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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.
Adobe PDF(1708Kb)  |  收藏  |  浏览/下载：470/207  |  提交时间：2017/12/18
H2o2/kerosene Bipropellant  Coaxial-swirl Injector  Geometric Constant  Performance  
Flow characteristic of highly underexpanded jets from various nozzle geometries 期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
作者:  Li XP(李晓鹏);  Zhou, Rui;  Yao W(姚卫);  Fan XJ(范学军);  Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(5723Kb)  |  收藏  |  浏览/下载：428/188  |  提交时间：2017/11/16
Underexpanded Jets  Noncircular Jets  Nozzle Geometry  Large Eddy Simulation  
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.
Adobe PDF(1848Kb)  |  收藏  |  浏览/下载：408/147  |  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.
Adobe PDF(5788Kb)  |  收藏  |  浏览/下载：458/101  |  提交时间：2017/11/16
Numerical studies of shock wave interactions with a supersonic turbulent boundary layer in compression corner:Turning angle effects 期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 149, 页码: 56-69
作者:  Tong FL(童福林);  Yu ZP(于长平);  Tang ZG(唐志共);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.;  Li, XL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
Adobe PDF(6937Kb)  |  收藏  |  浏览/下载：457/162  |  提交时间：2017/10/27
Compression Corner  Low-frequency Oscillation  Coherent Vortex Structure  Power Spectrum  Turbulent Kinetic Energy Budget  Direct Numerical Simulation  
振动激发对高超声速气动力/热影响 期刊论文
力学学报, 2017, 卷号: 49, 期号: 03, 页码: 616-626
作者:  张子健;  刘云峰;  姜宗林
Adobe PDF(711Kb)  |  收藏  |  浏览/下载：369/75  |  提交时间：2017/12/22
振动激发  气动力/热  边界层  高温气体效应  
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：435/115  |  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：342/79  |  提交时间：2017/07/24
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)
Adobe PDF(1173Kb)  |  收藏  |  浏览/下载：461/224  |  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)
Adobe PDF(623Kb)  |  收藏  |  浏览/下载：269/94  |  提交时间：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft