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| Study on the propulsive performance of oblique detonation engine 期刊论文
ENERGY, 2024, 卷号: 292, 页码: 11
作者: Liu YF(刘云峰) ; Han, Xin; Zhang, Zijian
  收藏 | 浏览/下载：1/0 | 提交时间：2024/04/15
Oblique detonation engine ODE Propulsive performance Specific impulse |
| 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：158/0 | 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 > |
| Standing oblique detonation for hypersonic propulsion: A review 期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
作者: Jiang ZL(姜宗林)
Adobe PDF(10386Kb) | 收藏 | 浏览/下载：26/1 | 提交时间：2024/02/26
Standing oblique detonation Scramjet engine Oblique detonation engine Shock wave Supersonic combustion Hypersonic ramjet propulsion |
| Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18
作者: Yang F(杨帆); Lin MY(林明月); Hu ZM(胡宗民); Han GL(韩桂来)
Adobe PDF(8946Kb) | 收藏 | 浏览/下载：61/1 | 提交时间：2023/11/28
oblique detonation engine cantilevered injection localized high heat flux boundary layer separation reattachment |
| 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：71/0 | 提交时间：2023/10/30
hybrid rocket engine swirl-radial injection regression rate flame images combustion efficiency |
| Analysis of spray characteristics of a jet film injection element based on Voronoi tessellation 期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 206, 页码: 100-113
作者: He CM(何成明); Zhang, Peng; He, Zhixia; Yue LJ(岳连捷)
Adobe PDF(20952Kb) | 收藏 | 浏览/下载：42/0 | 提交时间：2023/04/20
Liquid rocket engine Pintle injector Spray characteristics Jet film injection Voronoi tessellation |
| 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：116/29 | 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：97/9 | 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：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 |
| Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
作者: Chen KT(陈科挺); Yue LJ(岳连捷); Zhang XY(张新宇)
Adobe PDF(511Kb) | 收藏 | 浏览/下载：193/35 | 提交时间：2022/01/12
Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
