|
Selected(0)Clear
Items/Page: Sort: |
| 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：301/111 | 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：310/77 | Submit date：2021/11/15
Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇)
Adobe PDF(8067Kb) | Favorite | View/Download：429/83 | Submit date：2021/03/03
Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(2608Kb) | Favorite | View/Download：282/123 | Submit date：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)
Adobe PDF(2023Kb) | Favorite | View/Download：366/113 | Submit date：2020/11/30
Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| 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)
 Adobe PDF(2678Kb) | Favorite | View/Download：290/63 | 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)
Adobe PDF(2678Kb) | Favorite | View/Download：238/77 | 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：372/133 | 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)
Adobe PDF(2894Kb) | Favorite | View/Download：427/155 | Submit date：2020/03/21
Supersonic combustion Turbulence jet Direct numerical simulations Coherent structures |
| Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263
Authors: Fang YS(方宜申); Hu ZM(胡宗民); Teng HH(滕宏辉); Jiang ZL(姜宗林); Ng HD
Adobe PDF(2663Kb) | Favorite | View/Download：407/103 | Submit date：2018/02/08
Oblique Detonation Equivalence Ratio Mixture Inhomogeneity Detailed Chemistry |
