LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection | |
Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk) | |
会议录名称 | 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017 |
2017 | |
会议名称 | 21st AIAA International Space Planes and Hypersonics Technologies Conference |
会议日期 | 6-9 March 2017 |
会议地点 | Xiamen, China |
摘要 | Supersonic combustion in the hydrogen fueled DLR model scramjet combustor was computationally investigated by using Large Eddy Simulation (LES) combined with the latest detailed reaction mechanism for hydrogen combustion. Two computational models were employed including a two-dimensional reduced model and a three-dimensional model with periodicity in the spanwise direction. The two-dimensional model was fully validated against the three-dimensional model and the experimental data for the wall pressure measurements and the axial velocity under non-reacting flow condition. For reacting flow, the present model shows good agreement with the experimental axial velocity and static temperature measurements. Furthermore, radical evolution and heat release analysis were conducted both qualitatively and quantitatively to reveal the flame stabilization mechanism in the DLR combustor. The results show that the combustion is characterized by a three-stage combustion mode, namely induction, radical transportation and intense turbulent combustion stages. 漏 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. |
关键词 | Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
ISBN号 | 978-1-62410-463-3 |
URL | 查看原文 |
收录类别 | EI |
语种 | 英语 |
文献类型 | 会议论文 |
条目标识符 | http://dspace.imech.ac.cn/handle/311007/72188 |
专题 | 高温气体动力学国家重点实验室 |
通讯作者 | Zhang, Peng(pengzhang.zhang@polyu.edu.hk) |
作者单位 | 1.Department of Mechanical Engineering, Hong Kong Polytechnic University, Hong Kong (2) State Key Laboratory of High Temperature Gas Dynamics, Chinese Academy of Sciences, Beijing 2.190, China (3) School of Engineering Science, University of Chinese Academy of Science, Beijing 3.100049, China |
推荐引用方式 GB/T 7714 | Wu K,Zhang P,Yao W,et al. LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection[C]21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,2017. |
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