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Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
Authors:  Luo K(罗凯);  Wang Q(汪球);  Li JW(栗继伟);  Li JP(李进平);  Zhao W(赵伟)
Adobe PDF(2023Kb)  |  Favorite  |  View/Download:339/106  |  Submit date:2020/11/30
Quasi-one-dimensional  Detonation  Shock tunnel  Shock speed  
A multi-time scale solution strategy for an elastomeric aircraft 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 13
Authors:  Yang L(杨磊);  Sun QH(孙泉华)
Adobe PDF(1858Kb)  |  Favorite  |  View/Download:224/90  |  Submit date:2020/08/26
Flight dynamic simulation  Multi-time scale  Elastomeric aircraft  Reduced order models  Store separation  
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:544/175  |  Submit date:2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation  
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors:  Yue LJ(岳连捷);  Jia YN(贾轶南);  Xu X;  Zhang XY(张新宇);  Zhang P(张鹏)
View  |  Adobe PDF(2110Kb)  |  Favorite  |  View/Download:387/138  |  Submit date:2018/10/30
Inlet restart  Cowl shock  Shock wave boundary layer interactions