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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：41/0  |  Submit date：2024/05/27
Shock waves  Shock-shock interaction  Theoretical analysis  Hysteresis  
爆轰双向驱动双状态并行技术的原理性研究 期刊论文
中国科学:技术科学, 2024, 页码: 1-15
Authors:  杨帆;  林明月;  胡宗民;  韩桂来
Adobe PDF(1748Kb)  |  Favorite  |  View/Download：117/31  |  Submit date：2024/03/01
高焓试验气流  爆轰双向驱动  激波风洞  热化学反应流动  缝合界面条件  
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：111/9  |  Submit date：2023/11/28
oblique detonation engine  cantilevered injection  localized high heat flux  boundary layer separation  reattachment  
Transitional wave configurations between Type III and Type IV oblique shock/bow shock interactions 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 96-106
Authors:  Peng J(彭俊);  Li S(李帅);  Yang F(杨帆);  Lin MY(林明月);  Han GL(韩桂来);  Hu ZM(胡宗民)
Adobe PDF(2838Kb)  |  Favorite  |  View/Download：66/6  |  Submit date：2023/04/20
Shock interactions  Transitional configuration  Aerodynamic heating  Shear layer  Mach interaction