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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：596/114  |  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  
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)
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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：364/243  |  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
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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：385/115  |  Submit date：2020/07/06
Compressible boundary layer combustion  Skin-friction reduction  Shock train/flame interaction  
基于工程转捩模型的高超声速进气道特性 期刊论文
北京航空航天大学学报, 2018, 卷号: 44, 期号: 7, 页码: 1408-1418
Authors:  杨慧;  路文睿;  李虹杨;  岳连捷
View  |  Adobe PDF(975Kb)  |  Favorite  |  View/Download：298/68  |  Submit date：2018/10/24
高超声速进气道  转捩模型  飞行高度  湍流度  数值模拟  
Aerothermal characteristics of bleed slot in hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
Authors:  Yue LJ(岳连捷);  Lu HB;  Xu X;  Chang XY;  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(3301Kb)  |  Favorite  |  View/Download：411/109  |  Submit date：2016/01/08
Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows