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| 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)
  Favorite | View/Download：104/0 | 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)
Favorite | View/Download：0/0 | Submit date：2021/03/30
Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors: Xue R; Zheng X; Yue LJ(岳连捷); Zhang SK; Weng C
 Adobe PDF(3912Kb) | Favorite | View/Download：20/2 | Submit date：2020/08/26
Compressible boundary layer combustion Skin-friction reduction Boundary layer transition Transition k-kl-w model Hydrogen combustion |
| 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：6/0 | Submit date：2020/11/30
Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors: Yang L; 岳连捷; 张启帆; 张新宇
Favorite | View/Download：10/0 | Submit date：2021/01/12 |
| 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：43/3 | Submit date：2020/07/06
Compressible boundary layer combustion Skin-friction reduction Shock train/flame interaction |
| 斜爆轰波的波角和法向速度-曲率关系初步探究 期刊论文
航空学报, 2020, 卷号: 41, 页码: 123701
Authors: 杨理; 岳连捷; 张新宇
Favorite | View/Download：6/0 | Submit date：2021/01/29 |
| 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：82/14 | Submit date：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
Authors: Meng Y(孟宇); Gu HB(顾洪斌); Zhuang JH(庄金衡); Sun WM(孙文明); Gao ZB(高占彪); Lian H(连欢); Yue LJ(岳连捷); Chang XY(张新宇)
View | Adobe PDF(3099Kb) | Favorite | View/Download：109/29 | Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| 全流量捕获的高超声速变截面内转式进气道快速设计方法 专利
发明专利. 全流量捕获的高超声速变截面内转式进气道快速设计方法, 专利号: ZL201810269911.2, 申请日期: 2018-03-29,
Inventors: 肖鸿文; 岳连捷; 肖雅彬
View | Adobe PDF(404Kb) | Favorite | View/Download：43/4 | Submit date：2020/02/10 |
