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Effect of pilot hydrogen on the mixing and combustion characteristics in kerosene-fueled scramjet 期刊论文
APPLIED THERMAL ENGINEERING, 2025, 卷号: 258, 页码: 10./通讯作者：Tian, Zhen-Yu
Authors:  Shi, HongQing;  Wang, Du;  Cui NF(崔乃夫);  Zhao, ChenYang;  Lei, JieMing;  Zhu, ZiQiang;  Zhang, YaNing;  Tian, ZhenYu
Favorite  |  View/Download：28/0  |  Submit date：2024/11/22
Scramjet  Pilot hydrogen  Dual cavities  Mixing efficiency  Combustion performance  
Superior Al90Mg10-Based Composite Fuel Grain for a Hybrid Rocket Engine 期刊论文
JOURNAL OF SPACECRAFT AND ROCKETS, 2024, 页码: 9./通讯作者：Lin, Xin
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Pan JJ(潘俊杰);  Luo JX(罗家枭);  Wang RY(王若岩);  Zhang ZL(张泽林);  Yu XL(余西龙)
Favorite  |  View/Download：45/0  |  Submit date：2024/05/21
Combustion Efficiency  Emission Spectroscopy  Hybrid Rocket Engines  Paraffin Based Fuels  Regression rate  Aluminium Alloys  3D Printing  
Regression Rate and Combustion Efficiency of Composite Hybrid Rocket Grains Based on Modular Fuel Units 期刊论文
AEROSPACE, 2024, 卷号: 11, 期号: 4, 页码: 18./通讯作者：Lin, Xin, Wang, Zezhong
Authors:  Pan JJ(潘俊杰);  Lin X(林鑫);  Wang ZZ(王泽众);  Wang RY(王若岩);  Wu K(吴坤);  Liang, Jinhu;  Yu XL(余西龙)
Favorite  |  View/Download：31/0  |  Submit date：2024/05/27
modular unit  modification  regression rate  combustion efficiency  hybrid rocket engine  
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./通讯作者：Lin, Xin, Wang, Zezhong
Authors:  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)  |  Favorite  |  View/Download：218/46  |  Submit date：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./通讯作者：Wei, XL
Authors:  Yao Y(姚远);  He, Junyao;  Chen, Qi;  Li T(李腾);  Li B(李博);  Wei XL(魏小林)
Adobe PDF(2563Kb)  |  Favorite  |  View/Download：216/23  |  Submit date：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./通讯作者：Wang, ZZ (corresponding author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Authors:  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)  |  Favorite  |  View/Download：143/15  |  Submit date：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./通讯作者：Lin, Xin, Li, Fei
Authors:  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)  |  Favorite  |  View/Download：622/83  |  Submit date：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./通讯作者：Yao, Wei, Wang, Jian
Authors:  Zhang Z;  Wu K(吴坤);  Yuen R;  Yao W(姚卫);  Wang J
View  |  Adobe PDF(3438Kb)  |  Favorite  |  View/Download：380/117  |  Submit date：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./通讯作者：Lin, Xin
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1961Kb)  |  Favorite  |  View/Download：372/135  |  Submit date：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
Authors:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军)
View  |  Adobe PDF(1388Kb)  |  Favorite  |  View/Download：383/126  |  Submit date：2018/12/27
Combustion Condition  Combustor Efficiency  Improved Delayed Detached Eddy Simulations  Initial Temperatures  Laminar Flame Speed  Scramjet Combustors  Supersonic Combustion  Turbulence-chemistry Interactions