期刊文献+

整体式液体冲压发动机旋流燃烧室试验研究 被引量:1

AN EXPERIMENTAL INVESTIGATION OF THE SWIRLING COMBUSTOR FOR INTEGRAL LIQUID FUEL RAMJET
下载PDF
导出
摘要 介绍了在燃烧室进口安置旋流室和火焰稳定器后,在增加燃烧稳定性和强化燃烧方面所取得的突破性进展。地面热试车的结果表明,旋流室与火焰稳定器相结合的结构方案,能够有效地消除低频燃烧振荡,提高燃烧效率。 In integral liquid fuel ramjet,the low frequency combustion oscillation is a very serious problem which greatly affects the normal operation of engine and fuel energy release .A great progress has been made in the enhancing of combustion stability and the improving of combustion process since the swirl ing chamber and flameholder was installed at combustor entrance. Ground hotting test results show that the combinative configuration of swirling chamber and flameholder can effectly eliminate the low frequency combustion oscillation and increase the combustion efficiency.
机构地区 航空航天部
出处 《推进技术》 EI CAS CSCD 北大核心 1992年第2期13-17,共5页 Journal of Propulsion Technology
关键词 喷气发动机 燃烧室 燃烧 Ramjet engine,Dump combustion chamber,Flame holder,Oscillation burning
  • 相关文献

同被引文献5

引证文献1

二级引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部