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Effect of ozone addition on oblique detonations in hydrogen-air mixtures

文献类型：期刊论文

作者Teng, Honghui2,3,4; Liu, Siyuan4; Li, Zhenzhen4; Yang, Pengfei1; Wang, Kuanliang4; Tian, Cheng4; Yang PF(杨鹏飞)
刊名APPLIED THERMAL ENGINEERING
出版日期2024-03-01
卷号240页码:10
关键词Oblique detonation Ozone Initiation
ISSN号1359-4311
DOI10.1016/j.applthermaleng.2023.122292
通讯作者Tian, Cheng(chengtianbit@outlook.com)
英文摘要Ozone addition is a promising method to enhance the ignition processes and may have potential use in the practical application of oblique detonation engines (ODEs), especially under challenging low Mach number conditions where ignition is hard to achieve. In this study, numerical simulations are conducted to explore the effect of ozone addition on oblique detonations. Numerical results show that with ozone addition, the transition between the induction oblique shock wave (OSW) and oblique detonation wave (ODW) will be smoother at relatively high flight Mach number (from 9 to 10). The reasons for this wave system transformation are dis-cussed. With the addition of ozone, the initiation of ODW can occur at a shorter distance and height, preventing the convergence of compression waves into shocks and resulting in a smoother transition. It was also found that adding ozone is an effective approach to decrease the initiation length, especially at a relatively low Mach number (9), which is crucial to the ODE's thermal protection. Furthermore, the effects of ozone addition on total pressure have been analyzed, demonstrating its positive influence on the propulsion performance of ODE. At a lower flight Mach number (8), ozone addition can re-stabilize the unsteady ODW with a normal detonation wave moving upstream. This is achieved by reducing the size of the subsonic regions, indicating that ozone addition can broaden the working flight Mach numbers of ODEs.
WOS关键词NUMERICAL-SIMULATION ; INITIATION ; CRITERIA ; WAVES
资助项目National Natural Science Foundation of China[12002041] ; National Natural Science Foundation of China[12325206] ; Advanced Jet Propulsion Innovation Center, Aero Engine Academy of China[HKCX2022-01-018]
WOS研究方向Thermodynamics ; Energy & Fuels ; Engineering ; Mechanics
语种英语
WOS记录号WOS:001165906200001
资助机构National Natural Science Foundation of China ; Advanced Jet Propulsion Innovation Center, Aero Engine Academy of China
源URL[http://dspace.imech.ac.cn/handle/311007/94540]  
专题力学研究所_高温气体动力学国家重点实验室
通讯作者Tian, Cheng
作者单位1.Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
2.Aero Engine Acad China, Adv Jet Prop Innovat Ctr, Beijing 101300, Peoples R China
3.Beijing Inst Technol Chongqing Innovat Ctr, Chongqing 401120, Peoples R China
4.Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China
推荐引用方式
GB/T 7714		 Teng, Honghui,Liu, Siyuan,Li, Zhenzhen,et al. Effect of ozone addition on oblique detonations in hydrogen-air mixtures[J]. APPLIED THERMAL ENGINEERING,2024,240:10.
APA Teng, Honghui.,Liu, Siyuan.,Li, Zhenzhen.,Yang, Pengfei.,Wang, Kuanliang.,...&杨鹏飞.(2024).Effect of ozone addition on oblique detonations in hydrogen-air mixtures.APPLIED THERMAL ENGINEERING,240,10.
MLA Teng, Honghui,et al."Effect of ozone addition on oblique detonations in hydrogen-air mixtures".APPLIED THERMAL ENGINEERING 240(2024):10.

入库方式： OAI收割

来源：力学研究所

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