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A novel method for analyzing pore size distribution of complex geometry shaped porous shale 会议论文
The Spring World Congress on Engineering and Technology 2020, Xi'an, China, April 24-26, 2020
作者:  Yang M(杨明);  Lin M(林缅)
Adobe PDF(926Kb)  |  收藏  |  浏览/下载：143/51  |  提交时间：2021/01/28
Adsorption, BJH, Capillary Condensation, Cylinder Pore, False Peak, Pore Size Distribution, Slit Pore  
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
作者:  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)  |  收藏  |  浏览/下载：216/67  |  提交时间：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
作者:  Yao W(姚卫);  Li B(李波)
Adobe PDF(1665Kb)  |  收藏  |  浏览/下载：142/43  |  提交时间：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
作者:  Chu QZ;  Liao LJ(廖丽涓);  Shi BL;  Luo KH;  Wang NF
浏览  |  Adobe PDF(850Kb)  |  收藏  |  浏览/下载：178/33  |  提交时间：2019/11/20
Aluminum nanoparticles  Concentration distributions  Heat and mass transfer process  Heat transfer efficiency  Molecular dynamics simulations  Oxidation mechanisms  Particle temperature  Structure evolution  
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
作者:  Fan E;  Wu K(吴坤);  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(567Kb)  |  收藏  |  浏览/下载：333/100  |  提交时间：2018/12/26
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
作者:  Wang Y;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1120Kb)  |  收藏  |  浏览/下载：489/104  |  提交时间：2018/12/26
An untethered free-fall vertical profiler for deep ocean mixing measurements 会议论文
Conference on OCEANS MTS/IEEE Charleston, Charleston, SC, OCT 22-25, 2018
作者:  Xu XY.;  Zhang SZ;  Xu DZ;  Peng SL(彭世镠);  Liu J.;  Yang XQ;  Tian C.
浏览  |  Adobe PDF(225Kb)  |  收藏  |  浏览/下载：458/82  |  提交时间：2019/04/19
untethered vertical profiler  microstructure sensors  turbulence  the rate of dissipation of TKE  
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：441/217  |  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)
Adobe PDF(623Kb)  |  收藏  |  浏览/下载：263/90  |  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)
Adobe PDF(517Kb)  |  收藏  |  浏览/下载：311/100  |  提交时间：2018/01/16
Combustors  Cracks  Diesel Engines  Efficiency  Ethylene  Fighter Aircraft  Fuels  High Speed Cameras  Ignition  Kerosene  Luminance  Spacecraft  Stabilization