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Temperature and H2O concentration measurements for a hybrid rocket motor plume using a single mid-infrared tunable diode laser 会议论文
2020 Applied Optics and Photonics China: Optical Sensing and Imaging Technology, AOPC 2020, Xiamen, PEOPLES R CHINA, 25 August 2020 through 27 August 2020
Authors:  Fang SH(方思晗);  Wang ZZ(王泽众);  Li RJ(李仁杰);  Zhang ZL(张泽林);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1569Kb)  |  Favorite  |  View/Download：234/69  |  Submit date：2021/06/11
concentration  hybrid rocket motor  nozzle exit  temperature  Tunable diode laser absorption spectroscopy (TDLAS)  water vapor  
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  
Supercritical GN2/GH2 jet modeled by the ECS method 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);  Jin YC(靳一超);  Lee YC(李亚超)
Adobe PDF(1048Kb)  |  Favorite  |  View/Download：187/73  |  Submit date：2020/11/20
Dynamic Response of Spar Wind Turbine Moored by Dynamic Catenaries Under Random Wind and Wave Loads 会议论文
38th International Conference on Ocean, Offshore and Arctic Engineering, Glasgow, Scotland, UK, June 9–14, 2019
Authors:  Li YL;  Guo SX(郭双喜);  Li M(李敏);  Chen WM(陈伟民)
Adobe PDF(1272Kb)  |  Favorite  |  View/Download：194/49  |  Submit date：2020/01/06
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)
Adobe PDF(567Kb)  |  Favorite  |  View/Download：362/107  |  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)
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)
Adobe PDF(623Kb)  |  Favorite  |  View/Download：298/105  |  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)
Adobe PDF(2297Kb)  |  Favorite  |  View/Download：286/122  |  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)
Adobe PDF(832Kb)  |  Favorite  |  View/Download：315/95  |  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