Research progress on high-enthalpy and hypersonic flows
文献类型:会议论文
作者 | Jiang ZL(姜宗林)![]() ![]() ![]() |
出版日期 | 2007 |
会议名称 | 5th International Conference on Fluid Mechanics |
会议日期 | AUG 15-19, 2007 |
会议地点 | Shanghai, PEOPLES R CHINA |
关键词 | Hypersonic Flows Detonation Driver Shock-Reflected Tunnels Shock-Expanded Tube Heat Transfer |
页码 | 37-44 |
通讯作者 | Jiang Z |
中文摘要 | The research progress on high-enthalpy and hypersorlic flows having been achieved in the Institute of Mechanics, Chinese Academy of Sciences, is reported in this paper. The paper consists of three main parts: The first part is on the techniques to develop advanced hypersonic test facilities, in which the detonation-driven shock-reflected tunnel and the detonation-driven shock-expanded tube are introduced. The shock tunnel can be used for generating hypersonic flows of a Mach number ranging from 10 to 20, and the expansion tube is applicable to simulate the flows with a speed of 7 similar to 10km/s. The second part is dedicated to the shock tunnel nozzle flow diagnosis to examine properties of the hypersonic flows thus created. The third part is on experiments and numerical simulations. The experiments include measuring the aerodynamic pitching moment and heat transfer in hypersonic flows, and the numerical work reports nozzle flow simulations and flow non-equilibrium effects on the possible experiments that may be carried out on the above-mentioned hypersonic test facilities. |
收录类别 | CPCI-S |
会议录 | New Trends In Fluid Mechanics Research - Proceedings Of The Fifth International Conference On Fluid Mechanics
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会议录出版者 | Beijing |
会议录出版地 | Tsinghua University Press |
语种 | 英语 |
ISSN号 | 978-7-302-15894-3 |
WOS记录号 | WOS:000254042000007 |
源URL | [http://dspace.imech.ac.cn/handle/311007/25444] ![]() |
专题 | 力学研究所_力学所知识产出(1956-2008) |
推荐引用方式 GB/T 7714 | Jiang ZL,Yu HR,Lin ZB. Research progress on high-enthalpy and hypersonic flows[C]. 见:5th International Conference on Fluid Mechanics. Shanghai, PEOPLES R CHINA. AUG 15-19, 2007. |
入库方式: OAI收割
来源:力学研究所
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