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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：89/5 | 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：67/4 | 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：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：123/32 | 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：99/10 | 提交时间：2022/11/08
Hybrid rocket engine Swirl injection Novel composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| 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：289/53 | 提交时间：2021/11/01
Hybrid rocket engine Fuel mass flow rate Tunable diode laser absorption spectroscopy Temperature Partial pressure |
| 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：252/58 | 提交时间：2021/06/15 |
| Temperature and H2O concentration measurements for a hybrid rocket motor plume using a single mid-infrared tunable diode laser 会议论文
2020 Applied Optics and Photonics China: Optical Sensing and Imaging Technology, AOPC 2020, Xiamen, PEOPLES R CHINA, 25 August 2020 through 27 August 2020
作者: Fang SH(方思晗); Wang ZZ(王泽众); Li RJ(李仁杰); Zhang ZL(张泽林); Lin X(林鑫); Li F(李飞); Yu XL(余西龙)
Adobe PDF(1569Kb) | 收藏 | 浏览/下载：219/67 | 提交时间：2021/06/11
concentration hybrid rocket motor nozzle exit temperature Tunable diode laser absorption spectroscopy (TDLAS) water vapor |
