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| Evaluation of the influence of radiation on a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion & Energy Forum, VIRTUAL EVENT, 2020-08-17
Authors: Li B(李波); Yao W(姚卫) ; Fan XJ(范学军)
 Adobe PDF(1358Kb) |  Favorite | View/Download：157/49 | Submit date：2021/02/01 |
| Modeling Analysis on Cavity-based Flame Stabilization in Scramjet Combustor 会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors: Wu K(吴坤); Zhang P(张鹏); Fan XJ(范学军)
 Favorite | View/Download：141/0 | Submit date：2019/11/20
Combustion chemistry Combustion dynamics Dual mode scramjet Flame stabilization Improved delayed detached eddy simulations Overall reactions Scramjet combustors Shock wave structures |
| 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
Authors: Yao W(姚卫); Wu K(吴坤); Lee YC(李亚超); Fan XJ(范学军)
Adobe PDF(1156Kb) | Favorite | View/Download：424/0 | Submit date：2018/12/26 |
| 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)
 View | Adobe PDF(567Kb) | Favorite | View/Download：342/102 | 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)
View | Adobe PDF(805Kb) | Favorite | View/Download：409/153 | 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)
View | Adobe PDF(1173Kb) | Favorite | View/Download：462/225 | 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：270/94 | Submit date：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
Authors: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
View | Adobe PDF(1249Kb) | Favorite | View/Download：316/93 | Submit date：2018/01/16
Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
| 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：264/114 | 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：291/87 | 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 |
