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| 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 |
| Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow 期刊论文
AIAA JOURNAL, 2022, 页码: 9
作者: Wu ZJ(吴振杰); Zhang QF(张启帆); Zhang X(张旭); Luo WH(罗苇航); Gao ZB(高占彪); Yue LJ(岳连捷)
Adobe PDF(3049Kb) | 收藏 | 浏览/下载：154/22 | 提交时间：2022/07/18 |
| Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor 期刊论文
AIAA JOURNAL, 2022, 页码: 7
作者: Zhang X(张旭); Zhang QF(张启帆); Wu ZJ(吴振杰); Yue LJ(岳连捷); Gao ZB(高占彪); Luo WH(罗苇航); Chen H(陈昊)
Adobe PDF(1382Kb) | 收藏 | 浏览/下载：151/27 | 提交时间：2022/03/22 |
| Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
作者: Chen KT(陈科挺); Yue LJ(岳连捷); Zhang XY(张新宇)
Adobe PDF(511Kb) | 收藏 | 浏览/下载：199/39 | 提交时间：2022/01/12
Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| Hysteresis of Shock Train Movement in the Isolator with a Ramp 期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882
作者: Huang TL(黄庭隆); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang P; Zhao QJ
Adobe PDF(2961Kb) | 收藏 | 浏览/下载：204/42 | 提交时间：2022/02/17 |
| 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 |
| 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
作者: 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)
Adobe PDF(3937Kb) | 收藏 | 浏览/下载：188/45 | 提交时间：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
作者: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇)
Adobe PDF(5176Kb) | 收藏 | 浏览/下载：254/103 | 提交时间：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
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)
 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 |
