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| Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27 Authors: Li, Mengzhe; Wang, Zhikai; Xu, Rongguang; Zhang, Xiaoliang; Chen, Zhitong; Wang Q(汪球) Adobe PDF(8841Kb)  |  Favorite  |  View/Download:277/108  |  Submit date:2021/11/01 Non-equilibrium plasma Plasma-assisted ignition Plasma-assisted combustion Aerospace engine Combustor Extreme condition |
| Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14 Authors: Yao W(姚卫); Liu H(刘杭); Yue LJ(岳连捷); Xiao YB(肖雅彬) Adobe PDF(2954Kb)  |  Favorite  |  View/Download:284/65  |  Submit date:2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788 Authors: Xue, Rui; Zheng, Xing; Yue LJ(岳连捷); Zhang, Qian; He, Xin; Yang, Jing; Weng, Chao; Li, Zhihao Adobe PDF(5483Kb)  |  Favorite  |  View/Download:136/46  |  Submit date:2022/10/25 Boundary layer combustion Skin-friction reduction Supersonic combustion Scramjet engine |
| Steadiness of wave complex induced by oblique detonation wave reflection before an expansion corner 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 112, 页码: 9 Authors: Wang KL(王宽亮); Yang PF(杨鹏飞); Teng HH(滕宏辉) Adobe PDF(2853Kb)  |  Favorite  |  View/Download:248/70  |  Submit date:2021/05/17 Oblique detonation Wave complex Instability Thermal choking Expansion corner |
| Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13 Authors: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇) Adobe PDF(5176Kb)  |  Favorite  |  View/Download:273/111  |  Submit date:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8 Authors: Ma KF(马凯夫); Zhang ZJ(张子健); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(1657Kb)  |  Favorite  |  View/Download:275/97  |  Submit date:2020/08/26 Scramjet engines Shock-induced combustion ramjet engines Supersonic combustion Chapman-Jouguet detonation |
| 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) View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download:347/121  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 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 |