冲压发动机燃烧室内低频燃烧不稳定试验

推进技术 ›› 2011, Vol. 32 ›› Issue (2): 188-190.

冲压发动机燃烧室内低频燃烧不稳定试验

谭建国,潘余,王振国

国防科技大学航天与材料工程学院, 湖南长沙 410073;国防科技大学航天与材料工程学院, 湖南长沙 410073;国防科技大学航天与材料工程学院, 湖南长沙 410073

发布日期:2021-08-15
作者简介:谭建国(1974—),男,博士,副教授,研究领域为液体火箭发动机和液体冲压发动机。E-mail:tanjgmail@yahoo.com.cn
基金资助:
国家自然科学基金(51076164)。

Experimental research on low-frequency instability in ramjet combustor

lnst. of Aerospace and Material Engineering, National Univ. of Defence Technology, Changsha 410073, China;lnst. of Aerospace and Material Engineering, National Univ. of Defence Technology, Changsha 410073, China;lnst. of Aerospace and Material Engineering, National Univ. of Defence Technology, Changsha 410073, China

Published:2021-08-15

摘要/Abstract

摘要： 在高空亚燃冲压发动机研究中,燃烧不稳定是一个突出问题。为解决30km,Ma=4亚燃冲压发动机直连式试验中所出现的低频燃烧不稳定问题,分析了燃烧室的声学特性,得出了燃烧不稳定的主要特征是燃烧放热与一阶纵向声振模态相耦合。采取在燃烧室内增加后向台阶形成凹腔的方法,成功得到了较为稳定的燃烧。

关键词: 亚燃冲压发动机; 燃烧不稳定; 低压; 声振

Abstract: Combustion instability is one of the most crucial problems for developing high-altitude ramjet. To solve combustion instability problem occurred in a direct-connected experiments of a 30km, Ma=4 ramjet, acoustic characteristics are analyzed. Results show that the main character of combustion instability is due to the coupling of heat release and longitudinal acoustic oscillation. Then relative stable combustion is achieved in cavity-type combustor by adding backward step. 

Key words: Ramjet; Combustion instability; Low pressure; Acoustic oscillation

谭建国,潘余,王振国. 冲压发动机燃烧室内低频燃烧不稳定试验[J]. 推进技术, 2011, 32(2): 188-190.