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Reconstruction model for heat release rate based on artificial neural network 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 37, 页码: 19599-19616
作者:  Li B(李波);  Yao W(姚卫);  Li YC(李亚超);  Fan XJ(范学军)
Adobe PDF(5169Kb)  |  收藏  |  浏览/下载：104/26  |  提交时间：2022/10/25
Heat release rate (HRR)  Artificial neural network (ANN)  Proper orthogonal -12omposition (POD)  Chemiluminescence  Supersonic hydrogen flame  
Enhancement of combustion performance in a microchannel: Synergistic effects of bluff-body and cavity 期刊论文
FUEL, 2020, 卷号: 265, 页码: 11
作者:  Zhang Z;  Wu K(吴坤);  Yao W(姚卫);  Yuen R;  Wang J
浏览  |  Adobe PDF(3821Kb)  |  收藏  |  浏览/下载：348/108  |  提交时间：2020/04/07
Micro-combustor  Bluff-body  Cavity  Combustion performance  Flame-flow interaction  
Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor 期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 卷号: 37, 期号: 3, 页码: 3685-3692
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1820Kb)  |  收藏  |  浏览/下载：456/155  |  提交时间：2018/12/27
Supersonic combustion  Flame stabilization mode  DLR Strut injection scheme  Stagnation Temperature  Overall equivalence ratio  
Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion 期刊论文
ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350
作者:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(1388Kb)  |  收藏  |  浏览/下载：302/97  |  提交时间：2018/12/27
Combustion Condition  Combustor Efficiency  Improved Delayed Detached Eddy Simulations  Initial Temperatures  Laminar Flame Speed  Scramjet Combustors  Supersonic Combustion  Turbulence-chemistry Interactions  
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：443/217  |  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  
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：319/94  |  提交时间：2017/12/27
Supersonic Combustion  Flame Stabilization  Stagtnation Temperature  Gloabal Equivalence Ratio  Ch** Ch*emiluminesenCh*e  
Numerical Investigation on Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 12, 页码: 2154-2179
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, P (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong 999077, Hong Kong, Peoples R China.
浏览  |  Adobe PDF(2993Kb)  |  收藏  |  浏览/下载：359/168  |  提交时间：2017/12/18
Detailed Hydrogen Oxidation Mechanism  Dlr  Flame Stabilization  Sensitivity Analysis  Supersonic Combustion  
Modeling analysis on the silica glass synthesis in a hydrogen diffusion flame 期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 卷号: 81, 页码: 797-803
作者:  Yao W(姚卫);  Zheng LL;  Zhang Hui;  Zhang, H (reprint author), Tsinghua Univ, Dept Engn Phys, Beijing 100084, Peoples R China.
浏览  |  Adobe PDF(1009Kb)  |  收藏  |  浏览/下载：380/106  |  提交时间：2015/03/17
Silica Glass  Flame Hydrolysis Deposition  Multiphase Model  Modeling  Hydrogen Flame  
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：474/173  |  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  
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)
Adobe PDF(973Kb)  |  收藏  |  浏览/下载：286/107  |  提交时间：2017/05/27
Ambient Pressures  Flame Temperatures  High Altitude  Insulation Board  Mass Burning Rate  Performance Standards  Pool Fires  Temperature Decrease