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Effect of characteristic structure of nested composite hybrid rocket fuel grain on combustion properties 期刊论文
ACTA ASTRONAUTICA, 2024, 卷号: 218, 页码: 269-281
Authors:  Wang RY(王若岩);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Pan JJ(潘俊杰);  Zhang ZL(张泽林);  Luo JX(罗家枭);  Li F(李飞);  Yu XL(余西龙)
Favorite  |  View/Download：20/0  |  Submit date：2024/05/21
Hybrid rocket  Composite fuel grain  Characteristic structure  Radiation image  Combustion properties  
Superior Al90Mg10-Based Composite Fuel Grain for a Hybrid Rocket Engine 期刊论文
JOURNAL OF SPACECRAFT AND ROCKETS, 2024, 页码: 9
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：23/0  |  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
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：9/0  |  Submit date：2024/05/27
modular unit  modification  regression rate  combustion efficiency  hybrid rocket engine  
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Peng JL(彭锦龙);  Liu, Yan;  Zhang ZL(张泽林);  Fang SH(方思晗);  Yu XL(余西龙)
Adobe PDF(6496Kb)  |  Favorite  |  View/Download：349/70  |  Submit date：2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
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
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：569/75  |  Submit date：2021/08/03
Tunable diode laser absorption spectroscopy  Hybrid rocket motor  Temperature  Partial pressure  Combustion efficiency  
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
Adobe PDF(4108Kb)  |  Favorite  |  View/Download：350/57  |  Submit date：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD