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Indexed By:EI
Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
Document Type:期刊论文
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Numerical studies of flow patterns and fuel distribution of tandem-arranged multi jets in a hypersonic crossflow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 139, 页码: 108383
Authors:
Wang JL(王嘉麟)
;
Han GL(韩桂来)
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Submit date:2023/07/17
Hypersonic flow
Tandem -arranged jets
Streamline pattern
Vortex structure
Fuel -air mixing
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
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
Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 112, 页码: 9
Authors:
Wang KL(王宽亮)
;
Yang PF(杨鹏飞)
;
Teng HH(滕宏辉)
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Submit date:2021/05/17
Oblique detonation
Wave complex
Instability
Thermal choking
Expansion corner
Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260
Authors:
Zhang W
;
Wang S
;
Wang Q
;
Ju SJ(鞠胜军)
;
Yan C
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Submit date:2021/02/09
Aerodynamic thermal
Opposing jets
Parametric sensitivity analysis
Uncertainty quantification
Analysis of Variance
Non-Intrusive Polynomial Chaos
Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10
Authors:
Ju SJ(鞠胜军)
;
Sun ZX(孙振旭)
;
Yang GW(杨国伟)
;
Prapamonthon P
;
Zhang JY
Adobe PDF(3818Kb)
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Submit date:2020/11/30
Optimization design
Drag reduction
Supersonic flow
Energy deposition
Opposing jet
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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Submit date:2019/10/21
Oblique detonation wave
Blunt wedge
Initiation
Hydrogen
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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Submit date:2019/09/09
Shock reflection
Vibration excitation
Mach reflection
Transition criterion
Hypersonic flow
Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781
Authors:
Zhong FQ(仲峰泉)
;
Cheng LW(程柳维)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
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Submit date:2019/05/29
Supersonic combustor
Hydrocarbon
Mixture fuel
Flame structure
Ignition
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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Adobe PDF(1937Kb)
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Submit date:2018/10/30
Hypersonic
Shock tunnel
Start-up process
Impulse force
Vibration