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)![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() |
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
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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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