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Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 124, 页码: 17
Authors:
Dai, Chunliang
;
Sun, Bo
;
Zhuo, Changfei
;
Zhou, Shengbing
;
Zhou, Changsheng
;
Yue LJ(岳连捷)
Adobe PDF(6822Kb)
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Submit date:2022/07/18
Hypervelocity double-wedge flow
High temperature non-equilibrium effects
Laminar and turbulence flow
Shock wave interaction
Shock wave
boundary layer interaction
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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View/Download:302/111
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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
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)
Adobe PDF(2853Kb)
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Submit date:2021/05/17
Oblique detonation
Wave complex
Instability
Thermal choking
Expansion corner
Numerical study on the shock/combustion interaction of oblique detonation waves
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
Authors:
Yang L
;
Yue LJ(岳连捷)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
Adobe PDF(5176Kb)
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Submit date:2020/11/30
Oblique detonation wave
Shock/combustion interaction
Shock polar analysis
High-resolution simulation
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
DNS analysis of the effects of combustion on turbulence in a supersonic H2/air jet flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 93, 页码: 9
Authors:
Fu YW(符耀威)
;
Yu ZP(于长平)
;
Yan Z(闫正)
;
Li XL(李新亮)
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View/Download:428/155
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Submit date:2020/03/21
Supersonic combustion
Turbulence jet
Direct numerical simulations
Coherent structures
The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
Authors:
Li HX(李慧鑫)
;
Ye L(叶亮)
;
Wei XL(魏小林)
;
Li T(李腾)
;
Li S(李森)
;
Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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View/Download:515/221
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Submit date:2017/12/18
H2o2/kerosene Bipropellant
Coaxial-swirl Injector
Geometric Constant
Performance