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| 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:10/0  |  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:2/0  |  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 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:102/7  |  Submit date: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 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:84/8  |  Submit date: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 Authors: 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)  |  Favorite  |  View/Download:55/2  |  Submit date: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 Authors: 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)  |  Favorite  |  View/Download:119/28  |  Submit date: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 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:312/58  |  Submit date: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 Authors: 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)  |  Favorite  |  View/Download:240/60  |  Submit date: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 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:545/67  |  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:342/52  |  Submit date:2021/09/07 High mach number scramjet Circular cross-section TDLAS Multi-view simultaneous imaging POD |