| The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability | |
Jia YN(贾轶南); Yue LJ(岳连捷) ; Zhang XY(张新宇); Jia, Yinan([email protected])
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| Source Publication | 21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017 |
| 2017 | |
| Conference Name | 21st AIAA International Space Planes and Hypersonics Technologies Conference |
| Conference Date | 6-9 March 2017 |
| Conference Place | Xiamen, China |
| Abstract | Wind tunnel experiments and numerical calculations were conducted to investigate the influence of several key factors on self-starting capability. The changes of maximum ICR with cowl shock strength, boundary layer thickness and wall temperature were explored and the sudden change of inlet self-starting capability was observed during a certain range of these influencing factors. A transitional phenomenon was obtained in both experiments and numerical simulations. It is found that the sudden changes of inlet self-starting capability with boundary layer thickness and wall temperature take place with a wide domain of transitional phenomenon. 漏 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved. |
| Keyword | Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
| ISBN | 978-1-62410-463-3 |
| Indexed By | EI |
| Language | 英语 |
| Document Type | 会议论文 |
| Identifier | http://dspace.imech.ac.cn/handle/311007/72195 |
| Collection | 高温气体动力学国家重点实验室 |
| Corresponding Author | Jia, Yinan([email protected]) |
| Affiliation | 1.Institute of Mechanics, Chinese Academy of Sciences, No.15 Beisihuanxi Road, Beijing 2.100190, China |
| Recommended Citation GB/T 7714 | Jia YN,Yue LJ,Zhang XY,et al. The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability[C]21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017,2017. |
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| File Name/Size | DocType | Version | Access | License | ||
| Cp-2017-040.pdf（566KB） | 会议论文 | 开放获取 | CC BY-NC-SA | View Download | ||
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