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超声速预混可燃气流的点火与燃烧
引用本文:孙英英,韩肇元,司徒明,琚诒光.超声速预混可燃气流的点火与燃烧[J].工程热物理学报,2002,23(6):776-778.
作者姓名:孙英英  韩肇元  司徒明  琚诒光
作者单位:1. 清华大学工程力学系,北京,100084
2. 中国科技大学力学和机械工程系,安徽,合肥,230027
3. 航天机电集团公司31所,北京 100074
基金项目:国家自然科学基金资助项目(No.19882005),国家“863”航天领域资助项目(No.863-2.99.9
摘    要:在激波风洞一激波管组合设备上开展了碳氢燃料超声速预混可燃气流的点火与燃烧实验研究。实验结果表明:利用激波对燃料进行预热,并以高温燃气作为引导火焰,可以有效缩短汽油空气超声速可燃混气的点火延迟时间,使之缩短到 0.2 ms以下。利用纹影照片对超声速燃烧流场结构作出了分析;研究了超声速预混可燃气流的温度以及当量比对超声速燃烧流场结构、点火与火焰传播特性的影响。

关 键 词:碳氢燃料  点火  超声速燃烧
文章编号:0253-231X(2002)06-0776-03
修稿时间:2001年12月8日

IGNITION AND COMBUSTION OF SUPERSONIC PREMIXED HYDROCARBON FUEL-AIR MIXTURE
SUN Ying-Ying,HAN Zhao-Yuan,SITU Ming JU Yi-Guang.IGNITION AND COMBUSTION OF SUPERSONIC PREMIXED HYDROCARBON FUEL-AIR MIXTURE[J].Journal of Engineering Thermophysics,2002,23(6):776-778.
Authors:SUN Ying-Ying  HAN Zhao-Yuan  SITU Ming JU Yi-Guang
Abstract:Experimental investigation on ignition and combustion of supersonic premixed hydrocarbon fuel-air mixture has been conducted in the combination facility consisting of a shock tunnel and a shock tube. The experimental results showed that the ignition delay of supersonic premixed gasoline-air mixture could be effectively shortened to less than 0.2 ms through preheating fuel by shock waves and by using hot gas as pilot flame. The structure of supersonic combustion flow field was investigated with the Schlieren pictures. The effects of temperature and equivalence ratio of supersonic premixed combustible flow on the structure of supersonic combustion flow field, ignition and flame propagation were studied.
Keywords:hydrocarbon fuel  ignition  supersonic combustion
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