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Mitigation of Shock-Induced Separation Using Square-Shaped Micro-Serrations-A Preliminary Study 期刊论文
AEROSPACE, 2024, 卷号: 11, 期号: 2, 页码: 16
Authors:  Yu FY(于方游);  Gao ZB(高占彪);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Chen H(陈昊)
Favorite  |  View/Download：25/0  |  Submit date：2024/05/21
micro-serration  separation control  shock wave/boundary layer interaction  
斜激波串非对称特性研究 期刊论文
推进技术, 2022, 卷号: 43, 期号: 04, 页码: 101-108
Authors:  黄庭隆;  贺理浩;  岳连捷
Adobe PDF(1632Kb)  |  Favorite  |  View/Download：192/52  |  Submit date：2022/06/10
隔离段  斜激波串  非对称性  建模分析  数值仿真  
高马赫数超燃冲压发动机技术研究进展 期刊论文
力学学报, 2022, 卷号: 54, 期号: 02, 页码: 263-288
Authors:  岳连捷;  张旭;  张启帆;  陈科挺;  李进平;  陈昊;  姚卫;  仲峰泉;  李飞;  王春;  陈宏
Adobe PDF(2622Kb)  |  Favorite  |  View/Download：581/111  |  Submit date：2022/03/16
高马赫数  超燃冲压发动机  热化学非平衡  超声速燃烧  低雷诺数流动  激波风洞  飞行试验  
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:  Yao W(姚卫);  Liu H(刘杭);  Yue LJ(岳连捷);  Xiao YB(肖雅彬)
Adobe PDF(2954Kb)  |  Favorite  |  View/Download：302/73  |  Submit date：2021/11/15
Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:  Xue, Rui;  Zheng, Xing;  Yue LJ(岳连捷);  Zhang, Qian;  He, Xin;  Yang, Jing;  Weng, Chao;  Li, Zhihao
Adobe PDF(5483Kb)  |  Favorite  |  View/Download：163/49  |  Submit date：2022/10/25
Boundary layer combustion  Skin-friction reduction  Supersonic combustion  Scramjet engine  
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：226/60  |  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：357/239  |  Submit date：2020/08/26
Compressible boundary layer combustion  Skin-friction reduction  Boundary layer transition  Transition k-kl-w model  Hydrogen combustion  
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
Adobe PDF(1289Kb)  |  Favorite  |  View/Download：235/62  |  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：376/115  |  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)
View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download：364/128  |  Submit date：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation