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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:8/0  |  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 11el 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; Li F(李飞); Yu XL(余西龙) Adobe PDF(9227Kb)  |  Favorite  |  View/Download:129/33  |  Submit date: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 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:101/11  |  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:307/58  |  Submit date:2021/11/01 Hybrid rocket engine Fuel mass flow rate Tunable diode laser absorption spectroscopy Temperature Partial pressure |