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 MaximumCamber

文献类型:期刊论文

作者Naixing Chen ; Hongwu Zhang ; Yanji Xu ; Weiguang Huang
刊名JOURNAL OF THERMAL SCIENCE
出版日期2003
卷号12期号:3页码:198,203
关键词axial transonic compressor 3D aerodynamic design optimization N.S. solver rapid generation of computational meshes.
公开日期2013-03-12
源URL[http://ir.etp.ac.cn/handle/311046/53454]  
专题工程热物理研究所_Journal of Thermal Science_期刊论文
推荐引用方式
GB/T 7714
Naixing Chen,Hongwu Zhang,Yanji Xu,et al. A Study of 3D Aerodynamic Design for a Transonic Compressor Blading Optimized by the Locations of Aerofoil Maximum Thickness and MaximumCamber[J]. JOURNAL OF THERMAL SCIENCE,2003,12(3):198,203.
APA Naixing Chen,Hongwu Zhang,Yanji Xu,&Weiguang Huang.(2003).A Study of 3D Aerodynamic Design for a Transonic Compressor Blading Optimized by the Locations of Aerofoil Maximum Thickness and MaximumCamber.JOURNAL OF THERMAL SCIENCE,12(3),198,203.
MLA Naixing Chen,et al."A Study of 3D Aerodynamic Design for a Transonic Compressor Blading Optimized by the Locations of Aerofoil Maximum Thickness and MaximumCamber".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

浏览0
下载0
收藏0
其他版本

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。