中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Effect of Axisymmetric Sonic Nozzle Geometry on Characteristics of Supersonic Air Jet

文献类型:期刊论文

作者Shigeru MATSU01; Masanori TANAKAl; Yumiko OTOBE2; Hideo KASHIMURA2; Heuy-Dong KIM3; Toshiaki SETOGUCHI1
刊名JOURNAL OF THERMAL SCIENCE
出版日期2004
卷号13期号:2页码:121,126
关键词Compressible Flow Supersonic Jet Non-equilibrium Condensation Simulation
英文摘要The effect of nozzle geometry on sonic line and characteristics of supersonic air jet was studied. Computational fluid dynamics was applied in this study. The axisymmetric nozzle geometries investigated were two different contour converging nozzles, two different conically converging sharp-edged nozzles and a sharp-edged orifice. The results show that the supersonic jet structure, sonic line and streamlines in supersonic jet are strongly influenced by the nozzle geometry, and the total pressure loss increases with the increase of Mach disk diameter. The present numerical simulation is an effective tool to evaluate compressible flows in supersonic air jet.
公开日期2013-03-11
源URL[http://ir.etp.ac.cn/handle/311046/53310]  
专题工程热物理研究所_Journal of Thermal Science
推荐引用方式
GB/T 7714
Shigeru MATSU01,Masanori TANAKAl,Yumiko OTOBE2,et al. Effect of Axisymmetric Sonic Nozzle Geometry on Characteristics of Supersonic Air Jet[J]. JOURNAL OF THERMAL SCIENCE,2004,13(2):121,126.
APA Shigeru MATSU01,Masanori TANAKAl,Yumiko OTOBE2,Hideo KASHIMURA2,Heuy-Dong KIM3,&Toshiaki SETOGUCHI1.(2004).Effect of Axisymmetric Sonic Nozzle Geometry on Characteristics of Supersonic Air Jet.JOURNAL OF THERMAL SCIENCE,13(2),121,126.
MLA Shigeru MATSU01,et al."Effect of Axisymmetric Sonic Nozzle Geometry on Characteristics of Supersonic Air Jet".JOURNAL OF THERMAL SCIENCE 13.2(2004):121,126.

入库方式: OAI收割

来源:工程热物理研究所

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