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| Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
作者: Wang KL(王宽亮) ; Li F(李飞); Zou PF(邹鹏飞); Lin X(林鑫); Mao RH(毛荣海); Yu XL(余西龙)
 浏览 |  Adobe PDF(2678Kb) |  收藏 | 浏览/下载：257/61 | 提交时间：2020/03/21
Swirl flame Heat release Chemiluminescence 3D-CTC |
| Effect of the fuel-air flow velocity on heat release rate of swirling non-premixed methane flames 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 95, 页码: UNSP 105465
作者: Wang KL(王宽亮); Li F(李飞); Zou PF(邹鹏飞); Lin X(林鑫); Mao RH(毛荣海); Yu XL(余西龙)
浏览 | Adobe PDF(2678Kb) | 收藏 | 浏览/下载：202/67 | 提交时间：2020/03/21
Swirl flame Heat release Chemiluminescence 3D-CTC |
| Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
作者: Zhang X(张旭); Yue LJ(岳连捷); Huang TL(黄庭隆); Zhang QF(张启帆); Zhang XY(张新宇)
浏览 | Adobe PDF(3862Kb) | 收藏 | 浏览/下载：331/114 | 提交时间：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| DNS analysis of the effects of combustion on turbulence in a supersonic H2/air jet flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 93, 页码: 9
作者: Fu YW(符耀威); Yu ZP(于长平); Yan Z(闫正); Li XL(李新亮)
浏览 | Adobe PDF(2894Kb) | 收藏 | 浏览/下载：376/139 | 提交时间：2020/03/21
Supersonic combustion Turbulence jet Direct numerical simulations Coherent structures |
| Initiation of oblique detonation waves induced by a blunt wedge in stoichiometric hydrogen-air mixtures 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 92, 页码: 676-684
作者: Fang YS(方宜申); Zhang ZJ(张子健); Hu ZM(胡宗民); Deng, X
浏览 | Adobe PDF(2321Kb) | 收藏 | 浏览/下载：316/80 | 提交时间：2019/10/21
Oblique detonation wave Blunt wedge Initiation Hydrogen |
| Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
作者: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇)
浏览 | Adobe PDF(3918Kb) | 收藏 | 浏览/下载：521/165 | 提交时间：2019/09/09
Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
作者: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林)
浏览 | Adobe PDF(2165Kb) | 收藏 | 浏览/下载：396/92 | 提交时间：2019/09/09
Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |
