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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：90/6  |  提交时间：2023/10/30
hybrid rocket engine  swirl-radial injection  regression rate  flame images  combustion efficiency  
Estimating energy release performance of oxidizer-activated aluminum fuel particles under ultrafast stimulus 期刊论文
DEFENCE TECHNOLOGY, 2023, 卷号: 23, 页码: 92-99
作者:  Li, Yaru;  Ren, Hui;  Wu, Xinzhou;  Wang, Huixin;  Yu XL(余西龙)
Adobe PDF(1900Kb)  |  收藏  |  浏览/下载：45/4  |  提交时间：2023/06/15
Aluminum  Glycidyl azide polymer  Laser  Detonation  Explosive  Ultrafast stimulus  
Investigation on plasma enhanced decomposition of ammonium dinitramide (ADN) based propellant with optical diagnosis 期刊论文
SPECTROCHIMICA ACTA PART B-ATOMIC SPECTROSCOPY, 2023, 卷号: 200, 页码: 8
作者:  Wang FY(王方仪);  Zhang SH(张少华);  Yu XL(余西龙)
Adobe PDF(2201Kb)  |  收藏  |  浏览/下载：124/4  |  提交时间：2023/02/03
Optical emission spectroscopy  Glow to filamentary discharge transition  ADN-based propellant  Plasma parameter  
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：67/4  |  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  
Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
作者:  Luo JX(罗家枭);  Zhang ZL(张泽林);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Zhou GX(周功喜);  Zhang SH(张森豪);  Li F(李飞);  Yu XL(余西龙);  Wu, Jie
Adobe PDF(732Kb)  |  收藏  |  浏览/下载：49/1  |  提交时间：2023/04/20
Combustion Instability  Rayleigh Scattering  Precombustion Chamber  Hybrid Propellant Rocket  Hybrid Rocket Motor  Mass Flow Rate  Convective Heat Transfer  Characteristic Velocity  Planar Laser Induced Fluorescence  Propulsion and Power  
Three-dimensional printed metal-nested composite fuel grains with superior mechanical and combustion properties 期刊论文
VIRTUAL AND PHYSICAL PROTOTYPING, 2022, 卷号: 17, 期号: 3, 页码: 437-450
作者:  Lin X(林鑫);  Qu DD(屈丹丹);  Chen XD(陈雪冬);  Wang ZZ(王泽众);  Luo JX(罗家枭);  Meng DD(孟东东);  Liu GL(刘国亮);  Zhang K(张坤);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(3694Kb)  |  收藏  |  浏览/下载：114/25  |  提交时间：2022/10/23
Hybrid rocket engine  additive manufacturing  metal-nested composite fuel grain  mechanical properties  combustion properties  optical emission spectroscopy  
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
作者:  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)  |  收藏  |  浏览/下载：293/54  |  提交时间：2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
Magnetic and Pressure Effects on E-H Mode Transition Power and Electron Energy Distribution in Helical Antenna-Coupled RF Plasma 期刊论文
IEEE TRANSACTIONS ON PLASMA SCIENCE, 2021, 卷号: 49, 期号: 9, 页码: 2806-2816
作者:  Wang CS(王传胜);  Liu, Xuhui;  Geng, Jinyue;  Li F(李飞);  Lin X(林鑫);  Yu XL(余西龙)
Adobe PDF(3369Kb)  |  收藏  |  浏览/下载：234/58  |  提交时间：2021/11/01
E-H mode transition  electron energy distribution function (EEDF)  helical antenna  magnetic  
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：523/64  |  提交时间：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
作者:  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)  |  收藏  |  浏览/下载：337/49  |  提交时间：2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD