中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Geometry Effects on Aerodynamics Performance of a Low Aspect Ratio Turbine Nozzle

文献类型:期刊论文

作者Chen, Naixing; Zhang, Hongwu; Xu, Yanji; Huang, Weiguang
刊名JOURNAL OF THERMAL SCIENCE
出版日期2004-11-01
卷号13期号:4页码:289-296
关键词3D aerodynamics of turbomachinery turbine design optimization geometry effect
英文摘要This paper describes the influence of some geometric parameters on aerodynamics performance of a low-aspect-ratio turbine blading designed by a novel method developed at the Institute of Engineering Thermophysics, Chinese Academy of Sciences. This is a part of the study on aerodynamics optimization of turbomachinery. It follows the development of the basic ideas in the turbomachinery aerodynamics research project at the institute. The present paper concentrates mainly on the effects of geometry, such as stagger angle, leading and trailing edge thickness, maximum thickness and its location on adiabatic efficiency, total pressure ratio and mass flow rate. The study was performed and assessed for a low- aspect ratio turbine nozzle using 3D steady Reynolds-averaged N.S. solver. Using the knowledge of the flow physics analysis an optimized turbine nozzle was obtained.
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:000208228300001
公开日期2015-12-22
源URL[http://ir.etp.ac.cn/handle/311046/106191]  
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 100080, Peoples R China
推荐引用方式
GB/T 7714
Chen, Naixing,Zhang, Hongwu,Xu, Yanji,et al. Geometry Effects on Aerodynamics Performance of a Low Aspect Ratio Turbine Nozzle[J]. JOURNAL OF THERMAL SCIENCE,2004,13(4):289-296.
APA Chen, Naixing,Zhang, Hongwu,Xu, Yanji,&Huang, Weiguang.(2004).Geometry Effects on Aerodynamics Performance of a Low Aspect Ratio Turbine Nozzle.JOURNAL OF THERMAL SCIENCE,13(4),289-296.
MLA Chen, Naixing,et al."Geometry Effects on Aerodynamics Performance of a Low Aspect Ratio Turbine Nozzle".JOURNAL OF THERMAL SCIENCE 13.4(2004):289-296.

入库方式: OAI收割

来源:工程热物理研究所

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