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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：89/5  |  Submit date：2023/11/28
oblique detonation engine  cantilevered injection  localized high heat flux  boundary layer separation  reattachment  
Wall heat flux in supersonic turbulent expansion flow with shock impingement 期刊论文
JOURNAL OF TURBULENCE, 2023, 页码: 29
Authors:  Tong FL(童福林);  Duan JY(段俊亦);  Yuan, Xianxu;  Li XL(李新亮)
Adobe PDF(7217Kb)  |  Favorite  |  View/Download：87/3  |  Submit date：2023/10/16
Expansion corner  turbulent boundary layer  shock impingement  wall heat flux  
Hypersonic shock wave and turbulent boundary layer interaction in a sharp cone/flare model 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 3, 页码: 80-95
Authors:  Tong FL(童福林);  Duan JY(段俊亦);  Lai, Jiang;  Sun, Dong;  Yuan, Xianxu
Adobe PDF(4757Kb)  |  Favorite  |  View/Download：52/2  |  Submit date：2023/04/20
Shock wave  Hypersonic turbulent  boundary layer  Heat transfer  Skin friction decomposition  Direct numerical simulation  
Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  Favorite  |  View/Download：417/78  |  Submit date：2022/08/24
Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels