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| Numerical investigation on the performance of bluff body augmented micro cavity-combustor 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 7, 页码: 4932-4945
作者: Zhang Z; Wu K(吴坤); Yuen R; Yao W(姚卫) ; Wang J
 浏览 |  Adobe PDF(3438Kb) |  收藏 | 浏览/下载：309/108 | 提交时间：2020/04/07
Micro combustor Cavity Bluff body Combustion efficiency Local Damkohler number |
| 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
作者: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军)
浏览 | Adobe PDF(1820Kb) | 收藏 | 浏览/下载：454/154 | 提交时间：2018/12/27
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
作者: Yao W(姚卫); Wu K(吴坤); Lee YC(李亚超); Fan XJ(范学军)
 Adobe PDF(1156Kb) | 收藏 | 浏览/下载：414/0 | 提交时间：2018/12/26 |
| 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
作者: Wu K(吴坤); Contino F; Yao W(姚卫); Fan XJ(范学军)
浏览 | Adobe PDF(4270Kb) | 收藏 | 浏览/下载：516/178 | 提交时间：2018/12/12
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
作者: 吴坤
Adobe PDF(18227Kb) | 收藏 | 浏览/下载：725/24 | 提交时间：2018/05/22
超声速燃烧 支板稳焰 凹腔稳焰 简化机理 动态自适应化学 |
| 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
作者: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
浏览 | Adobe PDF(1249Kb) | 收藏 | 浏览/下载：300/89 | 提交时间：2018/01/16
Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
