中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Flowfield and Heat Transfer past an Unshrouded Gas Turbine Blade Tip with Different Shapes

文献类型:期刊论文

作者Liu, Jian-Jun; Li, Peng; Zhang, Chao; An, Bai-Tao
刊名JOURNAL OF THERMAL SCIENCE
出版日期2013-04-01
卷号22期号:2页码:128-134
关键词Turbine Rotor Blade Squealer Blade Tip Tip Leakage Flow Aerodynamic Loss Heat Transfer
英文摘要This paper describes the numerical investigations of flow and heat transfer in an unshrouded turbine rotor blade of a heavy duty gas turbine with four tip configurations. By comparing the calculated contours of heat transfer coefficients on the flat tip of the BP turbine rotor blade in the GE-E-3 aircraft engine with the corresponding experimental data, the kappa-omega turbulence model was chosen for the present numerical simulations. The inlet and outlet boundary conditions for the turbine rotor blade are specified as the real gas turbine, which were obtained from the 3D full stage simulations. The rotor blade and the hub endwall are rotary and the casing is stationary. The influences of tip configurations on the tip leakage flow and blade tip heat transfer were discussed. It's showed that the different tip configurations changed the leakage flow patterns and the pressure distributions on the suction surface near the blade tip. Compared with the flat tip, the total pressure loss caused by the leakage flow was decreased for the full squealer tip and pressure side squealer tip, while increased for the suction side squealer tip. The suction side squealer tip results in the lowest averaged heat transfer coefficient on the blade tip compared to the other tip configurations.
WOS标题词Science & Technology ; Physical Sciences ; Technology
类目[WOS]Thermodynamics ; Engineering, Mechanical
研究领域[WOS]Thermodynamics ; Engineering
收录类别SCI
语种英语
WOS记录号WOS:000315936000006
公开日期2015-12-22
源URL[http://ir.etp.ac.cn/handle/311046/98875]  
专题工程热物理研究所_中国科学院工程热物理所(论文库)_期刊论文(SCI)
作者单位Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China
推荐引用方式
GB/T 7714
Liu, Jian-Jun,Li, Peng,Zhang, Chao,et al. Flowfield and Heat Transfer past an Unshrouded Gas Turbine Blade Tip with Different Shapes[J]. JOURNAL OF THERMAL SCIENCE,2013,22(2):128-134.
APA Liu, Jian-Jun,Li, Peng,Zhang, Chao,&An, Bai-Tao.(2013).Flowfield and Heat Transfer past an Unshrouded Gas Turbine Blade Tip with Different Shapes.JOURNAL OF THERMAL SCIENCE,22(2),128-134.
MLA Liu, Jian-Jun,et al."Flowfield and Heat Transfer past an Unshrouded Gas Turbine Blade Tip with Different Shapes".JOURNAL OF THERMAL SCIENCE 22.2(2013):128-134.

入库方式: OAI收割

来源:工程热物理研究所

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