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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)![](/image/person.jpg)
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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)![](/image/person.jpg)
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| Influence of compressibility effect on supersonic combustion modeling 会议论文 AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019 Authors: Chen L; Yao W(姚卫) ; Fan XJ(范学军)![](/image/person.jpg)
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| A novel method of cooling channel optimization for active-cooled structure using the calculus of variations 会议论文 AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019 Authors: Li X(李轩); Lu Y(陆阳) ; Wu K(吴坤); Fan XJ(范学军)![](/image/person.jpg)
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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 Authors: Yao W(姚卫) ; Wu K(吴坤); Lee YC(李亚超) ; Fan XJ(范学军)![](/image/person.jpg)
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| 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)![](/image/person.jpg)
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| 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 Authors: Wang Y; Yao W(姚卫) ; Fan XJ(范学军)![](/image/person.jpg)
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| 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:485/234  |  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)![](/image/person.jpg)
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| 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:338/103  |  Submit date:2018/01/16 Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |