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| Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17
作者: Liu H(刘杭); Yao W(姚卫) ; Zhang X(张旭); Zhang XY(张晓源); Liu, Jianwen; Yue LJ(岳连捷); Sun QH(孙泉华)
  收藏 | 浏览/下载：30/0 | 提交时间：2024/03/11
Scramjet Dynamic Zone Flamelet Model High Enthalpy Shock Tunnel Combustors Improved Delayed Detached Eddy Simulation Vibrational Energy nonequilibrium heating cooling effects thermal nonequilibrium chemical nonequilibrium hydrogen |
| Effects of Thermal/Chemical Nonequilibrium on a High-Mach Ethylene-Fueled Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023, 页码: 18
作者: Yao W(姚卫); Liu H(刘杭); Zhang Z(张政); Zhang X(张旭); Yue LJ(岳连捷); Zhang XY(张晓源); Li JP(李进平)
 Adobe PDF(689Kb) | 收藏 | 浏览/下载：181/0 | 提交时间：2023/02/27 |
| Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
作者: Zhou GX(周功喜); Zhang X(张旭); Li JP(李进平); Zhang XY(张晓源); Zhang SZ(张仕忠); Lin X(林鑫); Li F(李飞); Chen H(陈宏); Yue LJ(岳连捷); Yu XL(余西龙)
Adobe PDF(4108Kb) | 收藏 | 浏览/下载：329/47 | 提交时间：2021/09/07
High mach number scramjet Circular cross-section TDLAS Multi-view simultaneous imaging POD |
| 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
作者: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇)
Adobe PDF(8067Kb) | 收藏 | 浏览/下载：378/62 | 提交时间：2021/03/03
Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
作者: Xue R(薛瑞); Zheng X; Yue LJ(岳连捷); Zhang SK; Weng C
Adobe PDF(3251Kb) | 收藏 | 浏览/下载：339/111 | 提交时间：2020/07/06
Compressible boundary layer combustion Skin-friction reduction Shock train/flame interaction |
| 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 |
| 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 |
