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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：215/67  |  提交时间：2021/06/11
concentration  hybrid rocket motor  nozzle exit  temperature  Tunable diode laser absorption spectroscopy (TDLAS)  water vapor  
Experimental Research on the Detonation in Gaseous Mixtures with Suspended Aluminum Particles 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:  Zhang XY(张晓源);  Chen H(陈宏);  Li JP(李进平);  Zhang SZ(张仕忠);  Yu HR(俞鸿儒)
Adobe PDF(543Kb)  |  收藏  |  浏览/下载：36/18  |  提交时间：2023/03/17
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：140/43  |  提交时间：2020/11/20
Dynamic zone flamelet model  GH2/GO2  Large Eddy Simulation (LES)  Rocket combustor  Turbulence-chemistry interaction  
Heat release and temperature diagnostics for swirling flames using chemiluminescence and absorption tomography 会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
作者:  Lin X(林鑫);  Wang KL(王宽亮);  Li F(李飞);  Yu XL(余西龙)
浏览  |  Adobe PDF(495Kb)  |  收藏  |  浏览/下载：224/54  |  提交时间：2019/11/06
Behavior of Alkali Metals in Fly Ash during Waste Heat Recovery for Municipal Solid Waste Incineration 会议论文
6th Sino-Australian Symposium on Advanced Coal and Biomass Utilisation Technologies, Perth, AUSTRALIA, DEC 04-08, 2017
作者:  Zhao J(赵京);  Wei XL(魏小林);  Li T(李腾);  Li HX(李慧鑫);  Bin F(宾峰)
Adobe PDF(844Kb)  |  收藏  |  浏览/下载：425/139  |  提交时间：2018/06/06
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：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  
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：452/97  |  提交时间：2018/01/16
Combustion  Gas Absorption  Infrared Devices  Monopropellants  Optical Parametric Oscillators  Spacecraft  
Theoretical calculation of mid-infrared spectra from hypersonic non-ablative sphere 会议论文
International Symposium on Infrared Technology and Application / International Symposium on Robot Sensing and Advanced Control, Beijing, PEOPLES R CHINA, MAY 09-11, 2016
作者:  Wu J;  Yu XL(余西龙);  Zhu XJ;  Ma J;  Mao HX;  Wu, J (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Wu, J (reprint author), Sci & Technol Opt Radiat Lab, Beijing 100854, Peoples R China.
Adobe PDF(1160Kb)  |  收藏  |  浏览/下载：277/84  |  提交时间：2017/05/12
Hypersonic  Mid-infrared  Atom  Diatomic Molecule  Partition-functions  Molecules  Air  
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：474/173  |  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  
Analysis for Combustion Properties of Crude Oil Pool Fire 会议论文
2014 International Symposium on Safety Science and Technology, Beijing, China, November 4-6, 2014
作者:  Chen Z(陈阵);  Wei XL(魏小林)
Adobe PDF(474Kb)  |  收藏  |  浏览/下载：341/97  |  提交时间：2015/09/16
Combustion Properties  Calculation Models  Burning Rate  Flame Shape  Thermal Radiation Intensity