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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:13/0  |  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:3/0  |  Submit date:2024/05/27 modular unit modification regression rate combustion efficiency hybrid rocket engine |
| Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades 期刊论文 VIRTUAL AND PHYSICAL PROTOTYPING, 2023, 卷号: 18, 期号: 1, 页码: e2235680 Authors: Qu DD(屈丹丹); Lin X(林鑫); Zhang K(张坤); Li ZY(李志永); Wang ZZ(王泽众); Liu GL(刘国亮); Meng Y(孟洋); Luo GX(罗耕星); Wang RY(王若岩); Yu XL(余西龙) Adobe PDF(4980Kb)  |  Favorite  |  View/Download:177/5  |  Submit date:2023/09/05 Hybrid rocket engine additive manufacturing three-dimensional printing breathable blade composite fuel grain mechanical and combustion properties porous structure > |
| 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:106/9  |  Submit date:2023/10/30 hybrid rocket engine swirl-radial injection regression rate flame images combustion efficiency |
| 一种固液发动机燃烧机理的研究方法及系统 专利 发明专利. 一种固液发动机燃烧机理的研究方法及系统, 专利号: CN202211556757.X, 申请日期: 2022-12-06, 授权日期: 2023-06-20 Inventors: 林鑫; 罗家枭; 张森豪; 周功喜; 张泽林; 王泽众; 李飞; 余西龙 Adobe PDF(517Kb)  |  Favorite  |  View/Download:44/14  |  Submit date:2024/01/23 |
| 固液火箭发动机燃烧控制方法及变推力固液火箭发动机 专利 发明专利. 固液火箭发动机燃烧控制方法及变推力固液火箭发动机, 专利号: 2022106664871, Inventors: 林鑫; 张泽林; 王若岩; 王泽众; 罗家枭; 李飞; 余西龙 Favorite  |  View/Download:52/0  |  Submit date:2023/08/28 |
| 固液火箭发动机燃烧控制方法及变推力固液火箭发动机 专利 发明专利. 固液火箭发动机燃烧控制方法及变推力固液火箭发动机, 专利号: CN202210666487.1, 申请日期: 2022-06-14, 授权日期: 2023-04-14 Inventors: 林鑫; 张泽林; 王若岩; 王泽众; 罗家枭; 李飞; 余西龙 Adobe PDF(631Kb)  |  Favorite  |  View/Download:36/12  |  Submit date:2024/01/23 |
| 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:148/46  |  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 |
| 一种固液发动机药柱及其制备方法 专利 发明专利. 一种固液发动机药柱及其制备方法, 专利号: 2022114971015, 申请日期: 2022-11-28, 授权日期: 2023-03-14 Inventors: 林鑫; 王若岩; 王泽众; 张泽林; 孟东东; 余西龙 Adobe PDF(594Kb)  |  Favorite  |  View/Download:71/14  |  Submit date:2023/08/18 |