Configuration of Shock Waves in Two-Dimensional Overexpanded Jets
文献类型:期刊论文
作者 | Masashi Kashitani1; Kazuyasu Matsuo3; Yutaka Yamaguchil; Yoshiaki Miyazato2; Mitsuharu Masuda2 |
刊名 | JOURNAL OF THERMAL SCIENCE
![]() |
出版日期 | 2003 |
卷号 | 12期号:4页码:294,298 |
关键词 | Overexpanded Jet Shock Wave Compressible Flow Supersonic Nozzle. |
英文摘要 | An experimental and analytical study has been carried out to obtain the clear understanding of a shock wave transition associated with a steady two-dimensional overexpanded flow. Two-dimensional inviscid theory with respect to a shock wave reflection is used in the present study on the characteristic of shock waves. The results obtained from the flow analysis are compared with those obtained from flow visualizations. It is shown that in the region of regular reflection, the angle of an incident shock wave becomes lower than that calculated by two shock theory with an increment in the ratio pe/pb of the nozzle exit pressure pe to the back pressure pb. It is indicated that the configuration of shock waves in overexpanded jets is influenced by the divergent angle at the nozzle exit. Also it is shown from the flow visualization that a series of shock waves move into the nozzle inside with a decrease in pressure ratio pe/pb, even if the pe/pb is under overexpanded conditions. |
公开日期 | 2013-03-12 |
源URL | [http://ir.etp.ac.cn/handle/311046/53492] ![]() |
专题 | 工程热物理研究所_Journal of Thermal Science |
推荐引用方式 GB/T 7714 | Masashi Kashitani1,Kazuyasu Matsuo3,Yutaka Yamaguchil,et al. Configuration of Shock Waves in Two-Dimensional Overexpanded Jets[J]. JOURNAL OF THERMAL SCIENCE,2003,12(4):294,298. |
APA | Masashi Kashitani1,Kazuyasu Matsuo3,Yutaka Yamaguchil,Yoshiaki Miyazato2,&Mitsuharu Masuda2.(2003).Configuration of Shock Waves in Two-Dimensional Overexpanded Jets.JOURNAL OF THERMAL SCIENCE,12(4),294,298. |
MLA | Masashi Kashitani1,et al."Configuration of Shock Waves in Two-Dimensional Overexpanded Jets".JOURNAL OF THERMAL SCIENCE 12.4(2003):294,298. |
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。