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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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Supersonic combustion  Flame stabilization mode  DLR Strut injection scheme  Stagnation Temperature  Overall equivalence ratio  
Influence of Chemical Mechanisms on Supersonic Combustion Characteristics Fueled by Kerosene 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018
Authors:  Yao W(姚卫);  Wu K(吴坤);  Lee YC(李亚超);  Fan XJ(范学军)
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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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Tabulated dynamic adaptive chemistry  Skeletal mechanism  Supersonic combustion  Ethylene  Large Eddy Simulation  
超声速燃烧室火焰稳定模式与化学反应机理简化研究 学位论文
博士论文,北京: 中国科学院大学, 2018
Authors:  吴坤
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超声速燃烧  支板稳焰  凹腔稳焰  简化机理  动态自适应化学  
Numerical study on supersonic combustion of hydrogen and its mixture with Ethylene and methane with strut injection 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2018, 卷号: 43, 期号: 15, 页码: 7591-7599
Authors:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇)
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Detached Eddy Simulation  Reduced Kinetic Mechanism  Supersonic Combustion  Hydrogen  Hydrocarbon  
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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Combustion Condition  Combustor Efficiency  Improved Delayed Detached Eddy Simulations  Initial Temperatures  Laminar Flame Speed  Scramjet Combustors  Supersonic Combustion  Turbulence-chemistry Interactions  
Development and Fidelity Evaluation of a Skeletal Ethylene Mechanism under Scramjet-Relevant Conditions 期刊论文
ENERGY & FUELS, 2017, 卷号: 31, 期号: 12, 页码: 14296
Authors:  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军);  Yao, W;  Fan, XJ
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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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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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Detailed Hydrogen Oxidation Mechanism  Dlr  Flame Stabilization  Sensitivity Analysis  Supersonic Combustion  
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军)
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Adiabatic Flame Temperature  Combustion  Directed Graphs  Flow Separation  Heat Flux  Kerosene  Large Eddy Simulation  Musculoskeletal System  Real Time Systems  Sensitivity Analysis  Spacecraft  Transients