上海航天（中英文）2025，Vol.42Issue(2)：166-176,11.DOI:10.19328/j.cnki.2096-8655.2025.02.016
横向氢气射流诱导斜爆轰波起爆的数值研究
Numerical Study on the Oblique Detonation Wave Induced by a Transverse Hydrogen Jet
摘要
Abstract
Setting a transverse hydrogen jet in the induction zone is an effective active control scheme to implement the controllable and fast initiation of an oblique detonation wave(ODW)under high altitude flight conditions.In this paper,the flow characteristics of the ODW induced by a transverse hydrogen jet and the effects of the jet dynamic pressure ratio and jet angle are studied by solving the two-dimensional reaction Euler equations.The results show that the accelerated initiation of an ODW can be implemented by setting a transverse hydrogen jet in the induction zone.The jet-induced ODW has two initiation patterns,i.e.,strong coupling and weak coupling.In addition,the height of the ODW at the exit of the combustor is proportional to the jet dynamic pressure ratio and jet angle,and the active control of the ODW can be implemented by changing the jet dynamic pressure ratio and jet angle.Therefore,with proper jet dynamic pressure ratio and jet angle,the stable operation of ODW engine can be achieved.关键词
高超声速/斜爆轰波(ODW)发动机/横向射流/加速起爆/波系结构/动态控制Key words
hypersonic velocity/oblique detonation wave(ODW)engine/transverse jet/accelerated initiation/wave structure/active control分类
力学引用本文复制引用
马君涵,姚瑞扬,张斌..横向氢气射流诱导斜爆轰波起爆的数值研究[J].上海航天（中英文）,2025,42(2):166-176,11.基金项目
国家自然科学基金资助项目(52176120) （52176120）
