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Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
Language:英语
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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)
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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
Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors:
Zhang ZJ(张子健)
;
Ma KF(马凯夫)
;
Zhang WS(张文硕)
;
Han X(韩鑫)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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Submit date:2020/11/30
Oblique detonation engine
Pre-injection
Detonative combustion
Mixing
Hydrogen
Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors:
Luo K(罗凯)
;
Wang Q(汪球)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2023Kb)
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Submit date:2020/11/30
Quasi-one-dimensional
Detonation
Shock tunnel
Shock speed
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
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