerical Analysis of Flow within an Isolated Rotor with Stepped Blades".JOURNAL OF THERMAL SCIENCE 21(2012):420,427.

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来源:工程热物理研究所

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