中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
A Study of 3D Aerodynamic Design for a Transonic Compressor Blading Optimized by the Locations of Aerofoil Maximum Thickness and Maximum Camber

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2003-08-01
卷号12期号:3页码:198-203
关键词axial transonic compressor 3D aerodynamic design optimization NS solver rapid generation of computational meshes
英文摘要A design procedure for improving the efficiency of a transonic compressor blading was proposed based on a rapid generation method for three-dimensional blade configuration and computational meshes, a three-dimensional Navier-Stokes solver and an optimization approach. The objective of the present paper is to design a transonic compressor blading optimized only by selection of the locations of maximum camber and maximum thickness for the airfoils at different span heights and to study how do these two design parameters affect the blade performance. The blading configuration and the computational meshes can be obtained very rapidly for any given combination of maximum camber and maximum thickness. The computational grid system generated is used for the Navier-Stokes solution to predict adiabatic efficiency, total pressure ratio and flow rate. As a main result of the optimization, adiabatic efficiency was successfully improved.
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:000208227800002
公开日期2015-12-22
源URL[http://ir.etp.ac.cn/handle/311046/106155]  
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. A Study of 3D Aerodynamic Design for a Transonic Compressor Blading Optimized by the Locations of Aerofoil Maximum Thickness and Maximum Camber[J]. JOURNAL OF THERMAL SCIENCE,2003,12(3):198-203.
APA Chen, Naixing,Zhang, Hongwu,Xu, Yanji,&Huang, Weiguang.(2003).A Study of 3D Aerodynamic Design for a Transonic Compressor Blading Optimized by the Locations of Aerofoil Maximum Thickness and Maximum Camber.JOURNAL OF THERMAL SCIENCE,12(3),198-203.
MLA Chen, Naixing,et al."A Study of 3D Aerodynamic Design for a Transonic Compressor Blading Optimized by the Locations of Aerofoil Maximum Thickness and Maximum Camber".JOURNAL OF THERMAL SCIENCE 12.3(2003):198-203.

入库方式: OAI收割

来源:工程热物理研究所

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