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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)
Favorite  |  View/Download：60/0  |  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  
Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023, 页码: 18
Authors:  Yao W(姚卫);  Liu H(刘杭);  Zhang Z(张政);  Zhang X(张旭);  Yue LJ(岳连捷);  Zhang XY(张晓源);  Li JP(李进平)
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Numerical study on wave configuration of wedge-induced oblique detonation wave: Reactive boundary layer effect 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 11, 页码: 11
Authors:  Yang L(杨理);  Yue LJ(岳连捷);  Yu, Dehai;  Chen, Zheng
Adobe PDF(4548Kb)  |  Favorite  |  View/Download：194/54  |  Submit date：2022/12/29
Onset of Oblique Detonation Waves for a Cavity-Based Wedge 期刊论文
AIAA JOURNAL, 2022, 页码: 14
Authors:  Yang, Li;  Yue LJ(岳连捷);  Zhang QF(张启帆)
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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)  |  Favorite  |  View/Download：306/75  |  Submit date：2021/11/15
Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
Adobe PDF(4108Kb)  |  Favorite  |  View/Download：347/56  |  Submit date：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
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)  |  Favorite  |  View/Download：166/50  |  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)  |  Favorite  |  View/Download：423/80  |  Submit date：2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
A COMPUTATIONAL MODEL FOR SPINNING EFFECTS ON POST-COLLISION VELOCITIES OF BOUNCING DROPLETS 期刊论文
ATOMIZATION AND SPRAYS, 2021, 卷号: 31, 期号: 10, 页码: 43-61
Authors:  He CM(何成明);  Yue LJ(岳连捷);  Zhang, Peng
Adobe PDF(4416Kb)  |  Favorite  |  View/Download：210/51  |  Submit date：2021/11/01
spinning droplets  droplet bouncing  post-collision characteristics  angular momentum  volume-of-fluid  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
Adobe PDF(3937Kb)  |  Favorite  |  View/Download：230/61  |  Submit date：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train