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凹腔喷射超声速燃烧火焰结构实验研究
引用本文:范周琴,刘卫东,林志勇,孙明波.凹腔喷射超声速燃烧火焰结构实验研究[J].推进技术,2013,34(1):62-68.
作者姓名:范周琴  刘卫东  林志勇  孙明波
作者单位:国防科技大学航天与材料工程学院/高超声速冲压发动机技术重点实验室,湖南长沙,410073
基金项目:国家自然科学基金(91116001;50906098)。
摘    要:为加深对凹腔喷射超声速燃烧火焰结构的认识,利用OH基自发辐射成像和PLIF技术对凹腔上游横向喷注氢气的超声速燃烧流场进行研究.结果表明,火焰主要分布在凹腔剪切层附近及喷流内部,喷口附近没有火焰;燃料喷注当量比、燃料喷注位置及凹腔构型对火焰分布和火焰强度影响较大,在设计燃烧室时应加以考虑.

关 键 词:OH基PLIF  自发辐射  凹腔剪切层  火焰
收稿时间:2011/10/26 0:00:00
修稿时间:2012/4/23 0:00:00

Experimental Investigation on Supersonic Combustion Flame Structure with Cavity Injectors
FAN Zhou-qin,LIU Wei-dong,LIN Zhi-yong and SUN Ming-bo.Experimental Investigation on Supersonic Combustion Flame Structure with Cavity Injectors[J].Journal of Propulsion Technology,2013,34(1):62-68.
Authors:FAN Zhou-qin  LIU Wei-dong  LIN Zhi-yong and SUN Ming-bo
Institution:Science and Technology on Scramjet Laboratory/Institute of Aerospace and Material Engineering, National University of Defence Technology, Changsha 410073,China;Science and Technology on Scramjet Laboratory/Institute of Aerospace and Material Engineering, National University of Defence Technology, Changsha 410073,China;Science and Technology on Scramjet Laboratory/Institute of Aerospace and Material Engineering, National University of Defence Technology, Changsha 410073,China;Science and Technology on Scramjet Laboratory/Institute of Aerospace and Material Engineering, National University of Defence Technology, Changsha 410073,China
Abstract:
Keywords:OH-PLIF  Spontaneous emission  Cavity shear layer  Flame
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