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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：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 |
| Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Cheng LW(程柳维); Zhong FQ(仲峰泉); Wang ZP(王知溥); Gu HB(顾洪斌); Ma SG(马素刚); Zhang XY(张新宇)
 Adobe PDF(517Kb) | Favorite | View/Download：326/107 | Submit date：2018/01/16
Combustors Cracks Diesel Engines Efficiency Ethylene Fighter Aircraft Fuels High Speed Cameras Ignition Kerosene Luminance Spacecraft Stabilization |
| 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：263/114 | 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)
Adobe PDF(832Kb) | Favorite | View/Download：290/87 | 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 |
| Multispecies Absorption Measurement in an Ammonium Dinitramide based Thruster 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Zeng W(曾徽); Lin X(林鑫); Zhen RP; Chen LZ; Li F(李飞); Yu XL(余西龙); Li, Fei(lifei@imech.ac.cn)
Adobe PDF(897Kb) | Favorite | View/Download：462/102 | Submit date：2018/01/16
Combustion Gas Absorption Infrared Devices Monopropellants Optical Parametric Oscillators Spacecraft |
| Performance of a detonation driven shock tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Li JW; Wang Q(汪球); Zhao W(赵伟); Lu P; Tan YX
Adobe PDF(468Kb) | Favorite | View/Download：305/83 | Submit date：2018/01/16
Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |
