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高速进气道低马赫数不起动特性及马赫数影响规律 期刊论文
推进技术, 2020, 卷号: 42, 期号: 10, 页码: 2207-2217
作者:  贺理浩;  张启帆;  岳连捷;  张新宇;  王卫星;  谭慧俊
Adobe PDF(9600Kb)  |  收藏  |  浏览/下载:235/34  |  提交时间:2021/11/12
高速进气道  低马赫数不起动  非定常  气动力  自起动  
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:185/43  |  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:253/103  |  提交时间:2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
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
作者:  Xue R;  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3912Kb)  |  收藏  |  浏览/下载:331/226  |  提交时间: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
作者:  Yang L;  岳连捷;  张启帆;  张新宇
Adobe PDF(1289Kb)  |  收藏  |  浏览/下载:200/48  |  提交时间: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
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:337/111  |  提交时间: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
作者:  杨理;  岳连捷;  张新宇
Adobe PDF(5656Kb)  |  收藏  |  浏览/下载:163/45  |  提交时间:2021/01/29