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Development of a radiative heating facility for studying flow and heat transfer in hydrocarbon-cooled structures 期刊论文
REVIEW OF SCIENTIFIC INSTRUMENTS, 2018, 卷号: 89, 期号: 6, 页码: 64901
Authors:  Dong D(董达);  Lu Y(陆阳);  Yuan YM(袁越明);  Fan XJ(范学军)
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Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
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Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
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一种流场和火焰结构同步探测方法 专利
发明专利. 一种流场和火焰结构同步探测方法, 专利号: ZL201410373701.X, 申请日期: 2014-07-31, 授权日期: 2017-01-18
Inventors:  袁越明;  张泰昌;  宋军浩;  范学军
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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
Authors:  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)
View  |  Adobe PDF(1173Kb)  |  Favorite  |  View/Download:107/34  |  Submit date: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  
Characterization of flame stabilization modes in an ethylene-fueled supersonic combustor using time-resolved CH* chemiluminescence 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 卷号: 36, 期号: 2, 页码: 2919-2925
Authors:  Yuan YM(袁越明);  Zhang TC(张泰昌);  Yao W(姚卫);  Fan XJ(范学军);  Zhang P(张鹏);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, PR, Peoples R China.
View  |  Adobe PDF(1681Kb)  |  Favorite  |  View/Download:104/6  |  Submit date:2017/12/27
Supersonic Combustion  Flame Stabilization  Stagtnation Temperature  Gloabal Equivalence Ratio  Ch** Ch*emiluminesenCh*e  
Hypergolic ignition by head-on collision of N,N,N',N'-tetramethylethylenediamine and white fuming nitric acid droplets 期刊论文
COMBUSTION AND FLAME, 2016, 卷号: 173, 页码: 276-287
Authors:  Zhang DW;  Zhang P;  Yuan YM(袁越明);  Zhang TC(张泰昌);  Zhang, P (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China.
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Hypergolic Ignition  White Fuming Nitric Acid  n  Droplet Collision  n  Jet-like Mixing  N'  N'-tetramethylethylenediamine  
一种用于主动冷却实验的辐射加热方法 专利
发明专利. 一种用于主动冷却实验的辐射加热方法, 专利号: ZL201310552308.2, 申请日期: 2013-11-08, 授权日期: 2016-04-13
Inventors:  袁越明;  李龙;  程迪;  陆阳;  卢锡年;  范学军
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一种用于主动冷却实验的辐射加热系统 专利
发明专利. 一种用于主动冷却实验的辐射加热系统, 专利号: ZL201310141329.0, 申请日期: 2013-09-16, 授权日期: 2016-03-09
Inventors:  袁越明;  李龙;  程迪;  陆阳;  卢锡年;  范学军
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Development of a radiative heating system for studies of heat transfer in fuel-cooled structures 会议论文
14th International Energy Conversion Engineering Conference, Salt Lake City, UT, JUL 25-27, 2016
Authors:  Dong D(董达);  Lu Y(陆阳);  Yuan YM(袁越明);  Fan XJ(范学军);  Dong, D (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Aviation Kerosene  Supercritical Conditions  Pressure  Rp-3