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
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。