中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Effects of Aspect Ratio in a Transonic Shock Tube Airfoil Flow

文献类型:期刊论文

作者Masashi KASHITANIl ; Keita MIURAl ; Shinichiro NAKA02 ; Yutaka YAMAGUCHI2
刊名JOURNAL OF THERMAL SCIENCE
出版日期2012
卷号21页码:435,440
关键词Shock tube Aerodynamics Transonic flows Aspect ratio Wind tunnel correction
公开日期2013-01-31
源URL[http://ir.etp.ac.cn/handle/311046/51878]  
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
Masashi KASHITANIl,Keita MIURAl,Shinichiro NAKA02,et al. Effects of Aspect Ratio in a Transonic Shock Tube Airfoil Flow[J]. JOURNAL OF THERMAL SCIENCE,2012,21:435,440.
APA Masashi KASHITANIl,Keita MIURAl,Shinichiro NAKA02,&Yutaka YAMAGUCHI2.(2012).Effects of Aspect Ratio in a Transonic Shock Tube Airfoil Flow.JOURNAL OF THERMAL SCIENCE,21,435,440.
MLA Masashi KASHITANIl,et al."Effects of Aspect Ratio in a Transonic Shock Tube Airfoil Flow".JOURNAL OF THERMAL SCIENCE 21(2012):435,440.

入库方式: OAI收割

来源:工程热物理研究所

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