中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Effect of Exit Geometry of Tail Pipe on the Performance of Pulse Jet Engines

文献类型:期刊论文

作者Toshihiro NAKANO ; Shigeru MATSU02 ; Kenbu TERAMOT03 ; Toshiaki SETOGUCHI4
刊名JOURNAL OF THERMAL SCIENCE
出版日期2006
卷号15期号:3页码:263,268
关键词compressible flow shock wave expansion wave pulse jet numerical simulation
公开日期2013-01-31
源URL[http://ir.etp.ac.cn/handle/311046/52106]  
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
Toshihiro NAKANO,Shigeru MATSU02,Kenbu TERAMOT03,et al. Effect of Exit Geometry of Tail Pipe on the Performance of Pulse Jet Engines[J]. JOURNAL OF THERMAL SCIENCE,2006,15(3):263,268.
APA Toshihiro NAKANO,Shigeru MATSU02,Kenbu TERAMOT03,&Toshiaki SETOGUCHI4.(2006).Effect of Exit Geometry of Tail Pipe on the Performance of Pulse Jet Engines.JOURNAL OF THERMAL SCIENCE,15(3),263,268.
MLA Toshihiro NAKANO,et al."Effect of Exit Geometry of Tail Pipe on the Performance of Pulse Jet Engines".JOURNAL OF THERMAL SCIENCE 15.3(2006):263,268.

入库方式: OAI收割

来源:工程热物理研究所

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