The dynamics of oblique detonation waves in non-uniform inflows: Flame structure and stability

IF 6.2 2区 工程技术 Q2 ENERGY & FUELS
Combustion and Flame Pub Date : 2026-05-01 Epub Date: 2026-02-27 DOI:10.1016/j.combustflame.2026.114886
Yichen Zhang , Xiaojing Zheng , Gaoxiang Xiang
{"title":"The dynamics of oblique detonation waves in non-uniform inflows: Flame structure and stability","authors":"Yichen Zhang ,&nbsp;Xiaojing Zheng ,&nbsp;Gaoxiang Xiang","doi":"10.1016/j.combustflame.2026.114886","DOIUrl":null,"url":null,"abstract":"<div><div>The successful operation of oblique detonation wave (ODW) engines is critically dependent on the stability of the detonation wavefront under realistic, non-uniform inflow conditions, a phenomenon that remains inadequately understood. This study employs two-dimensional simulations with a detailed H<sub>2</sub>/air mechanism to systematically elucidate the dynamic response of ODW structures to both gradient-type and sine-type inhomogeneities in equivalence ratio, pressure, temperature, and velocity. Results reveal that gradient-type inflows induce progressive deflection of the wavefront and alter the transition locus, whereas sine-type non-uniformities trigger periodic modulation, leading to distinctive flame dynamics including cellular patterns and localized extinction-reignition cycles. Crucially, large-amplitude oscillations are found to provoke decoupling of the shock and reaction fronts, defining critical stability boundaries. These findings provide fundamental insights into the coupling between inflow perturbations and detonation combustion, offering vital guidelines for the robust design of hypersonic propulsion systems.</div></div>","PeriodicalId":280,"journal":{"name":"Combustion and Flame","volume":"287 ","pages":"Article 114886"},"PeriodicalIF":6.2000,"publicationDate":"2026-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Combustion and Flame","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0010218026001227","RegionNum":2,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"2026/2/27 0:00:00","PubModel":"Epub","JCR":"Q2","JCRName":"ENERGY & FUELS","Score":null,"Total":0}
引用次数: 0

Abstract

The successful operation of oblique detonation wave (ODW) engines is critically dependent on the stability of the detonation wavefront under realistic, non-uniform inflow conditions, a phenomenon that remains inadequately understood. This study employs two-dimensional simulations with a detailed H2/air mechanism to systematically elucidate the dynamic response of ODW structures to both gradient-type and sine-type inhomogeneities in equivalence ratio, pressure, temperature, and velocity. Results reveal that gradient-type inflows induce progressive deflection of the wavefront and alter the transition locus, whereas sine-type non-uniformities trigger periodic modulation, leading to distinctive flame dynamics including cellular patterns and localized extinction-reignition cycles. Crucially, large-amplitude oscillations are found to provoke decoupling of the shock and reaction fronts, defining critical stability boundaries. These findings provide fundamental insights into the coupling between inflow perturbations and detonation combustion, offering vital guidelines for the robust design of hypersonic propulsion systems.
非均匀流入中斜爆震波的动力学:火焰结构和稳定性
斜爆震波(ODW)发动机的成功运行在很大程度上取决于爆震波前在现实的非均匀流入条件下的稳定性,这一现象仍然没有得到充分的了解。本研究通过二维模拟H2/空气的详细机理,系统地阐明了ODW结构对梯度型和正弦型非均匀性在等效比、压力、温度和速度方面的动态响应。结果表明,梯度型流入引起波前逐渐偏转并改变过渡轨迹,而正弦型非均匀性引发周期性调制,导致独特的火焰动力学,包括细胞模式和局部熄灭-重燃循环。至关重要的是,发现大振幅振荡会引起冲击和反应锋面的解耦,从而定义临界稳定性边界。这些发现对流入扰动和爆轰燃烧之间的耦合提供了基本的见解,为高超声速推进系统的鲁棒设计提供了重要的指导。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
Combustion and Flame
Combustion and Flame 工程技术-工程:化工
CiteScore
9.50
自引率
20.50%
发文量
631
审稿时长
3.8 months
期刊介绍: The mission of the journal is to publish high quality work from experimental, theoretical, and computational investigations on the fundamentals of combustion phenomena and closely allied matters. While submissions in all pertinent areas are welcomed, past and recent focus of the journal has been on: Development and validation of reaction kinetics, reduction of reaction mechanisms and modeling of combustion systems, including: Conventional, alternative and surrogate fuels; Pollutants; Particulate and aerosol formation and abatement; Heterogeneous processes. Experimental, theoretical, and computational studies of laminar and turbulent combustion phenomena, including: Premixed and non-premixed flames; Ignition and extinction phenomena; Flame propagation; Flame structure; Instabilities and swirl; Flame spread; Multi-phase reactants. Advances in diagnostic and computational methods in combustion, including: Measurement and simulation of scalar and vector properties; Novel techniques; State-of-the art applications. Fundamental investigations of combustion technologies and systems, including: Internal combustion engines; Gas turbines; Small- and large-scale stationary combustion and power generation; Catalytic combustion; Combustion synthesis; Combustion under extreme conditions; New concepts.
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:604180095
Book学术官方微信
小红书