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| Study on heat transfer coupling mechanism of direct thermoelectric conversion with regenerative cooling for supersonic combustor applications 期刊论文
APPLIED THERMAL ENGINEERING, 2024, 卷号: 238, 页码: 15
作者: Gao EK(高尔康) ; Zhong FQ(仲峰泉)
  收藏 | 浏览/下载：27/0 | 提交时间：2024/02/26
Direct thermoelectric conversion Regenerative cooling Supersonic combustor Analytical model Genetic algorithm |
| Additively manufactured aluminium nested composite hybrid rocket fuel grains with breathable blades 期刊论文
VIRTUAL AND PHYSICAL PROTOTYPING, 2023, 卷号: 18, 期号: 1, 页码: e2235680
作者: Qu DD(屈丹丹); Lin X(林鑫); Zhang K(张坤); Li ZY(李志永); Wang ZZ(王泽众); Liu GL(刘国亮); Meng Y(孟洋); Luo GX(罗耕星); Wang RY(王若岩); Yu XL(余西龙)
 Adobe PDF(4980Kb) | 收藏 | 浏览/下载：160/0 | 提交时间：2023/09/05
Hybrid rocket engine additive manufacturing three-dimensional printing breathable blade composite fuel grain mechanical and combustion properties porous structure > |
| Numerical study on hypersonic aerodynamic characteristics of the high-pressure capturing wing configuration with wing dihedral 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 15
作者: Chang SY(常思源); Xiao Y(肖尧); Li GL(李广利); Tian ZW(田中伟); Cui K(崔凯)
Adobe PDF(8136Kb) | 收藏 | 浏览/下载：39/1 | 提交时间：2024/03/11
High-pressure capturing wing Hypersonic Numerical simulation Wing dihedral Stability |
| 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：74/1 | 提交时间：2023/10/30
hybrid rocket engine swirl-radial injection regression rate flame images combustion efficiency |
| 基于气动导数的高压捕获翼飞行器纵向稳定性数值研究 期刊论文
中国科学:技术科学, 2023, 卷号: 54, 期号: 02, 页码: 275-288
作者: 常思源; 田中伟; 李广利; 肖尧; 崔凯
Adobe PDF(2549Kb) | 收藏 | 浏览/下载：63/11 | 提交时间：2024/03/01
高压捕获翼 数值模拟 纵向稳定性 动稳定导数 不确定性 |
| An analytical model for maximum temperature and temperature distribution of plate structure with active cooling 期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 5, 页码: 322290
作者: Hu GH(胡国豪); Zhong FQ(仲峰泉); Chen KT(陈科挺)
Adobe PDF(2013Kb) | 收藏 | 浏览/下载：48/0 | 提交时间：2023/04/20
Plate structure Active cooling Thermal protection Convective heat transfer Analytical model |
| 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：57/2 | 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：45/0 | 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 |
| Numerical study on flow and heat transfer of aviation kerosene at supercritical pressure in cooling channels with surface corrugations 期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2023, 卷号: 140, 页码: 14
作者: Gao EK(高尔康); Fan WH(范文慧); Li X(李冼); Zhong FQ(仲峰泉)
Adobe PDF(6628Kb) | 收藏 | 浏览/下载：154/3 | 提交时间：2023/02/09
Aviation kerosene Surface corrugation Convective heat transfer Supercritical conditions |
| Three-dimensional printed metal-nested composite fuel grains with superior mechanical and combustion properties 期刊论文
VIRTUAL AND PHYSICAL PROTOTYPING, 2022, 卷号: 17, 期号: 3, 页码: 437-450
作者: Lin X(林鑫); Qu DD(屈丹丹); Chen XD(陈雪冬); Wang ZZ(王泽众); Luo JX(罗家枭); Meng DD(孟东东); Liu GL(刘国亮); Zhang K(张坤); Li F(李飞); Yu XL(余西龙)
Adobe PDF(3694Kb) | 收藏 | 浏览/下载：111/24 | 提交时间：2022/10/23
Hybrid rocket engine additive manufacturing metal-nested composite fuel grain mechanical properties combustion properties optical emission spectroscopy |
