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| Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文 2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018 作者: Wang Y; Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(1120Kb)  |  收藏  |  浏览/下载:488/104  |  提交时间:2018/12/26 |
| Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017 作者: Yao W(姚卫); Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶); Wu K(吴坤); Fan XJ(范学军) 浏览  |  Adobe PDF(805Kb)  |  收藏  |  浏览/下载:393/147  |  提交时间:2018/06/06 |
| A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 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); Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶); Fan XJ(范学军); Fan, Xuejun(xfan@imech.ac.cn) 浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载:441/217  |  提交时间:2018/01/16 Adiabatic Flame Temperature Aerodynamics Boundary Layer Flow Boundary Layers Chemical Analysis Combustion Computational Chemistry Directed Graphs Flow Separation Mach Number Principal Component Analysis Regression Analysis Sensitivity Analysis Spacecraft Supersonic Aerodynamics Supersonic Aircraft Transients |
| Experimental Studies of Film Cooling in Supersonic Combustors 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Fan C(樊川); Wang J(王晶); Fan XJ(范学军) 浏览  |  Adobe PDF(735Kb)  |  收藏  |  浏览/下载:310/102  |  提交时间:2018/01/16 Combustion Combustors Coolants Kerosene Spacecraft Supersonic Aerodynamics |
| Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor 会议论文 32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016 作者: Cheng D(程迪); Wang J(王晶); Gong J; Lu Y(陆阳); Yao W(姚卫); Li L(李龙); Fan XJ(范学军); Fan, Xuejun (xfan@imech.ac.cn) 浏览  |  Adobe PDF(2131Kb)  |  收藏  |  浏览/下载:322/123  |  提交时间:2017/05/05 Equivalence Ratios Heat Flux Distributions Heat Transfer Characteristics Scramjet Supercritical Kerosenes Supersonic Combustion Supersonic Combustors Total Temperatures |
| 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 |
| 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 作者: Yao W(姚卫); Wang J(王晶); Lu Y(陆阳); Li XP(李晓鹏); Fan XJ(范学军) Adobe PDF(1195Kb)  |  收藏  |  浏览/下载:474/173  |  提交时间:2016/07/01 Adiabatic Flame Temperature Combustion Directed Graphs Flow Separation Heat Flux Kerosene Large Eddy Simulation Musculoskeletal System Real Time Systems Sensitivity Analysis Spacecraft Transients |
| 同步辐射单光子电离技术研究航空煤油替代燃料环烷烃的热解反应 会议论文 中国力学大会——2013, 中国北京, 2013-08-19 作者: 王晶; 范学军; 王占东; 蔡江淮; 张李东; 齐飞 浏览  |  Adobe PDF(384Kb)  |  收藏  |  浏览/下载:597/165  |  提交时间:2014/04/02 单光子电离 同步辐射 替代燃料 环烷烃 航空煤油 热解反应 光电离效率谱 技术研究 分子束质谱 超声速燃烧 热解炉 环己烷 真空紫外 热解过程 光子能量 碳氢燃料 热解模型 两种模式 热解机理 分布情况 |
| Blowout limits of supercritical kerosene in supersonic combustors 会议论文 49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United states, JUL 14-17, 2013 作者: Zhang TC(张泰昌); Wang J(王晶); Yuan YM(袁越明); Li JG(李建国); Yu G(俞刚); Fan XJ(范学军); Zhang TC(张泰昌) 浏览  |  Adobe PDF(619Kb)  |  收藏  |  浏览/下载:587/187  |  提交时间:2014/02/24 |
| 主动冷却超燃冲压发动机燃烧室内流道设计 会议论文 高超声速研讨会暨第五届全国高超声速科学技术会议, 中国广西桂林, 2012-11-12 作者: 张泰昌; 王晶; 范学军 浏览  |  Adobe PDF(60Kb)  |  收藏  |  浏览/下载:666/198  |  提交时间:2014/04/02 超燃冲压发动机 燃烧室 主动冷却 超声速燃烧 流道设计 超临界态 火焰稳定 扩张角 喷注 发动机不起动 隔离段 直联式 发动机性能 贫油 燃烧效率 燃烧强度 向上游 进气道 释热 流量分配 |