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Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences 期刊论文
ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12
Authors:  Lin MY(林明月);  Yang F(杨帆);  Hu ZM(胡宗民);  Han GL(韩桂来)
Favorite  |  View/Download：16/0  |  Submit date：2024/05/27
Shock waves  Shock-shock interaction  Theoretical analysis  Hysteresis  
Numerical Study on the Aerodynamic Heating Characteristics of the Cantilevered Injection System for Oblique Detonation Engine Inlets 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 10, 页码: 18
Authors:  Yang F(杨帆);  Lin MY(林明月);  Hu ZM(胡宗民);  Han GL(韩桂来)
Adobe PDF(8946Kb)  |  Favorite  |  View/Download：89/5  |  Submit date：2023/11/28
oblique detonation engine  cantilevered injection  localized high heat flux  boundary layer separation  reattachment  
Analytic investigation on error of heat flux measurement and data processing for large curvature models in hypersonic shock tunnels 期刊论文
APPLIED MATHEMATICS LETTERS, 2022, 卷号: 134, 页码: 8
Authors:  Han GL(韩桂来);  Qi L(齐力);  Jiang ZL(姜宗林)
Adobe PDF(1715Kb)  |  Favorite  |  View/Download：283/45  |  Submit date：2022/11/08
Heat flux  Measurement  Data processing  Error  Approximate solution  
Experimental study on the evolution of mode waves in laminar boundary layer on a large-scale flat plate 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 1, 页码: 16
Authors:  Liu MK(刘美宽);  Han GL(韩桂来);  Jiang ZL(姜宗林)
Adobe PDF(5472Kb)  |  Favorite  |  View/Download：280/45  |  Submit date：2022/03/05