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Reconstruction model for heat release rate based on artificial neural network 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 37, 页码: 19599-19616
Authors:  Li B(李波);  Yao W(姚卫);  Li YC(李亚超);  Fan XJ(范学军)
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Heat release rate (HRR)  Artificial neural network (ANN)  Proper orthogonal -12omposition (POD)  Chemiluminescence  Supersonic hydrogen flame  
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)
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Influences of Domain Symmetry on Supersonic Combustion Modeling 期刊论文
JOURNAL OF PROPULSION AND POWER, 2019, 卷号: 35, 期号: 2, 页码: 451-465
Authors:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(862Kb)  |  Favorite  |  View/Download：347/102  |  Submit date：2019/04/11
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：452/0  |  Submit date：2018/12/26
Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 4, 页码: 975-991
Authors:  Yao W(姚卫);  Lu Y(陆阳);  Wu K(吴坤);  Wang J(王晶);  Fan XJ(范学军)
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Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion 期刊论文
ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350
Authors:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军)
View  |  Adobe PDF(1388Kb)  |  Favorite  |  View/Download：334/108  |  Submit date：2018/12/27
Combustion Condition  Combustor Efficiency  Improved Delayed Detached Eddy Simulations  Initial Temperatures  Laminar Flame Speed  Scramjet Combustors  Supersonic Combustion  Turbulence-chemistry Interactions  
Flow characteristic of highly underexpanded jets from various nozzle geometries 期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
Authors:  Li XP(李晓鹏);  Zhou, Rui;  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
View  |  Adobe PDF(5723Kb)  |  Favorite  |  View/Download：446/192  |  Submit date：2017/11/16
Underexpanded Jets  Noncircular Jets  Nozzle Geometry  Large Eddy Simulation  
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：480/232  |  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：285/99  |  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：333/101  |  Submit date：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow