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Knowledge Management System of Institue of Mechanics, CAS
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IDDES method based on differential Reynolds-stress model and its application in bluff body turbulent flows
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 119, 页码: 13
Authors:
Wang, Gang
;
Li, Quanzheng
;
Liu Y(刘毅)
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Submit date:2022/06/11
Detached-eddy simulation
Reynolds-stress model
Massively separated flows
Tandem cylinders
Launch vehicle
Transonic buffet
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:
Li, Mengzhe
;
Wang, Zhikai
;
Xu, Rongguang
;
Zhang, Xiaoliang
;
Chen, Zhitong
;
Wang Q(汪球)
Adobe PDF(8841Kb)
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Submit date:2021/11/01
Non-equilibrium plasma
Plasma-assisted ignition
Plasma-assisted combustion
Aerospace engine
Combustor
Extreme condition
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
Reduction of surface friction drag in scramjet engine by boundary layer combustion
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:
Xue, Rui
;
Zheng, Xing
;
Yue LJ(岳连捷)
;
Zhang, Qian
;
He, Xin
;
Yang, Jing
;
Weng, Chao
;
Li, Zhihao
Adobe PDF(5483Kb)
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Submit date:2022/10/25
Boundary layer combustion
Skin-friction reduction
Supersonic combustion
Scramjet engine
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
Authors:
Wang KL(王宽亮)
;
Li F(李飞)
;
Zou PF(邹鹏飞)
;
Lin X(林鑫)
;
Mao RH(毛荣海)
;
Yu XL(余西龙)
Adobe PDF(2678Kb)
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Submit date:2020/03/21
Swirl flame
Heat release
Chemiluminescence
3D-CTC
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
Authors:
Wang KL(王宽亮)
;
Li F(李飞)
;
Zou PF(邹鹏飞)
;
Lin X(林鑫)
;
Mao RH(毛荣海)
;
Yu XL(余西龙)
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  |  
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Submit date:2020/03/21
Swirl flame
Heat release
Chemiluminescence
3D-CTC
Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 92, 页码: 676-684
Authors:
Fang YS(方宜申)
;
Zhang ZJ(张子健)
;
Hu ZM(胡宗民)
;
Deng, X
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View/Download:364/91
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Submit date:2019/10/21
Oblique detonation wave
Blunt wedge
Initiation
Hydrogen
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors:
Yue LJ(岳连捷)
;
Jia YN(贾轶南)
;
Xu X
;
Zhang XY(张新宇)
;
Zhang P(张鹏)
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Submit date:2018/10/30
Inlet restart
Cowl shock
Shock wave boundary layer interactions
Numerical investigation of the axial impulse load during the startup in the shock tunnel
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 332-342
Authors:
Meng BQ(孟宝清)
;
Han GL(韩桂来)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
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Submit date:2018/10/30
Hypersonic
Shock tunnel
Start-up process
Impulse force
Vibration