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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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姜宗林 [3]
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Funding Project:National Natural Science Foundation of China[11672308]
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Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
Adobe PDF(1129Kb)
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View/Download:365/179
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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
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:371/114
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Submit date:2020/11/30
Quasi-one-dimensional
Detonation
Shock tunnel
Shock speed
Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel
期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(1471Kb)
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View/Download:283/63
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Submit date:2020/07/06
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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View/Download:436/102
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Submit date:2019/09/09
Shock reflection
Vibration excitation
Mach reflection
Transition criterion
Hypersonic flow