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Source Publication：AEROSPACE SCIENCE AND TECHNOLOGY
Funding Organization：National Natural Science Foundation of China
Funding Project：National Natural Science Foundation of China[11672308]
Community：高温气体动力学国家重点实验室
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Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors:
Luo K(罗凯)
;
Wang Q(汪球)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2023Kb)
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View/Download：326/104
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Submit date：2020/11/30
Quasi-one-dimensional
Detonation
Shock tunnel
Shock speed
A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors:
Peng J(彭俊)
;
Zhang ZJ(张子健)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
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Adobe PDF(2165Kb)
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View/Download：411/94
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Submit date：2019/09/09
Shock reflection
Vibration excitation
Mach reflection
Transition criterion
Hypersonic flow
