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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  
Laminar flame speed of lignocellulosic biomass-derived oxygenates and blends of gasoline/oxygenates 期刊论文
FUEL, 2017, 卷号: 202, 页码: 572-582
作者:  Wu Y;  Rossow B;  Modica V;  Yu XL(余西龙);  Wu LL;  Grisch F;  Wu, Y (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(1848Kb)  |  收藏  |  浏览/下载：392/140  |  提交时间：2017/08/15
Laminar Flame Speed  Oxygenated Fuels  Gasoline  High Pressure And High Temperature  
Initiation structure of oblique detonation waves behind conical shocks 期刊论文
PHYSICS OF FLUIDS, 2017, 卷号: 29, 期号: 8
作者:  Yang PF(杨鹏飞);  Ng, Hoi Dick;  Teng HH(滕宏辉);  Jiang ZL(姜宗林);  Teng, HH (reprint author), Beijing Inst Technol, Sch Aerosp Engn, Dept Mech, Beijing 100081, Peoples R China.
浏览  |  Adobe PDF(5788Kb)  |  收藏  |  浏览/下载：448/98  |  提交时间：2017/11/16
Influence of Thermal Sensor Installation on Measuring Accuracy at Stagnation Points 期刊论文
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2017, 卷号: 31, 期号: 2, 页码: 318-323
作者:  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林);  Li, JP (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(419Kb)  |  收藏  |  浏览/下载：426/114  |  提交时间：2017/10/27
Effect of HCl on NO Formation during CO/NH3 Combustion in an Entrained Flow Reactor at 1023-1223 K 期刊论文
ENERGY & FUELS, 2017, 卷号: 31, 期号: 3, 页码: 3281-3287
作者:  Wang Y(王阳);  Zhao J;  Wei XL(魏小林);  Li S(李森);  Wei, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.;  Wei, XL (reprint author), Univ Chinese Acad Sci, Sch Sci & Engn, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1719Kb)  |  收藏  |  浏览/下载：333/77  |  提交时间：2017/07/24
Surrogate Based Optimization of Aerodynamic Noise for Streamlined Shape of High Speed Trains 期刊论文
APPLIED SCIENCES-BASEL, 2017, 卷号: 7, 期号: 2
作者:  Sun ZX(孙振旭);  Zhang Y;  Yang GW(杨国伟);  Sun, ZX (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(6165Kb)  |  收藏  |  浏览/下载：612/325  |  提交时间：2017/07/24
Aerodynamic Noise  Nlas  Kriging Model  Cross Validation  Equivalent Continuous Spl  
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  
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
浏览  |  Adobe PDF(1249Kb)  |  收藏  |  浏览/下载：299/89  |  提交时间：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
Force Test in a Large-Scale Shock Tunnel 会议论文
55th AIAA Aerospace Sciences Meeting , Grapevine, Texas, 9-13 January 2017
作者:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(6096Kb)  |  收藏  |  浏览/下载：305/87  |  提交时间：2018/01/16