Direct numerical simulation of round supersonic free jet

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.
会议录名称	RECENT ADVANCES IN FLUID MECHANICS
	2004
会议名称	4th International Conference on Fluid Mechanics
会议日期	JUL 20-30, 2004
会议地点	Dalian, PEOPLES R CHINA
摘要	6th 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记录号	WOS:000225709300159
ISBN号	7-302-08817-9
收录类别	CPCI-S
语种	英语
引用统计
文献类型	会议论文
条目标识符	http://dspace.imech.ac.cn/handle/311007/58920
专题	力学所知识产出(1956-2008)
通讯作者	Li, XL (reprint author), Chinese Acad Sci, LNM, Inst Mech, Beijing 100080, Peoples R China.
推荐引用方式 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.