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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 |
| 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：55/2 | 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 |
| 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：110/14 | Submit date：2022/11/08
Hybrid rocket engine Swirl injection Novel composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| Experimental Study of Combustion Characteristics of Micron-Sized Aluminum Particles and Liquid Water 期刊论文
JOURNAL OF PROPULSION AND POWER, 2022, 页码: 1-8
Authors: Ma P(马鹏); Wang SF(王双峰); Wang XZ(王秀珍)
Adobe PDF(2629Kb) | Favorite | View/Download：210/47 | Submit date：2022/03/25 |
| 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：327/61 | Submit date：2021/11/01
Hybrid rocket engine Fuel mass flow rate Tunable diode laser absorption spectroscopy Temperature Partial pressure |
| Very high cycle fatigue (VHCF) response of additively manufactured materials: A review 期刊论文
FATIGUE & FRACTURE OF ENGINEERING MATERIALS & STRUCTURES, 2021, 页码: 25
Authors: Caivano, Riccardo; Tridello, Andrea; Chiandussi, Giorgio; Qian GA(钱桂安); Paolino, Davide; Berto, Filippo
Adobe PDF(26537Kb) | Favorite | View/Download：259/40 | Submit date：2021/11/01
additive manufacturing (AM) aluminum alloy In718 Ti6Al4V very high cycle fatigue (VHCF) |
| 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：556/72 | Submit date：2021/08/03
Tunable diode laser absorption spectroscopy Hybrid rocket motor Temperature Partial pressure Combustion efficiency |
| Numerical and experimental study on high-speed hydrogen-oxygen combustion gas flow and aerodynamic heating characteristics 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 7, 页码: 11
Authors: Yu JP(于江鹏); Li JP(李进平); Wang Q(汪球); Zhang SZ(张仕忠); Zhang XY(张晓源)
Adobe PDF(3271Kb) | Favorite | View/Download：262/50 | Submit date：2021/11/01 |
| 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：294/71 | 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：554/160 | Submit date：2019/09/09
Al particle cellular detonation heat capacity hybrid model |
