Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism
文献类型：期刊论文
| 作者 | Zhong FQ(仲峰泉) ; Chen LH(陈立红); Li F(李飞); Zhang XY(张新宇); Sung CJ
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| 刊名 | COMBUSTION SCIENCE AND TECHNOLOGY
 |
| 出版日期 | 2013-04-03 |
| 卷号 | 185期号:4页码:548-563 |
| 通讯作者邮箱 | fzhong@imech.ac.cn |
| 关键词 | Ethylene Ignition Numerical simulation Reduced kinetic mechanism Supersonic combustion |
| ISSN号 | 0010-2202 |
| 产权排序 | [Zhong, Fengquan; Chen, Lihong; Li, Fei; Zhang, Xinyu] Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China; [Sung, Chih-Jen] Univ Connecticut, Storrs, CT USA |
| 通讯作者 | Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China. |
| 合作状况 | 国际 |
| 中文摘要 | The unsteady process of ignition and combustion of ethylene at varied fuel/air equivalence ratios in a Mach 2.5 supersonic model combustor is studied numerically. The reacting turbulent flow is solved using the shear stress transport (SST) k-ω turbulence model and a reduced kinetic mechanism obtained with sensitivity analysis and the assumption of quasi-steady-state from a detailed mechanism of ethylene. The present results reveal that ignition of ethylene first takes place in the cavity due to the local low speed and high static temperature. At a low equivalence ratio of 0.32, combustion is established and stabilized downstream of the cavity. However, as the equivalence ratio increases to 0.6, the combustion downstream of the cavity generates sufficient heat release to cause pressure and the flame to propagate upstream and to generate a shock train upstream of the injection point. Formation of the shock structure results in subsonic flow in the vicinity of the injection and combustion with higher efficiency stabilized mainly in the fuel/air mixing shear layer. The time evolutions of fuel jet and C2H2 qualitatively agree well with the experimental results, of which high-speed schlieren photos and chemiluminescence images of CH* are obtained at similar flow conditions. |
| 学科主题 | 计算流体力学 |
| 分类号 | 二类 |
| 收录类别 | SCI ; EI |
| 资助信息 | Natural Science Foundation of China [10921062, 11172309]; China's Programme of Introducing Talents of Discipline to Universities-111 Project [B08009]; Thousand Talents Program |
| 原文出处 | http://dx.doi.org/10.1080/00102202.2012.730080 |
| 语种 | 英语 |
| WOS记录号 | WOS:000316780400002 |
| 公开日期 | 2013-05-03 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/47192]  |
| 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 | Zhong FQ,Chen LH,Li F,et al. Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism[J]. COMBUSTION SCIENCE AND TECHNOLOGY,2013,185(4):548-563. |
| APA | 仲峰泉,陈立红,李飞,张新宇,&Sung CJ.(2013).Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism.COMBUSTION SCIENCE AND TECHNOLOGY,185(4),548-563. |
| MLA | 仲峰泉,et al."Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism".COMBUSTION SCIENCE AND TECHNOLOGY 185.4(2013):548-563. |
入库方式： OAI收割
来源：力学研究所
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