已选(0)清除
条数/页: 排序方式: |
| 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:162/0  |  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 > |
| 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:78/2  |  提交时间:2023/10/30 hybrid rocket engine swirl-radial injection regression rate flame images combustion efficiency |
| 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:120/29  |  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:98/9  |  提交时间:2022/11/08 Hybrid rocket engine Swirl injection Novel composite fuel grain Regression rate Oxidizer-to-fuel ratio |
| 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:113/25  |  提交时间:2022/10/23 Hybrid rocket engine additive manufacturing metal-nested composite fuel grain mechanical properties combustion properties optical emission spectroscopy |
| 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 作者: 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)  |  收藏  |  浏览/下载:277/51  |  提交时间:2021/11/01 Hybrid rocket engine Fuel mass flow rate Tunable diode laser absorption spectroscopy Temperature Partial pressure |
| 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 作者: Wang ZZ(王泽众); Lin X(林鑫); Li F(李飞); Yu XL(余西龙) Adobe PDF(1961Kb)  |  收藏  |  浏览/下载:268/103  |  提交时间:2020/05/18 Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |