Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor
文献类型：会议论文
| 作者 | Zhong FQ(仲峰泉) ; Chen LH(陈立红); Chang XY(张新宇); Zhong FQ(仲峰泉)
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| 出版日期 | 2012 |
| 会议名称 | 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012 |
| 会议日期 | SEP 24-28, 2012 |
| 会议地点 | Tours, France |
| 通讯作者 | 仲峰泉 |
| 中文摘要 | In this paper, unsteady process of ignition of partially cracked kerosene in a Mach 2.5 supersonic model combustor was studied numerically. The reaction flow was solved with SST k-ω turbulence model and a kinetic mechanism of kerosene reduced from a detailed mechanism. Eddy dissipation concept is used to model the turbulence/chemistry interaction and In Situ adaptive tabulation algorithm applied for the acceleration of numerical integrations. Based on the present results, time evolutions of ignitions of partially cracked kerosene are described and the temporal and spatial changes of main radicals and products are provided. It is found that the pilot hydrogen supplies a radical pool of OH in the cavity that promotes the ignition of kerosene and stabilizes the flame. For the present flow and fuel conditions, ignition of partially cracked kerosene is completed at a physical time of approximately 5.6ms. However, for uncracked gaseous kerosene, the finish time of ignition is significantly longer. It is believed that the HCO radical formed by the oxidation of C2H4, one of the major products of kerosene cracking, attributes to the ignition acceleration for partially cracked kerosene. |
| 收录类别 | EI |
| 产权排序 | [Zhong Fengquan;Chen Lihong;Chang Xinyu] State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing, 100190, China |
| 会议主办者 | American Institute for Aeronautics and Astronautics (AIAA) |
| 会议录 | 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012
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| 会议录出版者 | AMER INST AERONAUT ASTRONAUT, RESTON |
| 语种 | 英语 |
| ISBN号 | 9781600869310 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/48283]  |
| 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 | Zhong FQ(仲峰泉) |
| 推荐引用方式 GB/T 7714 | Zhong FQ,Chen LH,Chang XY,et al. Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor[C]. 见:18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012. Tours, France. SEP 24-28, 2012. |
入库方式： OAI收割
来源：力学研究所
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