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Combustion Characteristics of a Swirl-Radial-Injection Composite Fuel Grain with Applications in Hybrid Rockets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 9, 页码: 19
作者:  Wang RY(王若岩);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Zhang ZL(张泽林);  Luo JX(罗家枭);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(8125Kb)  |  收藏  |  浏览/下载：70/0  |  提交时间：2023/10/30
hybrid rocket engine  swirl-radial injection  regression rate  flame images  combustion efficiency  
Analysis of energy, exergy and CO2 emissions in a fiberglass furnace with oxy-fuel combustion 期刊论文
FUEL, 2023, 卷号: 348, 页码: 128484
作者:  Yao Y(姚远);  He, Junyao;  Chen, Qi;  Li T(李腾);  Li B(李博);  Wei XL(魏小林)
Adobe PDF(2563Kb)  |  收藏  |  浏览/下载：109/0  |  提交时间：2023/06/15
Energy and exergy efficiency  CO2 emission  Heat recovery  Oxy-fuel combustion  Fiberglass melting furnace  
Charactering Catalytic Ignition and Combustion for the Ninety Percent Hydrogen Peroxide/Paraffin Based Hybrid Rocket Engine 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Wu K(吴坤);  Zhang ZL(张泽林);  Fang SH(方思晗);  Meng DD(孟东东);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(712Kb)  |  收藏  |  浏览/下载：53/0  |  提交时间：2023/04/20
Hybrid Rocket Engines  Propellant  Thermocouples  Numerical Analysis  Catalysis  Absorption Spectroscopy  Combustion Products  decomposition efficiency  Paraffin Fuel  Ignition Systems  
Characterizing combustion of a hybrid rocket using laser absorption spectroscopy 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9
作者:  Fang SH(方思晗);  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Li RJ(李仁杰);  Li, Jing;  Zhang, Zhedian;  Liu, Yan;  Yu XL(余西龙)
Adobe PDF(4367Kb)  |  收藏  |  浏览/下载：507/60  |  提交时间：2021/08/03
Tunable diode laser absorption spectroscopy  Hybrid rocket motor  Temperature  Partial pressure  Combustion efficiency  
Numerical investigation on the performance of bluff body augmented micro cavity-combustor 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 7, 页码: 4932-4945
作者:  Zhang Z;  Wu K(吴坤);  Yuen R;  Yao W(姚卫);  Wang J
浏览  |  Adobe PDF(3438Kb)  |  收藏  |  浏览/下载：305/106  |  提交时间：2020/04/07
Micro combustor  Cavity  Bluff body  Combustion efficiency  Local Damkohler number  
Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
作者:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1961Kb)  |  收藏  |  浏览/下载：262/101  |  提交时间：2020/05/18
Hybrid rocket engine  Paraffin-based fuel  Acrylonitrile-butadiene-styrene  Regression rate  Combustion efficiency  
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)
浏览  |  Adobe PDF(1388Kb)  |  收藏  |  浏览/下载：295/95  |  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  
INFLUENCE OF HIGH ALTITUDE ON COMBUSTION EFFICIENCY AND RADIATION FRACTION OF HYDROCARBON FIRES 期刊论文
HEAT TRANSFER RESEARCH, 2017, 卷号: 48, 期号: 10, 页码: 865-875
作者:  Li HH;  Yao W(姚卫);  Li P;  Zhou ZH;  Wang J
浏览  |  Adobe PDF(1193Kb)  |  收藏  |  浏览/下载：353/121  |  提交时间：2017/11/29
Hydrocarbon Fire  Heat Release Rate  Combustion Efficiency  Radiation Fraction  Transmittance  
Experimental study of the burning behavior of n-heptane pool fires at high altitude 期刊论文
FIRE AND MATERIALS, 2016, 卷号: 40, 期号: 1, 页码: 80-88
作者:  Zhou ZH;  Yao W(姚卫);  Hu XK;  Yuen R;  Wang J;  Wang, J (reprint author), Univ Sci & Technol China, State Key Lab Fire Sci, Hefei 230027, Peoples R China.
浏览  |  Adobe PDF(1435Kb)  |  收藏  |  浏览/下载：314/98  |  提交时间：2016/03/21
High Altitude  N-heptane Pool Fire  Burning Intensity  Heat Release Rate  Combustion Efficiency  
Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
作者:  Wang ZP(王知溥);  Li F(李飞);  Gu HS;  Yu XL(余西龙);  Zhang XY(张新宇);  Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1112Kb)  |  收藏  |  浏览/下载：534/225  |  提交时间：2015/06/12
Scramjet  Dual-mode Combustor  Divergent Angle  Cavity Location  Combustion Efficiency  Tdlas