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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
作者: 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)
 浏览 |  Adobe PDF(1173Kb) |  收藏 | 浏览/下载：440/216 | 提交时间：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
作者: Yao W(姚卫); Fan XJ(范学军)
浏览 | Adobe PDF(623Kb) | 收藏 | 浏览/下载：258/87 | 提交时间：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
作者: 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)
浏览 | Adobe PDF(517Kb) | 收藏 | 浏览/下载：310/100 | 提交时间：2018/01/16
Combustors Cracks Diesel Engines Efficiency Ethylene Fighter Aircraft Fuels High Speed Cameras Ignition Kerosene Luminance Spacecraft Stabilization |
| 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
作者: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
浏览 | Adobe PDF(1249Kb) | 收藏 | 浏览/下载：300/89 | 提交时间：2018/01/16
Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
| 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
作者: Fan E; Wu K(吴坤); Lee YC; Yao W(姚卫); Fan XJ(范学军)
浏览 | Adobe PDF(2297Kb) | 收藏 | 浏览/下载：252/108 | 提交时间：2018/01/16 |
| Numerical study of oblique detonation initiations with chain-branching kinetics 会议论文
AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting, Grapevine, Texas, 9-13 January 2017
作者: Teng HH(滕宏辉); Yang PF(杨鹏飞); Jiang ZL(姜宗林)
浏览 | Adobe PDF(464Kb) | 收藏 | 浏览/下载：276/109 | 提交时间：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
作者: Yao W(姚卫); Fan XJ(范学军)
浏览 | Adobe PDF(832Kb) | 收藏 | 浏览/下载：273/81 | 提交时间：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 |
| Detailed transitional process of the flames in hot and diluted environments from lifted flames to MILD combustion 会议论文
10th U.S. National Combustion Meeting, College Park, MD, United states, April 23, 2017 - April 26, 2017
作者: Liu CY; Zhang J(张健)
浏览 | Adobe PDF(414Kb) | 收藏 | 浏览/下载：217/76 | 提交时间：2018/11/08
Oxygen Diluted environments Monotonic trend Partial premixing Stabilization mechanisms Transition process Transitional flames Transitional process 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
作者: 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)
浏览 | Adobe PDF(897Kb) | 收藏 | 浏览/下载：451/97 | 提交时间：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
作者: Li JW; Wang Q(汪球); Zhao W(赵伟); Lu P; Tan YX
浏览 | Adobe PDF(468Kb) | 收藏 | 浏览/下载：295/82 | 提交时间：2018/01/16
Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |
