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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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Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
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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)
Adobe PDF(4661Kb)
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Submit date:2022/06/11
Detached-eddy simulation
Reynolds-stress model
Massively separated flows
Tandem cylinders
Launch vehicle
Transonic buffet
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)
Adobe PDF(8067Kb)
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Aerodynamic principles of shock-induced combustion ramjet engines
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
Authors:
Ma KF(马凯夫)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(1657Kb)
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Submit date:2020/08/26
Scramjet engines
Shock-induced combustion ramjet engines
Supersonic combustion
Chapman-Jouguet detonation
Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:
Zhang X(张旭)
;
Yue LJ(岳连捷)
;
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
Adobe PDF(3862Kb)
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Submit date:2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
Numerical study of a fully confined supersonic slot impinging jet from bleed system
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Chang XY(张新宇)
Adobe PDF(3918Kb)
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Submit date:2019/09/09
Fully confined supersonic jet
Inclined impingement
Heat transfer
Boundary layer bleed
Numerical simulation
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors:
Wang ZP(王知溥)
;
Li F(李飞)
;
Gu HS
;
Yu XL(余西龙)
;
Zhang XY(张新宇)
;
Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1112Kb)
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Submit date:2015/06/12
Scramjet
Dual-mode Combustor
Divergent Angle
Cavity Location
Combustion Efficiency
Tdlas
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Tong YG(仝颖刚)
;
Shen Y(沈岩)
;
Chen J(陈健)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1235Kb)
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Submit date:2013/07/30
Scramjet
Kerosene Fuel
Plasma Torch
Ignition