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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：88/5  |  Submit date：2023/11/28
oblique detonation engine  cantilevered injection  localized high heat flux  boundary layer separation  reattachment  
Transitional criterion and hysteresis of multiple shock-shock interference 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 4, 页码: 46110
Authors:  Lin MY(林明月);  Yang F(杨帆);  Hu ZM(胡宗民);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5430Kb)  |  Favorite  |  View/Download：85/7  |  Submit date：2023/06/15
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：63/3  |  Submit date：2023/04/20
Shock interactions  Transitional configuration  Aerodynamic heating  Shear layer  Mach interaction