Performance of a detonation driven shock tunnel
文献类型：会议论文
| 作者 | Li JW ; Wang Q(汪球); Zhao W(赵伟); Lu P; Tan YX
|
| 出版日期 | 2017 |
| 会议日期 | 6-9 March 2017 |
| 会议地点 | Xiamen, China |
| 关键词 | Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |
| 英文摘要 | Because of the high costs of flight tests, ground test facilities are a necessity in hypersonic flow research. Compared with other impulse facilities, shock tunnels show their advantages in relatively large-size models and low operational costs. To continuously improve the capacities of shock tunnels, a new detonation-driven shock tunnel was developed in the Laboratory of High Temperature Gas Dynamics (LHD), Institute of Mechanics, Chinese Academy of Sciences. In this paper, performance of the detonation-driven shock tube is investigated, with the help of numerical calculation. Some key issues, including the filling of the gases, pressure loss caused by diaphragm rupture, and the nearly tailored status are discussed in detail. 漏 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. |
| 会议录 | 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
 |
| 会议录出版者 | American Institute of Aeronautics and Astronautics Inc, AIAA |
| 会议录出版地 | USA |
| 语种 | 英语 |
| URL标识 | 查看原文 |
| ISBN号 | 978-1-62410-463-3 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/72191]  |
| 专题 | 力学研究所_高温气体动力学国家重点实验室 |
| 作者单位 | 1.School of Chemical and Environmental Engineering, North University of China, No.3 XueYuan road, Taiyuan 2.051, China (2) State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, No.15 Beisihuanxi Road, Beijing 3.100190, China |
| 推荐引用方式 GB/T 7714 | Li JW,Wang Q,Zhao W,et al. Performance of a detonation driven shock tunnel[C]. 见:. Xiamen, China. 6-9 March 2017. |
入库方式： OAI收割
来源：力学研究所
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