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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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Indexed By:SCI
Date Issued:2024
Funding Organization:National Natural Science Foundation of China
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Experimental study on shock interaction control of double wedge in high-enthalpy hypersonic flow subject to plasma synthetic jet
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2024, 卷号: 37, 期号: 4, 页码: 151-165
Authors:
Xie, Xuzhen
;
Liu, Qiang
;
Zhou, Yan
;
Luo, Zhenbing
;
Xie, Wei
;
Bai, Guanghui
;
Luo, Kai
;
Wang, Qiu
;
Wu, Jianjun
Favorite
  |  
View/Download:10/0
  |  
Submit date:2024/06/11
Hypersonic flow
High-enthalpy flow
Plasma synthetic jet
Shock wave
Flow control
Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet
期刊论文
JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17
Authors:
Liu H(刘杭)
;
Yao W(姚卫)
;
Zhang X(张旭)
;
Zhang XY(张晓源)
;
Liu, Jianwen
;
Yue LJ(岳连捷)
;
Sun QH(孙泉华)
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  |  
View/Download:56/0
  |  
Submit date:2024/03/11
Scramjet
Dynamic Zone Flamelet Model
High Enthalpy Shock Tunnel
Combustors
Improved Delayed Detached Eddy Simulation
Vibrational Energy
nonequilibrium heating
cooling effects
thermal nonequilibrium
chemical nonequilibrium
hydrogen
Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities
期刊论文
AIAA JOURNAL, 2024, 页码: 8
Authors:
Wang WT(王文韬)
;
Wang Q(汪球)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Gao, Liangjie
;
Liu, Zhongchen
;
Qian, Zhansen
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  |  
View/Download:76/0
  |  
Submit date:2024/02/26
Finite Element Method
Hypersonic
Shock Tube/Tunnel
Diaphragm
Burst Pressure