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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：77/2 | 提交时间：2023/10/30
hybrid rocket engine swirl-radial injection regression rate flame images combustion efficiency |
| 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：60/3 | 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：48/1 | 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 |
| 高马赫数燃烧强化的激波风洞试验研究 期刊论文
力学学报, 2022, 卷号: 54, 期号: 05, 页码: 1403-1413
作者: 张旭; 张启帆; 岳连捷; 孟东东; 罗苇航; 于江鹏; 张晓源; 李进平; 陈宏; 李飞
Adobe PDF(3069Kb) | 收藏 | 浏览/下载：232/42 | 提交时间：2022/08/11
高马赫数 超声速燃烧 燃烧强化 小支板 JF-24激波风洞 |
| 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：275/50 | 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：223/56 | 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：515/62 | 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：329/47 | 提交时间：2021/09/07
High mach number scramjet Circular cross-section TDLAS Multi-view simultaneous imaging POD |
| Improving the Combustion Performance of a Hybrid Rocket Engine using a Novel Fuel Grain with a Nested Helical Structure 期刊论文
JOVE-JOURNAL OF VISUALIZED EXPERIMENTS, 2021, 期号: 167, 页码: 17
作者: Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Zhang ZL(张泽林); Yu XL(余西龙)
Adobe PDF(1456Kb) | 收藏 | 浏览/下载：241/57 | 提交时间：2021/06/15 |
| 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：266/103 | 提交时间：2020/05/18
Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
