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A peculiar bifurcation transition route of thermocapillary convection in rectangular liquid layers 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2017, 卷号: 88, 页码: 8-15
作者:  Jiang H(姜欢);  Duan L(段俐);  Kang Q(康琦);  Duan, L;  Kang, Q (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Micrograv, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(2469Kb)  |  收藏  |  浏览/下载：336/106  |  提交时间：2017/11/29
Thermocapillary Convection  Temperature Oscillation  Transition Route  Tangent Bifurcation  Chaotic Characteristic  
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：395/141  |  提交时间：2017/08/15
Laminar Flame Speed  Oxygenated Fuels  Gasoline  High Pressure And High Temperature  
Highly efficient one-step synthesis of carbon encapsulated nanocrystals by the oxidation of metal pi-complexes 期刊论文
NANOTECHNOLOGY, 2017, 卷号: 28, 期号: 32, 页码: 10.1088/1361-6528/aa7995
作者:  Liu BY;  Shao YF(邵颖峰);  Xiang X;  Zhang FH;  Yan SC;  Li WG;  Liu BY
浏览  |  Adobe PDF(2570Kb)  |  收藏  |  浏览/下载：245/97  |  提交时间：2017/10/27
Carbon Encapsulated Nanocrystals  Core-shell  Low Temperature Synthesis  Metal Pi-complex  
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：440/216  |  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  
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：300/89  |  提交时间：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
Numerical analysis of shock wave and supersonic turbulent boundary interaction between adiabatic and cold walls 期刊论文
JOURNAL OF TURBULENCE, 2017, 卷号: 18, 期号: 6, 页码: 569-588
作者:  Tong, Fulin;  Tang, Zhigong;  Yu ZP(于长平);  Zhu, Xingkun;  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing, Peoples R China.
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Shock Wave/turbulent Boundary Layer Interaction  Wall Temperature  Turbulence Structure  Shock Motion  Dynamic Mode Decomposition  
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
作者:  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.
浏览  |  Adobe PDF(1681Kb)  |  收藏  |  浏览/下载：318/94  |  提交时间：2017/12/27
Supersonic Combustion  Flame Stabilization  Stagtnation Temperature  Gloabal Equivalence Ratio  Ch** Ch*emiluminesenCh*e  
Assessment of Vibrational Non-Equilibrium Effect on Detonation Cell Size 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 5, 页码: 841-853
作者:  Shi LS;  Shen H;  Zhang P;  Zhang DL(张德良);  Wen CH;  Wen, CY (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China.
浏览  |  Adobe PDF(1584Kb)  |  收藏  |  浏览/下载：289/147  |  提交时间：2017/07/24
Cellular Structure  Coupled-vibration-chemistry-vibration (Cvcv) Model  Detonation  Two-temperature Model  Vibrational Non-equilibrium