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| 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 Authors: 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)  |  Favorite  |  View/Download:416/88  |  Submit date: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 Authors: 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)  |  Favorite  |  View/Download:460/169  |  Submit date: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 |
| A comparative study of highly underexpanded nitrogen and hydrogenjets using large eddy simulation 会议论文 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015 Authors: Li XP(李晓鹏); Wu K(吴坤); Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(728Kb)  |  Favorite  |  View/Download:263/85  |  Submit date:2017/05/05 Comparative Studies Flow Charac Teristics High Order Harmonics High Resolution Instability Modes Near Field Structure Shock Structure Under Expanded Jets |
| Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet 会议论文 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015 Authors: Wu K(吴坤); Li XP(李晓鹏); Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(590Kb)  |  Favorite  |  View/Download:356/88  |  Submit date:2017/05/05 Frequency Spectrum Analysis High Temporal Resolution Instantaneous Flow Noise Generation Mechanisms Theoretical Modeling Three Dimensional Numerical Studies Transport Mechanism Under Expanded Jets |
| 超声速燃烧熄火极限实验研究 会议论文 第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28 Authors: 张泰昌; 袁越明; 范学军; 张鹏 View  |  Adobe PDF(625Kb)  |  Favorite  |  View/Download:346/70  |  Submit date:2016/08/16 熄火极限 超声速燃烧 凹腔 火焰稳定 层流火焰 化学发光 剪切层 隔离段 速度计算 总温 |
| 基于大庆RP-3航空煤油的轴对称截面燃烧室DES模拟 会议论文 第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28 Authors: 姚卫; 李晓鹏; 吴坤; 范学军 View  |  Adobe PDF(653Kb)  |  Favorite  |  View/Download:301/81  |  Submit date:2016/08/16 Des Rp-3 超声速燃烧 流场结构 航空煤油 点火过程 湍流模型 自由基浓度 热释放速率 预测分析 |
| 超声速燃烧稳焰模式分布研究 会议论文 第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28 Authors: 袁越明; 张泰昌; 范学军; 张鹏 View  |  Adobe PDF(625Kb)  |  Favorite  |  View/Download:270/65  |  Submit date:2016/08/16 火焰结构 超声速燃烧 凹腔 当量比 燃烧室内 火焰稳定 总温 一维性 隔离段 参数空间 |
| 超临界碳氢燃料供给系统的动态频域特性研究 会议论文 第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28 Authors: 刘文超; 肖雪峰; 刘祥灿; 周伟星; 范学军; 于达仁 View  |  Adobe PDF(621Kb)  |  Favorite  |  View/Download:345/82  |  Submit date:2016/08/16 燃料供给系统 再生冷却 超燃冲压发动机 频域特性 碳氢 动态特性参数 零维模型 供油系统 热沉 燃油加热 |