The Role of Three-Dimensional Shock Wave Interaction in the Complex Hypersonic Heating | |
Wang C(王春); Xiang GX(项高翔); Jiang ZL(姜宗林); Li XD(李旭东); Shi CM(师曾敏) | |
Source Publication | 31st International Symposium on Shock Waves 2 |
2019-03-22 | |
Pages | 905-910 |
Conference Name | 31st International Symposium on Shock Waves |
Conference Date | 2017-07-9~14 |
Conference Place | Nagoya, Japan |
Abstract | A shock-expansion tube/tunnel is a ground-based test facility to generate hypervelocity test flows for the study of atmospheric reentry physics. Such a high enthalpy test flow features thermochemically non-equilibrium which may lead to critical difficulties in flow diagnostics and measurements. In addition, the test time of such an impulse facility is extremely short which implies a requirement of transducers with high-frequency response capability for model tests or flow diagnostics. In the present work, computations for non-equilibrium reacting flow are conducted to diagnose the key flow parameters and evaluate the test flow for facility upgrading. A conic nozzle is appended to the original facility and to obtain a larger test section and larger Mach numbers. Further experiments are conducted to visualize the overall flow structures over the test models by self-illumination of radicals at high-energy states post strong shock waves. The heat flux at the stagnation point is measured with specially designed thermal couples. |
ISBN | 978-3-319-91017-8 |
Language | 英语 |
Document Type | 会议论文 |
Identifier | http://dspace.imech.ac.cn/handle/311007/80808 |
Collection | 高温气体动力学国家重点实验室 |
Recommended Citation GB/T 7714 | Wang C,Xiang GX,Jiang ZL,et al. The Role of Three-Dimensional Shock Wave Interaction in the Complex Hypersonic Heating[C]31st International Symposium on Shock Waves 2,2019:905-910. |
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Cp2019059.pdf(376KB) | 会议论文 | 开放获取 | CC BY-NC-SA | View Download |
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