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Investigation on the cycle performance and the combustion characteristic of two CO2-based binary mixtures for the transcritical power cycle 期刊论文
ENERGY, 2019, 卷号: 179, 页码: 454-463
作者:  Pan LS(潘利生);  Ma YJ;  Li T(李腾);  Li HX(李慧鑫);  Li B;  Wei XL(魏小林)
Adobe PDF(1691Kb)  |  收藏  |  浏览/下载：237/73  |  提交时间：2019/09/09
CO2-Based mixtures  Transcritical power cycle  Waste heat recovery  Flammability  
Experimental Investigation of Laminar Flame Speed Measurement for Kerosene Fuels: Jet A-1, Surrogate Fuel, and Its Pure Components 期刊论文
Enery & Fuels, 2018, 卷号: 32, 期号: 2, 页码: 2332-2343
作者:  Wu Y(武毅);  Modica V;  Yu XL(余西龙);  Grisch F
Adobe PDF(2808Kb)  |  收藏  |  浏览/下载：676/200  |  提交时间：2018/02/02
Alkylated Cyclohexane Flames  Ignition Delay Times  Burning Velocities  High-pressure  Diesel Fuels  N-decane  Mixtures  Combustion  Temperature  Extinction  
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  
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：271/81  |  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  
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.
浏览  |  Adobe PDF(2568Kb)  |  收藏  |  浏览/下载：277/102  |  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  
Laser Diagnostics of Combustion Enhancement on a CH4/Air Bunsen Flame by Dielectric Barrier Discharge 期刊论文
CHINESE PHYSICS LETTERS, 2013, 卷号: 30, 期号: 8, 页码: 085203/1-085203/4
作者:  Zhang SH(张少华);  Yu XL(余西龙);  Chen LH(陈立红);  Zhang XY(张新宇);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1970Kb)  |  收藏  |  浏览/下载：833/263  |  提交时间：2013/09/27
Premixed Flames  Plasma  Methane  Mixtures  Planar Laser Induced Fluorescence  Laser Diagnostics  Flame Velocities  Emission Spectra  Dielectric Barrier Discharge  
Measurements of non-equilibrium and equilibrium temperature behind a strong shock wave in simulated martian atmosphere 期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 5, 页码: 1296-1302
作者:  Lin X;  Yu XL(余西龙);  Li F(李飞);  Zhang SH(张少华);  Xin JG;  Zhang XY(张新宇);  Yu, XL;  Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(828Kb)  |  收藏  |  浏览/下载：797/240  |  提交时间：2013/01/18
Radiation Measurements  Shock Wave  Mars Re-entry  Rotational Temperature  Vibrational Temperature  Radiation Measurements  Cn  Entry  Tube  Mixtures  Model  
Shock tube study of kerosene ignition delay at high pressures 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2012, 卷号: 55, 期号: 6, 页码: 947-954
作者:  Liang JH(梁金虎);  Wang S(王苏);  Hu HH(胡弘浩);  Zhang ST;  Fan BC(范秉诚);  Cui JP(崔季平);  Wang, S;  Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(690Kb)  |  收藏  |  浏览/下载：743/259  |  提交时间：2013/01/18
Ignition Delay Time  Kerosene  Shock Tube  High Pressure  Mixtures  Autoignition  Temperatures  Times