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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
Adobe PDF(4548Kb)  |  Favorite  |  View/Download：167/43  |  Submit date：2022/12/29
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)
Adobe PDF(5573Kb)  |  Favorite  |  View/Download：196/46  |  Submit date：2022/03/05
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
Authors:  Huang TL(黄庭隆);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang P;  Zhao QJ
Adobe PDF(2961Kb)  |  Favorite  |  View/Download：221/44  |  Submit date：2022/02/17
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：399/69  |  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)
Adobe PDF(3937Kb)  |  Favorite  |  View/Download：208/52  |  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)
Adobe PDF(5176Kb)  |  Favorite  |  View/Download：277/113  |  Submit date：2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
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：351/124  |  Submit date：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
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Chang XY(张新宇)
View  |  Adobe PDF(3918Kb)  |  Favorite  |  View/Download：539/173  |  Submit date：2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation