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| 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
作者: 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) |  收藏 | 浏览/下载：163/0 | 提交时间：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
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：82/3 | 提交时间：2023/10/30
hybrid rocket engine swirl-radial injection regression rate flame images combustion efficiency |
| 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 |
| 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
作者: 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) | 收藏 | 浏览/下载：121/30 | 提交时间：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
作者: 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) | 收藏 | 浏览/下载：98/9 | 提交时间：2022/11/08
Hybrid rocket engine Swirl injection Novel composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| 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 |
| 基于金属燃料添加方法的固液火箭发动机药柱 专利
发明专利. 基于金属燃料添加方法的固液火箭发动机药柱, 专利号: ZL202110711172.X, 申请日期: 2021-06-25, 授权日期: 2022-06-21
发明人: 林鑫; 王泽众; 张泽林; 李飞; 余西龙
Adobe PDF(769Kb) | 收藏 | 浏览/下载：99/33 | 提交时间：2022/10/17 |
| Error Analysis of Integrated Absorbance for TDLAS in a Nonuniform Flow Field 期刊论文
APPLIED SCIENCES-BASEL, 2021, 卷号: 11, 期号: 22, 页码: 15
作者: Li RJ(李仁杰); Li F(李飞); Lin X(林鑫); Yu XL(余西龙)
Adobe PDF(7410Kb) | 收藏 | 浏览/下载：241/44 | 提交时间：2022/01/13
TDLAS integrated absorbance error analysis |
| 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：281/51 | 提交时间：2021/11/01
Hybrid rocket engine Fuel mass flow rate Tunable diode laser absorption spectroscopy Temperature Partial pressure |
| 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：518/62 | 提交时间：2021/08/03
Tunable diode laser absorption spectroscopy Hybrid rocket motor Temperature Partial pressure Combustion efficiency |
