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The design and main performance of a hydrogen peroxide/kerosene coaxial-swirl injector in a lab-scale rocket engine 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 70, 页码: 636-643
作者:  Li HX(李慧鑫);  Ye L(叶亮);  Wei XL(魏小林);  Li T(李腾);  Li S(李森);  Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1708Kb)  |  收藏  |  浏览/下载：454/199  |  提交时间：2017/12/18
H2o2/kerosene Bipropellant  Coaxial-swirl Injector  Geometric Constant  Performance  
高温引气对亚燃冲压燃烧室性能影响的研究 期刊论文
推进技术, 2017, 期号: 12, 页码: 10
作者:  王亚妹;  方祥军;  顾洪斌;  林鹏;  王霄
浏览  |  Adobe PDF(2088Kb)  |  收藏  |  浏览/下载：218/48  |  提交时间：2017/12/22
亚燃冲压燃烧室  凹腔/支板结构  高温引气  混合效率  燃烧效率  
An Experimental Study of Chilton-Colburn Analogy Between Turbulent Flow and Convective Heat Transfer of Supercritical Kerosene 期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2017, 卷号: 139, 期号: 6
作者:  Zhang YJ(张永江);  Zhong FQ(仲峰泉);  Xing YF(邢云绯);  张新宇 Xinyu;  Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.;  Zhong, FQ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
浏览  |  Adobe PDF(1041Kb)  |  收藏  |  浏览/下载：434/114  |  提交时间：2017/07/24
Aviation Kerosene  Supercritical  Skin Friction Coefficient  Convective Heat Transfer  Chilton-colburn Analogy  
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  
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  
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)
浏览  |  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  
Experimental Studies of Film Cooling in Supersonic Combustors 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Fan C(樊川);  Wang J(王晶);  Fan XJ(范学军)
浏览  |  Adobe PDF(735Kb)  |  收藏  |  浏览/下载：308/101  |  提交时间：2018/01/16
Combustion  Combustors  Coolants  Kerosene  Spacecraft  Supersonic Aerodynamics  
Full Scale Detached Eddy Simulation of Transverse Hydrogen Jet in Supersonic Combustion 会议论文
53rd AIAA/SAE/ASEE Joint Propulsion Conference , Atlanta, GA., 10-12 July 2017
作者:  Fan E;  Wu K(吴坤);  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(2297Kb)  |  收藏  |  浏览/下载：252/108  |  提交时间：2018/01/16
超临界压力下航空煤油流动与传热特性研究 学位论文
博士论文，北京: 中国科学院大学, 2017
作者:  张永江
Adobe PDF(8162Kb)  |  收藏  |  浏览/下载：446/20  |  提交时间：2017/07/07
氢气和煤油驱动超声速燃烧数值模拟研究 学位论文
硕士论文，北京: 中国科学院大学, 2017
作者:  范锷
Adobe PDF(5546Kb)  |  收藏  |  浏览/下载：305/7  |  提交时间：2017/07/07