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Numerical investigation for subsonic performance of the high-pressure capturing wing configuration with wing dihedral 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 16
Authors:  Chang SY(常思源);  Xiao Y(肖尧);  Li GL(李广利);  Tian ZW(田中伟);  Cui K(崔凯)
Favorite  |  View/Download:89/0  |  Submit date:2024/01/22
High-pressure capturing wing  Subsonic  Numerical simulation  Wing dihedral  Stability  
Optimal design of E-type coaxial thermocouples for transient heat measurements in shock tunnels 期刊论文
APPLIED THERMAL ENGINEERING, 2023, 卷号: 218, 页码: 11
Authors:  Qi L(齐力);  Han GL(韩桂来);  Jiang ZL(姜宗林)
Adobe PDF(5274Kb)  |  Favorite  |  View/Download:197/7  |  Submit date:2022/11/21
Coaxial thermocouples  Lateral heat conduction  Maximum temperature point  Optimal design  Numerical simulation  
Numerical investigations of the lateral heat transfer in coaxial thermocouples 期刊论文
NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2022, 页码: 19
Authors:  Qi L(齐力);  Han GL(韩桂来);  Hu ZM(胡宗民);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(3726Kb)  |  Favorite  |  View/Download:272/54  |  Submit date:2022/07/18
Coaxial thermocouples  lateral heat transfer  maximum temperature point  numerical simulation  surface heat flux  
Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors:  Tong FL(童福林);  Sun D(孙栋);  Li XL(李新亮)
Adobe PDF(4402Kb)  |  Favorite  |  View/Download:212/50  |  Submit date:2021/06/07
Direct numerical simulation  Low-frequency unsteadiness  Shock waves  Turbulent boundary layer  Wavy-wall  
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Ma SG(马素刚);  Zhang XY(张新宇)
View  |  Adobe PDF(4075Kb)  |  Favorite  |  View/Download:309/91  |  Submit date:2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
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:539/173  |  Submit date:2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation