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Coupling noise analysis of force and temperature on Taiji-1 interferometer 会议论文
1st Optics Frontier Conference 2021, Hangzhou, 24 April 2021 到 26 April 2021
作者:  Wang J(王娟);  Deng XQ(邓小芹);  Yang R(杨然);  Luo ZR(罗子人)
Adobe PDF(1012Kb)  |  收藏  |  浏览/下载：185/56  |  提交时间：2021/11/30
Force noise  Interferometry  Noise coupling  Taiji-1  Temperature noise  
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：210/66  |  提交时间：2021/06/11
concentration  hybrid rocket motor  nozzle exit  temperature  Tunable diode laser absorption spectroscopy (TDLAS)  water vapor  
Oxidation of Ammonia and NO Formation during NH3/CO Post-combustion 会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
作者:  Wei XL(魏小林);  Zhang YF(张玉锋);  Zhao J(赵京)
收藏  |  浏览/下载：128/0  |  提交时间：2019/11/20
Chemical mechanism  Entrained Flow Reactor  Hydrocarbon fuel  Hydrogen carriers  Ignition energies  NO and CO emissions  Post  combustion  Temperature increase  
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：171/31  |  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  
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)
Adobe PDF(1173Kb)  |  收藏  |  浏览/下载：434/214  |  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  
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)
Adobe PDF(1249Kb)  |  收藏  |  浏览/下载：294/87  |  提交时间：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
The effects of air vitiation on the supersonic turbulent channel flow using direct numerical simulation 会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
作者:  Chen XP;  Li XP(李晓鹏);  Dou HS
Adobe PDF(1216Kb)  |  收藏  |  浏览/下载：213/73  |  提交时间：2017/05/05
Mass Fraction  Mean Velocities  Nondimensional  Reynolds Analogy  Static Temperature  Statistical Characteristics  Temperature Correlation  Turbulent Channel Flows  
Plasma Assisted Low Temperature Combustion 会议论文
22nd International Symposium on Plasma Chemistry (ISPC 22), Antwerp, BELGIUM, JUL 05-10, 2015
作者:  Ju YG;  Lefkowitz JK;  Reuter CB;  Won SH;  Yang XL;  Yang S;  Sun WT;  Jiang ZL(姜宗林);  Chen Q;  Ju, YG (reprint author), Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA.
Adobe PDF(2568Kb)  |  收藏  |  浏览/下载：274/101  |  提交时间：2017/05/04
Plasma Assisted Combustion  Low Temperature Chemistry  Kinetics  Cool Flames  S-curve Transition  Nonequilibrium Plasma  Saturated-hydrocarbons  Diffusion Flames  Pulsed Discharge  Ignition  Mixtures  Oxidation  Kinetics  Enhancement  
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Yao W(姚卫);  Wang J(王晶);  Lu Y(陆阳);  Li XP(李晓鹏);  Fan XJ(范学军)
Adobe PDF(1195Kb)  |  收藏  |  浏览/下载：464/170  |  提交时间：2016/07/01
Adiabatic Flame Temperature  Combustion  Directed Graphs  Flow Separation  Heat Flux  Kerosene  Large Eddy Simulation  Musculoskeletal System  Real Time Systems  Sensitivity Analysis  Spacecraft  Transients  
Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Zhong, Fengquan (fzhong@imech.ac.cn)
Adobe PDF(496Kb)  |  收藏  |  浏览/下载：244/72  |  提交时间：2017/05/05
Combustion Pro  Cess  Directed Relation Graph  Dynamic Evolution  Fuel Injection Velocities  Kinetic Mechanism  Reduced Mechanisms  Temperature Profiles  Temporal And Spatial Evolutions