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| 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:417/0  |  提交时间:2018/12/26 |
| Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文 2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018 作者: Li B; Lee YC(李亚超); Yao W(姚卫); Lu Y(陆阳); Fan XJ(范学军) 浏览  |  Adobe PDF(1813Kb)  |  收藏  |  浏览/下载:307/82  |  提交时间:2018/12/26 |
| 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:489/104  |  提交时间:2018/12/26 |
| Prediction of kerosene properties at supercritical pressures by Artificial Neural Network 会议论文 2018 Joint Propulsion Conference, Cincinnati, Ohio., July 9-11, 2018 作者: Li B(李波); Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) 浏览  |  Adobe PDF(1813Kb)  |  收藏  |  浏览/下载:174/64  |  提交时间:2020/08/27 |
| 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:395/147  |  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:443/217  |  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 |
| 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 |
| 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) Adobe PDF(832Kb)  |  收藏  |  浏览/下载:276/82  |  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:428/92  |  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:475/173  |  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 |