中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Characteristics of supersonic combustion with Hartmann-Sprenger tube aided fuel injection

文献类型:会议论文

作者Gu HB(顾洪斌); Li Z(李智); Li F(李飞); Chen LH(陈立红); Gu SL(顾声龙); Zhang XY(张新宇); Gu HB(顾洪斌); Gu HB(顾洪斌); Gu HB(顾洪斌)
出版日期2011
会议名称17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference
会议日期APR 11-14, 2011
会议地点San Francisco, CA, United states
通讯作者邮箱guhb@imech.ac.cn
页码AIAA 2011-2326
通讯作者顾洪斌
中文摘要The TDLAS and static pressure were used to investigate the combustion of the excited ethylene jet into the supersonic flow in this article. The jet was from the Hartmann-Sprenger tube, which was put into the traditional jet device. The jet was excited at three different frequencies and compared with the base case without excitation. The results showed that the higher static pressure could be obtained in the excited cases. The excited jet didn't only take effects on the jet shear layer, but also influenced the turbulence intensity near field, and the right excited frequency can short the mixing and combusting distance. The excited jet can help reduce the combustor length.
收录类别EI
产权排序[Gu, Hongbin;Li, Zhi; Li, Fei;Chen, Lihong;Gu, Shenglong;Chang Xinyu] Key Lab of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China
会议主办者American Institute of Aeronautics and Astronautics (AIAA)
会议网址http://dx.doi.org/10.2514/6.2011-2326
会议录17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2011
会议录出版者AMER INST AERONAUT ASTRONAUT, RESTON
语种英语
ISBN号978-1-60086-942-6
源URL[http://dspace.imech.ac.cn/handle/311007/48285]  
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Gu HB(顾洪斌); Gu HB(顾洪斌); Gu HB(顾洪斌)
推荐引用方式
GB/T 7714
Gu HB,Li Z,Li F,et al. Characteristics of supersonic combustion with Hartmann-Sprenger tube aided fuel injection[C]. 见:17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco, CA, United states. APR 11-14, 2011.http://dx.doi.org/10.2514/6.2011-2326.

入库方式: OAI收割

来源:力学研究所

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