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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:15/0  |  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:12/0  |  Submit date:2024/05/21 Combustion Efficiency Emission Spectroscopy Hybrid Rocket Engines Paraffin Based Fuels Regression rate Aluminium Alloys 3D Printing |
| 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:105/8  |  Submit date:2023/10/30 hybrid rocket engine swirl-radial injection regression rate flame images combustion efficiency |
| 特征结构对复合式石蜡基药柱燃烧特性的影响研究 期刊论文 推进技术, 2023, 页码: 9 Authors: 张泽林; 林鑫; 王若岩; 罗家枭; 王泽众; 张春元; 李飞; 余西龙 Adobe PDF(1532Kb)  |  Favorite  |  View/Download:145/45  |  Submit date:2023/05/08 固液混合火箭发动机 复合式药柱 特征结构 尺度 燃烧特性 |
| 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:85/8  |  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 |
| Effects of swirl injection on the combustion of a 11el composite hybrid rocket fuel grain 期刊论文 ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182 Authors: Zhang ZL(张泽林); Lin X(林鑫); Wang ZZ(王泽众); Wu K(吴坤); Luo JX(罗家枭); Fang SH(方思晗); Zhang CY; Li F(李飞); Yu XL(余西龙) Adobe PDF(9227Kb)  |  Favorite  |  View/Download:130/33  |  Submit date:2022/10/23 Hybrid rocket engine Swirl injection 11el composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| Effects of swirl injection on the combustion of a novel composite hybrid rocket fuel grain 期刊论文 ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182 Authors: Zhang ZL(张泽林); Lin X(林鑫); Wang ZZ(王泽众); Wu K(吴坤); Luo JX(罗家枭); Fang SH(方思晗); Zhang CY(张春元); Li F(李飞); Yu XL(余西龙) Adobe PDF(9227Kb)  |  Favorite  |  View/Download:103/11  |  Submit date:2022/11/08 Hybrid rocket engine Swirl injection Novel composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| 嵌套式螺旋药柱燃烧特性影响因素探究 期刊论文 固体火箭技术, 2022, 卷号: 45, 期号: 04, 页码: 506-511 Authors: 王泽众; 张泽林; 林鑫; 李飞; 余西龙 Adobe PDF(726Kb)  |  Favorite  |  View/Download:144/36  |  Submit date:2022/11/14 固液火箭发动机 燃烧特性 退移速率 特征速度 |
| 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:315/59  |  Submit date:2021/11/01 Hybrid rocket engine Fuel mass flow rate Tunable diode laser absorption spectroscopy Temperature Partial pressure |