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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：18/0 | Submit date：2024/05/21
Hybrid rocket Composite fuel grain Characteristic structure Radiation image Combustion properties |
| 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：111/14 | Submit date：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
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：330/62 | 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：558/73 | Submit date：2021/08/03
Tunable diode laser absorption spectroscopy Hybrid rocket motor Temperature Partial pressure Combustion efficiency |
| 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
Authors: 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) | Favorite | View/Download：297/71 | Submit date：2021/06/15 |
| Cellular Aluminum Particle-Air Detonation Based on Realistic Heat Capacity Model 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2020, 卷号: 192, 期号: 10, 页码: 1931-1945
Authors: Xiang GX(项高翔); Yang PF(杨鹏飞); Teng HH(滕宏辉); Jiang ZL(姜宗林)
Adobe PDF(1871Kb) | Favorite | View/Download：555/160 | Submit date：2019/09/09
Al particle cellular detonation heat capacity hybrid model |
| Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors: Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Yu XL(余西龙)
Adobe PDF(1961Kb) | Favorite | View/Download：296/112 | Submit date：2020/05/18
Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
| Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework 期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40
Authors: Zhang ZJ(张子健); Wen CY; Liu YF(刘云峰); Zhang DL(张德良); Jiang ZL(姜宗林)
Adobe PDF(4374Kb) | Favorite | View/Download：426/146 | Submit date：2019/09/09
Two-phase detonation CE/SE Eulerian-Lagrangian MPI Aluminum-air detonation |
