中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Investigation of pressure oscillations in supersonic cavity flow

文献类型:期刊论文

作者Matsuo, S; Setoguchi, T; Yu, S
刊名INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES
出版日期1997
卷号14期号:4页码:239-246
关键词supersonic cavity flow pressure oscillation wavelet transform
英文摘要In a supersonic intake, at the shock position, a cavity with bleed plays an important role in the control of normal shock wave. The supersonic intake now tends to be unstable due to the shock wave / wall boundary layer or the shock wave / shear layer interactions occurring close to the leading edge of the cavity. In the present study, the effects of cavity / oblique shock wave interaction and bleeding on the pressure oscillation in the cavity were investigated experimentally in the case of the flow Mach number 1.74 at the cavity entrance and the characteristics of oscillation in the cavity were analyzed using the wavelet transforms.
WOS标题词Science & Technology ; Technology
类目[WOS]Engineering, Aerospace
研究领域[WOS]Engineering
收录类别SCI
语种英语
WOS记录号WOS:000072458700005
公开日期2015-12-22
源URL[http://ir.etp.ac.cn/handle/311046/106134]  
专题工程热物理研究所_中国科学院工程热物理所(论文库)_期刊论文(SCI)
作者单位1.Saga Univ, Dept Mech Engn, Saga 840, Japan
2.Chinese Acad Sci, Inst Engn Thermophys, Beijing 100080, Peoples R China
推荐引用方式
GB/T 7714
Matsuo, S,Setoguchi, T,Yu, S. Investigation of pressure oscillations in supersonic cavity flow[J]. INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES,1997,14(4):239-246.
APA Matsuo, S,Setoguchi, T,&Yu, S.(1997).Investigation of pressure oscillations in supersonic cavity flow.INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES,14(4),239-246.
MLA Matsuo, S,et al."Investigation of pressure oscillations in supersonic cavity flow".INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES 14.4(1997):239-246.

入库方式: OAI收割

来源:工程热物理研究所

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