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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 Authors: 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) View  |  Adobe PDF(2678Kb)  |  Favorite  |  View/Download:276/62  |  Submit date: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 Authors: 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) View  |  Adobe PDF(2678Kb)  |  Favorite  |  View/Download:213/70  |  Submit date: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 Authors: Zhang X(张旭); Yue LJ(岳连捷); Huang TL(黄庭隆); Zhang QF(张启帆); Zhang XY(张新宇) Adobe PDF(3862Kb)  |  Favorite  |  View/Download:348/122  |  Submit date: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 Authors: Fu YW(符耀威); Yu ZP(于长平); Yan Z(闫正); Li XL(李新亮) View  |  Adobe PDF(2894Kb)  |  Favorite  |  View/Download:394/144  |  Submit date:2020/03/21 Supersonic combustion Turbulence jet Direct numerical simulations Coherent structures |
| 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 Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇) View  |  Adobe PDF(3918Kb)  |  Favorite  |  View/Download:538/173  |  Submit date: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 Authors: Peng J(彭俊); Zhang ZJ(张子健); Hu ZM(胡宗民); Jiang ZL(姜宗林) View  |  Adobe PDF(2165Kb)  |  Favorite  |  View/Download:411/94  |  Submit date:2019/09/09 Shock reflection Vibration excitation Mach reflection Transition criterion Hypersonic flow |