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Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet 会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
作者:  Wang Y;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(1120Kb)  |  收藏  |  浏览/下载：485/103  |  提交时间：2018/12/26
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
作者:  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)
浏览  |  Adobe PDF(805Kb)  |  收藏  |  浏览/下载：389/145  |  提交时间：2018/06/06
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)
浏览  |  Adobe PDF(1173Kb)  |  收藏  |  浏览/下载：438/216  |  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  
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor 会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
作者:  Cheng D(程迪);  Wang J(王晶);  Gong J;  Lu Y(陆阳);  Yao W(姚卫);  Li L(李龙);  Fan XJ(范学军);  Fan, Xuejun (xfan@imech.ac.cn)
浏览  |  Adobe PDF(2131Kb)  |  收藏  |  浏览/下载：319/122  |  提交时间：2017/05/05
Equivalence Ratios  Heat Flux Distributions  Heat Transfer Characteristics  Scramjet  Supercritical Kerosenes  Supersonic Combustion  Supersonic Combustors  Total Temperatures  
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
作者:  Lu Y(陆阳);  Wang XZ(王新竹);  Li L(李龙);  Cheng D(程迪);  Yuan T(袁涛);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(445Kb)  |  收藏  |  浏览/下载：424/90  |  提交时间：2016/01/08
Hydrocarbons  Combustors  Cooling  Heat Transfer  
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：469/171  |  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  
基于推力潜能的燃烧室性能评估 会议论文
第十六届全国激波与激波管学术会议, 中国河南洛阳, 2014-07-15
作者:  姚轩宇;  王春;  姜宗林
浏览  |  Adobe PDF(2149Kb)  |  收藏  |  浏览/下载：289/93  |  提交时间：2015/07/01
超燃冲压发动机  性能评价  推力潜能  
Experimental study on Jet-A pool fire at high altitude 会议论文
11th International Symposium on Fire Safety Science, FSS 2014, Canterbury, New zealand, February 10, 2014 - February 14, 2014
作者:  Zhou ZH;  Yao W(姚卫);  Li HH;  Lin CH;  Yin J;  Wu T;  Meier OC;  Wang J;  Wang, Jian (wangj@ustc.edu.cn)
浏览  |  Adobe PDF(973Kb)  |  收藏  |  浏览/下载：280/105  |  提交时间：2017/05/27
Ambient Pressures  Flame Temperatures  High Altitude  Insulation Board  Mass Burning Rate  Performance Standards  Pool Fires  Temperature Decrease  
超声速燃烧室中脉冲爆轰混合/燃烧强化机理研究 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
作者:  姚轩宇;  王春;  姜宗林
Adobe PDF(769Kb)  |  收藏  |  浏览/下载：1134/153  |  提交时间：2014/01/23
超燃冲压发动机  燃烧室  爆轰  混合  助燃  
基于压电效应的高超声速摩阻直接测量技术 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
作者:  张陈安;  姚文秀;  陈文龙;  王发民;  李静美
Adobe PDF(1002Kb)  |  收藏  |  浏览/下载：634/215  |  提交时间：2014/01/23
高超声速  激波风洞  摩阻  直接测量  压电效应