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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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吴坤 [6]
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姚卫 [5]
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Indexed By:EI
Creator:吴坤
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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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Submit date:2022/01/24
Supersonic combustion
Jet-wake flame stabilization
Hybrid LES
RANS
Detailed hydrogen chemistry
Counter-rotating vortex pair
Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor
期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 卷号: 37, 期号: 3, 页码: 3685-3692
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2018/12/27
Supersonic combustion
Flame stabilization mode
DLR Strut injection scheme
Stagnation Temperature
Overall equivalence ratio
On the application of tabulated dynamic adaptive chemistry in ethylene-fueled supersonic combustion
期刊论文
COMBUSTION AND FLAME, 2018, 卷号: 197, 页码: 265-275
Authors:
Wu K(吴坤)
;
Contino F
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2018/12/12
Tabulated dynamic adaptive chemistry
Skeletal mechanism
Supersonic combustion
Ethylene
Large Eddy Simulation
Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion
期刊论文
ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350
Authors:
Yao W(姚卫)
;
Wu K(吴坤)
;
Fan XJ(范学军)
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Submit date:2018/12/27
Combustion Condition
Combustor Efficiency
Improved Delayed Detached Eddy Simulations
Initial Temperatures
Laminar Flame Speed
Scramjet Combustors
Supersonic Combustion
Turbulence-chemistry Interactions
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
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Submit date:2018/01/16
Combustion
Diesel Engines
Hydrogen
Large Eddy Simulation
Spacecraft
Stabilization
Supersonic Aircraft
Temperature Measurement
Wall Flow
Numerical Investigation on Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 12, 页码: 2154-2179
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang, P (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong 999077, Hong Kong, Peoples R China.
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Submit date:2017/12/18
Detailed Hydrogen Oxidation Mechanism
Dlr
Flame Stabilization
Sensitivity Analysis
Supersonic Combustion