已选(0)清除
条数/页: 排序方式: |
| 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:91/6  |  提交时间:2023/10/30 hybrid rocket engine swirl-radial injection regression rate flame images combustion efficiency |
| 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:72/6  |  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:50/2  |  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 |
| Effects of swirl injection on the combustion of a 11el composite hybrid rocket fuel grain 期刊论文 ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182 作者: 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; Li F(李飞); Yu XL(余西龙) Adobe PDF(9227Kb)  |  收藏  |  浏览/下载:125/33  |  提交时间:2022/10/23 Hybrid rocket engine Swirl injection 11el composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| 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 作者: 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)  |  收藏  |  浏览/下载:100/11  |  提交时间:2022/11/08 Hybrid rocket engine Swirl injection Novel composite fuel grain Regression rate Oxidizer-to-fuel ratio |