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Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
Community:高温气体动力学国家重点实验室
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On jet-wake flame stabilization in scramjet: A LES/RANS study from chemical kinetic and fluid-dynamical perspectives
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 120, 页码: 12
Authors:
Wu K(吴坤)
;
Zhang, Peng
;
Fan XJ(范学军)
Adobe PDF(3834Kb)
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View/Download:351/55
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Submit date:2022/01/24
Supersonic combustion
Jet-wake flame stabilization
Hybrid LES
RANS
Detailed hydrogen chemistry
Counter-rotating vortex pair
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
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)
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
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
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
Authors:
Wang KL(王宽亮)
;
Li F(李飞)
;
Zou PF(邹鹏飞)
;
Lin X(林鑫)
;
Mao RH(毛荣海)
;
Yu XL(余西龙)
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Submit date:2020/03/21
Swirl flame
Heat release
Chemiluminescence
3D-CTC
Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
Authors:
Wang KL(王宽亮)
;
Li F(李飞)
;
Zou PF(邹鹏飞)
;
Lin X(林鑫)
;
Mao RH(毛荣海)
;
Yu XL(余西龙)
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  |  
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View/Download:220/72
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Submit date:2020/03/21
Swirl flame
Heat release
Chemiluminescence
3D-CTC
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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Submit date:2020/03/21
Supersonic combustion
Turbulence jet
Direct numerical simulations
Coherent structures
Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263
Authors:
Fang YS(方宜申)
;
Hu ZM(胡宗民)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Ng HD
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View/Download:393/99
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Submit date:2018/02/08
Oblique Detonation
Equivalence Ratio
Mixture Inhomogeneity
Detailed Chemistry
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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Submit date:2017/12/18
H2o2/kerosene Bipropellant
Coaxial-swirl Injector
Geometric Constant
Performance