Numerical Study on Kerosene Spray in Supersonic Flow

IMECH-IR > 力学所知识产出(1956-2008)

	Numerical Study on Kerosene Spray in Supersonic Flow
	Yue LJ(岳连捷); Yu G(俞刚)
会议录名称	Shock Waves, Vols 1 and 2, Proceedings of 24th International Symposium on Shock Waves,2004 Pages: 927-933 Published: 2005
	2004-07-11
会议名称	24th International Symposium on Shock Waves, JUL 11-16, 2004 Beijing, PEOPLES R CHINA
摘要	Numerical simulation was conducted to study the kerosene spray characteristics injecting into supersonic cross flow. The verification of the simulation was carried out by experimental Schlieren image, and the agreement was obtained by compared the spray plume pictures. Furthermore, the aerodynamic secondary breakup effect of the supersonic cross flow on the initial droplets was investigated. It was revealed that the initial parent drops were broken up into small drops whose diameter is about O(10) micrometers soon after they entered into the supersonic cross flow. During the appropriate range of initial drop size, the parent droplets would be broken up into small drops with the same magnitude diameter no matter how large the initial drops SMD was.
WOS记录号	WOS:000231243300141
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/311007/13910
专题	力学所知识产出(1956-2008)
通讯作者	Yu G(俞刚)
推荐引用方式 GB/T 7714	Yue LJ,Yu G. Numerical Study on Kerosene Spray in Supersonic Flow[C]Shock Waves, Vols 1 and 2, Proceedings of 24th International Symposium on Shock Waves,2004 Pages: 927-933 Published: 2005,2004.

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