IMECH-IR  > 高温气体动力学国家重点实验室
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(yuelj@imech.ac.cn)
Source Publication21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
2017
Conference Name21st AIAA International Space Planes and Hypersonics Technologies Conference
Conference Date6-9 March 2017
Conference PlaceXiamen, 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.

KeywordBoundary Layer Flow Boundary Layers Spacecraft Wind Tunnels
ISBN978-1-62410-463-3
Indexed ByEI
Language英语
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/72195
Collection高温气体动力学国家重点实验室
Corresponding AuthorJia, Yinan(yuelj@imech.ac.cn)
Affiliation1.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]. USA:American Institute of Aeronautics and Astronautics Inc, AIAA,2017.
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