Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures
文献类型：期刊论文
| 作者 | Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民)
|
| 刊名 | INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
 |
| 出版日期 | 2019-08-30 |
| 卷号 | 44期号:41页码:23429-23435 |
| 关键词 | Oblique detonation wave Boundary layer Viscosity Detonation initiation Hydrogen-air mixture |
| ISSN号 | 0360-3199 |
| DOI | 10.1016/j.ijhydene.2019.07.005 |
| 通讯作者 | Zhang, Zijian(zhangzijian@imech.ac.cn) |
| 英文摘要 | Oblique detonation wave (ODW) structures are studied widely in recent years, but most of them are solved by the Euler equations without considering viscosity and then effects of boundary layer. In this study, the Navier-Stokes Equations are used to simulate the wedge-induced ODWs in hydrogen-air mixtures, and the two types of ODW transition structures at different incident Mach number M-i are analyzed to clarify the effects of viscosity and hence the boundary layer. Results show that the effect of boundary layer on ODW structures should be classified by the types of ODW transition patterns. As for the smooth transition pattern of ODW at high Mach numbers, the effect of boundary layer can be neglected, but for the abrupt transition pattern of ODW at low Mach numbers, the effect of boundary layer is large and it changes the ODW structure greatly. Resulting from the interaction of shock and boundary layer, a recirculation zone is formed within the viscous ODW layer at M-i = 7, which leads to the phenomenon that the straight oblique shock wave evolves into two sections, with the downstream one having a larger shock angle. Additionally, the corresponding transition position moves upstream, and the initiation length becomes only one third of that in inviscid ODW. The great importance of considering viscosity in ODW simulations and future designs of combustor of oblique detonation engine has been addressed. (C) 2019 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved. |
| 分类号 | 二类 |
| WOS关键词 | WAVES ; INITIATION ; SIMULATIONS ; TRANSITION |
| 资助项目 | National Natural Science Foundation of China[11672308] ; National Natural Science Foundation of China[11532014] |
| WOS研究方向 | Chemistry ; Electrochemistry ; Energy & Fuels |
| 语种 | 英语 |
| WOS记录号 | WOS:000485210500063 |
| 资助机构 | National Natural Science Foundation of China |
| 其他责任者 | Zhang, Zijian |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/80018]  |
| 专题 | 力学研究所_高温气体动力学国家重点实验室 |
| 推荐引用方式 GB/T 7714 | Fang YS,Zhang ZJ,Hu ZM. Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures[J]. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY,2019,44(41):23429-23435. |
| APA | 方宜申,张子健,&胡宗民.(2019).Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures.INTERNATIONAL JOURNAL OF HYDROGEN ENERGY,44(41),23429-23435. |
| MLA | 方宜申,et al."Effects of boundary layer on wedge-induced oblique detonation structures in hydrogen-air mixtures".INTERNATIONAL JOURNAL OF HYDROGEN ENERGY 44.41(2019):23429-23435. |
入库方式： OAI收割
来源：力学研究所
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