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| Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model 会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
作者: Yao W(姚卫) ; Chen L(陈留)
 Adobe PDF(2272Kb) |  收藏 | 浏览/下载：264/145 | 提交时间：2021/06/11 |
| Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Yao W(姚卫); Fan XJ(范学军)
 浏览 | Adobe PDF(623Kb) | 收藏 | 浏览/下载：263/90 | 提交时间：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| 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 |
| Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者: Yao W(姚卫); Fan XJ(范学军)
浏览 | Adobe PDF(832Kb) | 收藏 | 浏览/下载：275/82 | 提交时间：2018/11/08
Combustion Cost benefit analysis Costs Mixtures Ramjet engines Supersonic aircraft Computational costs Equivalence ratios Local flow conditions Scramjet combustors Statistics approaches Supersonic combustion Supersonic combustors Turbulent combustion |
| Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
作者: Lu Y(陆阳); Wang XZ(王新竹); Li L(李龙); Cheng D(程迪); Yuan T(袁涛); Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(445Kb) | 收藏 | 浏览/下载：427/92 | 提交时间：2016/01/08
Hydrocarbons Combustors Cooling Heat Transfer |
| 超声速燃烧室隔离段壁面热流的分析 会议论文
中国力学大会——2013, 中国北京, 2013-08-19
作者: 陈小平; 李新亮; 窦华书
浏览 | Adobe PDF(583Kb) | 收藏 | 浏览/下载：508/134 | 提交时间：2014/04/02
超声速燃烧 壁面热流 隔离段 平均热流 超燃 直接数值模拟 槽道湍流 网格分布 高雷诺数 计算域 格分辨率 误差:吻合的:0 |
| Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者: Xiao YB(肖雅彬); Yue LJ(岳连捷); Chen LH(陈立红); Zhang XY(张新宇); Xiao YB(肖雅彬)
浏览 | Adobe PDF(1674Kb) | 收藏 | 浏览/下载：431/112 | 提交时间：2014/02/24 |
| Modeling and measurements of heat release distributions in dual-mode scramjet combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
作者: Tian L(田璐); Chen LH(陈立红); Chen Q(陈强); Li F(李飞); Zhang XY(张新宇); Tian L(田璐)
浏览 | Adobe PDF(677Kb) | 收藏 | 浏览/下载：615/195 | 提交时间：2014/02/24 |
