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凹腔型亚燃冲压发动机燃烧效率研究
引用本文:谭建国,黄国庆,潘余,王振国.凹腔型亚燃冲压发动机燃烧效率研究[J].航空动力学报,2011,26(6):1415-1419.
作者姓名:谭建国  黄国庆  潘余  王振国
作者单位:国防科学技术大学航天与材料工程学院,长沙,410073
基金项目:国家自然科学基金(51076164)
摘    要:通过开展亚燃冲压发动机直连式试验,研究了不同来流条件、不同余气系数时的燃烧性能.结果表明:燃烧效率受来流温度的影响较小,但随着余气系数增加,燃烧效率降低.总体而言,凹腔型燃烧室具有0.9左右的燃烧效率,初步达到了亚燃冲压发动机的实用化要求.

关 键 词:亚燃冲压发动机  燃烧效率  凹腔  余气系数  直连式
收稿时间:2010/5/22 0:00:00
修稿时间:2010/10/18 0:00:00

Research on combustion efficiency of cavity-type ramjet
TAN Jian-guo,HUANG Guo-qing,PAN Yu and WANG Zhen-guo.Research on combustion efficiency of cavity-type ramjet[J].Journal of Aerospace Power,2011,26(6):1415-1419.
Authors:TAN Jian-guo  HUANG Guo-qing  PAN Yu and WANG Zhen-guo
Institution:TAN Jian-guo,HUANG Guo-qing,PAN Yu,WANG Zhen-guo(College of Aerospace and Materials Engineering,National University of Defense Technology,Changsha 410073,China)
Abstract:Direct-connected experiments were conducted to reveal combustion performance of cavity-type ramjet under different incoming flow and excess air coefficients.Results show that the combustion efficiency decreases with excess air coefficient,but depends little on the temperature of the incoming flow.Generally speaking,90% combustion efficiency of cavity-type combustor is sufficient enough to satisfy the requirement of ramjet.
Keywords:ramjet  combustion efficient  cavity  excess air coefficient  direct-connected  
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