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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:20/0  |  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:23/0  |  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:9/0  |  Submit date:2024/05/27 modular unit modification regression rate combustion efficiency hybrid rocket engine |
| 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:60/3  |  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 |
| 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:349/70  |  Submit date: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 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:569/75  |  Submit date:2021/08/03 Tunable diode laser absorption spectroscopy Hybrid rocket motor Temperature Partial pressure Combustion efficiency |
| 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 Authors: 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)  |  Favorite  |  View/Download:238/69  |  Submit date:2021/06/11 concentration hybrid rocket motor nozzle exit temperature Tunable diode laser absorption spectroscopy (TDLAS) water vapor |