中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共10条，第1-10条 帮助

限定条件            
已选(0)清除 条数/页：   排序方式：
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：459/224  |  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：268/94  |  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：320/104  |  提交时间：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
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：262/113  |  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：282/84  |  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  
Numerical simulations of sessile droplet evaporating on heated substrate 会议论文
8th Meeting of the International-Marangoni-Association (IMA), Bad Honnef, GERMANY, 2016
作者:  Chen X(陈雪);  Chen, Paul G.;  Ouazzani, Jalil;  Liu QS(刘秋生);  Chen, PG (reprint author), Aix Marseille Univ, CNRS, Cent Marseille, M2P2, Marseille, France.
浏览  |  Adobe PDF(659Kb)  |  收藏  |  浏览/下载：269/76  |  提交时间：2018/01/16
Microdroplets  Surfaces  Water  
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)
Adobe PDF(414Kb)  |  收藏  |  浏览/下载：222/79  |  提交时间：2018/11/08
Oxygen  Diluted environments  Monotonic trend  Partial premixing  Stabilization mechanisms  Transition process  Transitional flames  Transitional process  Turbulent combustion  
Large-eddy simulation of turbulent preferential concentration and collision of bidisperse heavy particles in isotropic turbulence 会议论文
1st International Workshop on Computational Particle Technology, Suzhou, PEOPLES R CHINA, MAR, 2016
作者:  Chen JC(陈进财);  Jin GD(晋国栋);  Jin, GD (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China.
Adobe PDF(962Kb)  |  收藏  |  浏览/下载：384/109  |  提交时间：2018/01/16
Direct Numerical Simulations  Space-time Correlations  Inertial Particles  Approximate Deconvolution  Cloud Droplets  Fluidized-bed  Flow  Model  Motion  Particle-laden Turbulence  Large-eddy Simulation  Subgrid Scale Motion  Bidisperse Particles  Preferential Concentration  Collision Rate Attenuation  
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)
Adobe PDF(897Kb)  |  收藏  |  浏览/下载：458/100  |  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
Adobe PDF(468Kb)  |  收藏  |  浏览/下载：301/83  |  提交时间：2018/01/16
Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics