IMECH-IR  > 力学所知识产出(1956-2008)
Direct numerical simulation of round supersonic free jet
Li XL(李新亮); Fu DX(傅德薰); Ma YW(马延文); Li, XL (reprint author), Chinese Acad Sci, LNM, Inst Mech, Beijing 100080, Peoples R China.
Source PublicationRECENT ADVANCES IN FLUID MECHANICS
2004
Conference Name4th International Conference on Fluid Mechanics
Conference DateJUL 20-30, 2004
Conference PlaceDalian, PEOPLES R CHINA
Abstract6th order group-velocity control scheme is constructed and used in direct numerical simulation of the round supersonic free jet. The exit Mach number of the jet is 2.5. The disturbance waves generated by the jet are showed and the reason of the existence up-stream propagated wave is analyzed.
WOS IDWOS:000225709300159
ISBN7-302-08817-9
Indexed ByCPCI-S
Language英语
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Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/58920
Collection力学所知识产出(1956-2008)
Corresponding AuthorLi, XL (reprint author), Chinese Acad Sci, LNM, Inst Mech, Beijing 100080, Peoples R China.
Recommended Citation
GB/T 7714
Li XL,Fu DX,Ma YW,et al. Direct numerical simulation of round supersonic free jet[C]RECENT ADVANCES IN FLUID MECHANICS,2004.
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