Numerical study on initiation of oblique detonations in hydrogen-air mixtures with various equivalence ratios | |
Zhang YN; Gong JS; Wang T(王涛); Zhang, YN (reprint author), Beijing Power Machinery Res Inst, State Key Lab Laser Prop & Applicat, Beijing 100074, Peoples R China. | |
发表期刊 | AEROSPACE SCIENCE AND TECHNOLOGY |
2016-02 | |
卷号 | 49页码:130-134 |
ISSN | 1270-9638 |
摘要 | Oblique detonations are simulated using Euler equations with the detailed chemical reaction models, and the initiation in hydrogen-air mixtures is studied. Different from most previous studies, inflow gas mixtures with low pressure and high temperature, derived from high altitude flight conditions of Oblique Detonation Wave Engines (ODWE), are used in this study. Numerical results demonstrate that the oblique shock-detonation surface is composed of three sections, including one section of quasi-detonation, demonstrating the weak coupling of shock and heat release. To study the inflow inhomogeneity effects derived from fuel injection, the simplified cases with different fuel-air equivalence ratios, from 0.1 to 2.0, are simulated and analyzed further. Results show that the dependence of characteristic length on fuel air equivalence ratio is the classical U-shape curve with critical ratio 0.8. Their values are influenced by inflow Ma but keep the same shape regardless of the inflow Ma. (C) 2015 Elsevier Masson SAS. All rights reserved. |
关键词 | Detonation Hydrogen Initiation Hypersonic |
DOI | 10.1016/j.ast.2015.11.035 |
URL | 查看原文 |
收录类别 | SCI ; EI |
语种 | 英语 |
WOS记录号 | WOS:000369198300013 |
关键词[WOS] | THERMOPLASTIC ELASTOMERS ; RUBBER ELASTICITY ; NETWORK MODELS ; BEHAVIOR ; NANOCOMPOSITES ; SIMULATIONS ; RECOVERY ; LIGHT |
WOS研究方向 | Engineering |
WOS类目 | Engineering, Aerospace |
项目资助者 | The research is supported by NSFC No. 51376165. We would like to thank Prof. Honghui Teng, from Institute of Mechanics CAS, for providing valuable comments on the analyze and help in the paper submission. |
课题组名称 | LHD激波与爆轰物理 |
论文分区 | 一类 |
力学所作者排名 | 3 |
引用统计 | |
文献类型 | 期刊论文 |
条目标识符 | http://dspace.imech.ac.cn/handle/311007/58680 |
专题 | 高温气体动力学国家重点实验室 |
通讯作者 | Zhang, YN (reprint author), Beijing Power Machinery Res Inst, State Key Lab Laser Prop & Applicat, Beijing 100074, Peoples R China. |
推荐引用方式 GB/T 7714 | Zhang YN,Gong JS,Wang T,et al. Numerical study on initiation of oblique detonations in hydrogen-air mixtures with various equivalence ratios[J]. AEROSPACE SCIENCE AND TECHNOLOGY,2016,49:130-134. |
APA | Zhang YN,Gong JS,Wang T,&Zhang, YN .(2016).Numerical study on initiation of oblique detonations in hydrogen-air mixtures with various equivalence ratios.AEROSPACE SCIENCE AND TECHNOLOGY,49,130-134. |
MLA | Zhang YN,et al."Numerical study on initiation of oblique detonations in hydrogen-air mixtures with various equivalence ratios".AEROSPACE SCIENCE AND TECHNOLOGY 49(2016):130-134. |
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