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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：16/0 | 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：14/0 | Submit date：2024/05/21
Combustion Efficiency Emission Spectroscopy Hybrid Rocket Engines Paraffin Based Fuels Regression rate Aluminium Alloys 3D Printing |
| 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：107/12 | Submit date：2022/11/08
Hybrid rocket engine Swirl injection Novel composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| Effect of rib height on turbulent flow and heat transfer of kerosene in rectangular duct 期刊论文
ACTA MECHANICA SINICA, 2022, 卷号: 38, 期号: 7, 页码: 12
Authors: Li X(李冼); Zhong FQ(仲峰泉); Xing YF(邢云绯)
Adobe PDF(5257Kb) | Favorite | View/Download：248/59 | Submit date：2022/07/18
Rib height Kerosene Heat transfer enhancement Turbulent flow |
| The Influence of Geometrical and Inlet Parameters on the Impingement Cooling of Aviation Kerosene 期刊论文
JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2022, 卷号: 144, 期号: 7, 页码: 5
Authors: Xing YF(邢云绯); Fan WH(范文慧); Du MM(杜蒙蒙); Zhong FQ(仲峰泉)
Adobe PDF(1128Kb) | Favorite | View/Download：262/52 | Submit date：2022/07/18
impingement cooling heat transfer kerosene numerical study |
| 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：322/60 | 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：554/72 | Submit date：2021/08/03
Tunable diode laser absorption spectroscopy Hybrid rocket motor Temperature Partial pressure Combustion efficiency |
| 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：290/110 | Submit date：2020/05/18
Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
| Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors: Fan WH(范文慧); Zhong FQ(仲峰泉); Ma SG(马素刚); Zhang XY(张新宇)
Adobe PDF(4075Kb) | Favorite | View/Download：317/95 | Submit date：2020/03/11
Wall heat flux Numerical simulation Ethylene Supersonic combustor |
| External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
Authors: Chen H; Tan H; Liu YZ; Zhang QF(张启帆)
Adobe PDF(4679Kb) | Favorite | View/Download：284/98 | Submit date：2019/09/09 |
