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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)
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Plasma properties measurements of parallel-plane electrodes in Argon by coupling OES and PLIF 会议论文
Global Intelligent Industry Conference, 中国上海, 2020/10/28-30
Authors:  Wang FY(王方仪);  Zhang SH(张少华);  Yu XL(余西龙)
Adobe PDF(975Kb)  |  Favorite  |  View/Download:438/48  |  Submit date:2021/02/01
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:177/59  |  Submit date:2021/02/01
Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:  Yao W(姚卫);  Li B(李波)
Adobe PDF(1665Kb)  |  Favorite  |  View/Download:173/51  |  Submit date:2020/11/20
Dynamic zone flamelet model  GH2/GO2  Large Eddy Simulation (LES)  Rocket combustor  Turbulence-chemistry interaction  
A molecular dynamics simulation on the oxidation of core-shell aluminum nanoparticles in oxygen and water environments 会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors:  Chu QZ;  Liao LJ(廖丽涓);  Shi BL;  Luo KH;  Wang NF
View  |  Adobe PDF(850Kb)  |  Favorite  |  View/Download:206/35  |  Submit date:2019/11/20
Aluminum nanoparticles  Concentration distributions  Heat and mass transfer process  Heat transfer efficiency  Molecular dynamics simulations  Oxidation mechanisms  Particle temperature  Structure evolution  
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:460/0  |  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)
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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)
View  |  Adobe PDF(1120Kb)  |  Favorite  |  View/Download:519/111  |  Submit date:2018/12/26
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)
View  |  Adobe PDF(623Kb)  |  Favorite  |  View/Download:298/105  |  Submit date:2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft