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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
Authors:  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)
View  |  Adobe PDF(517Kb)  |  Favorite  |  View/Download：340/110  |  Submit date：2018/01/16
Combustors  Cracks  Diesel Engines  Efficiency  Ethylene  Fighter Aircraft  Fuels  High Speed Cameras  Ignition  Kerosene  Luminance  Spacecraft  Stabilization  
Experimental study of combustion oscillations in a dual-mode scramjet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
Authors:  Tian XD;  Chen LH(陈立红);  Gu HB(顾洪斌);  Liu C;  Cheng LW;  Chang XY(张新宇);  Chen, Lihong (lhchen@imech.ac.cn)
View  |  Adobe PDF(824Kb)  |  Favorite  |  View/Download：253/74  |  Submit date：2017/09/04
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
Authors:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Zhong, Fengquan (fzhong@imech.ac.cn)
View  |  Adobe PDF(496Kb)  |  Favorite  |  View/Download：270/80  |  Submit date：2017/05/05
Combustion Pro  Cess  Directed Relation Graph  Dynamic Evolution  Fuel Injection Velocities  Kinetic Mechanism  Reduced Mechanisms  Temperature Profiles  Temporal And Spatial Evolutions  
Combined TDLAS and OES technique for CO concentration measurement in shock-heated Martian atmosphere 会议论文
2nd International Symposium on Laser Interaction with Matter (LIMIS), Xian, PEOPLES R CHINA, SEP 09-12, 2012
Authors:  Lin X(林鑫);  Yu XL(余西龙);  Li F(李飞);  Zhang SH(张少华);  Xin JG;  Zhang XY(张新宇);  Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(683Kb)  |  Favorite  |  View/Download：821/286  |  Submit date：2013/12/12
Optical Emission Spectroscopy (Oes)  Tunable Diode Laser Absorption Spectroscopy (Tdlas)  Shock Wave  Temperature  Concentration  
Numerical study of ignition and combustion of partially cracked kerosene in a mach 2.5 supersonic model combustor 会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:  Zhong FQ(仲峰泉);  Chen LH(陈立红);  Chang XY(张新宇);  Zhong FQ(仲峰泉)
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CFD Simulation of Kerosene-Fueled Supersonic Combustion Ramjet Combustor Experiments 会议论文
Asia-Pacific International Symposium on Aerospace Technology, Xian, PEOPLES R CHINA, SEP 13-15, 2010
Authors:  Wan T(万田);  Chen LH(陈立红);  Wang J(王晶);  Fan XJ(范学军);  Zhang XY(张新宇);  Wan, TA (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
View  |  Adobe PDF(468Kb)  |  Favorite  |  View/Download：163/40  |  Submit date：2016/06/28
Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor 会议论文
AIAA/ASME/SAE/ASEE 40th Joint Propulsion Conference
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Zhang XY(张新宇);  Sung CJ
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Investigation of Vaporized Kerosene Injection in a Supersonic Model Combustor 会议论文
12th AIAA International Space Planes and Hypersonic Systems and Technologies, Norfolk, Virginia, December 15 – 19, 2003
Authors:  Yu G(俞刚);  Li JG(李建国);  Zhao Z;  Zhang XY(张新宇);  Sun CJ;  Yu G(俞刚)
Adobe PDF(244Kb)  |  Favorite  |  View/Download：772/211  |  Submit date：2007/12/18