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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 Authors: 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)![](/image/person.jpg)
![](/themes/default/image/downing1.png) Favorite  |  View/Download:61/0  |  Submit date: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 Authors: 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)![](/image/person.jpg)
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| Numerical study on wave configuration of wedge-induced oblique detonation wave: Reactive boundary layer effect 期刊论文 PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 11, 页码: 11 Authors: Yang L(杨理); Yue LJ(岳连捷) ; Yu, Dehai ; Chen, Zheng
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| Onset of Oblique Detonation Waves for a Cavity-Based Wedge 期刊论文 AIAA JOURNAL, 2022, 页码: 14 Authors: Yang, Li; Yue LJ(岳连捷) ; Zhang QF(张启帆)![](/image/person.jpg)
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| 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 Authors: 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)![](/image/person.jpg)
Adobe PDF(4108Kb)  |   Favorite  |  View/Download:348/56  |  Submit date: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 Authors: Tong XT(仝晓通) ; Zhang QF(张启帆) ; Yue LJ(岳连捷) ; Zhang XY(张新宇)![](/image/person.jpg)
Adobe PDF(8067Kb)  |   Favorite  |  View/Download:427/82  |  Submit date:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188 Authors: Huang TL(黄庭隆); Yue LJ(岳连捷) ; Ma SH(马生虎); Zhang QF(张启帆) ; Zhang, Peng; Zhang XY(张新宇)![](/image/person.jpg)
Adobe PDF(3937Kb)  |   Favorite  |  View/Download:235/62  |  Submit date:2021/03/30 Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| 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)![](/image/person.jpg)
Adobe PDF(5176Kb)  |   Favorite  |  View/Download:299/116  |  Submit date:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 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 Authors: Xue R(薛瑞); Zheng X; Yue LJ(岳连捷) ; Zhang SK; Weng C
Adobe PDF(3251Kb)  |   Favorite  |  View/Download:384/115  |  Submit date: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 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)![](/image/person.jpg)
View  |   Adobe PDF(3862Kb)  |   Favorite  |  View/Download:371/133  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |