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| A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文 AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日 Authors: Jin YC(靳一超); Wu K(吴坤); Lu Y(陆阳); Fan XJ(范学军) Adobe PDF(1121Kb)  |  Favorite  |  View/Download:190/51  |  Submit date:2022/07/04 |
| Full-scale Improved Delayed Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文 2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018 Authors: Fan E; Wu K(吴坤); Lee YC(李亚超); Yao W(姚卫); Fan XJ(范学军) Adobe PDF(567Kb)  |  Favorite  |  View/Download:366/108  |  Submit date: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 Authors: 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) Adobe PDF(805Kb)  |  Favorite  |  View/Download:430/165  |  Submit date: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 Authors: 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) Adobe PDF(1173Kb)  |  Favorite  |  View/Download:487/235  |  Submit date: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 Authors: Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(623Kb)  |  Favorite  |  View/Download:303/107  |  Submit date:2018/01/16 Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| Full Scale Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文 53rd AIAA/SAE/ASEE Joint Propulsion Conference , Atlanta, GA., 10-12 July 2017 Authors: Fan E; Wu K(吴坤); Lee YC; Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(2297Kb)  |  Favorite  |  View/Download:288/122  |  Submit date:2018/01/16 |
| 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 Authors: Yao W(姚卫); Fan XJ(范学军) View  |  Adobe PDF(832Kb)  |  Favorite  |  View/Download:320/97  |  Submit date: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 |
| 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 Authors: 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) View  |  Adobe PDF(2131Kb)  |  Favorite  |  View/Download:354/129  |  Submit date: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 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:501/100  |  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:519/191  |  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 |