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Experimental study on the effects of the cone nose-tip bluntness 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 10, 页码: 7
Authors:  Liu MK(刘美宽);  Han GL(韩桂来);  Li, Zongxian;  Jiang ZL(姜宗林)
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Direct numerical simulation of shock-wave/boundary layer interaction controlled with convergent-divergent riblets 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 8, 页码: 18
Authors:  Guo TB(郭同彪);  Fang, Jian;  Zhang J(张继);  Li XL(李新亮)
Adobe PDF(11403Kb)  |  Favorite  |  View/Download:196/38  |  Submit date:2022/08/28
A hybrid kinetic WGVC-WENO scheme for compressible flows 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 229, 页码: 12
Authors:  He K(何康);  Liu HW(刘洪伟);  Li XL(李新亮)
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Gas kinetic theory  WGVC-WENO methods  Hybrid flux  Numerical dissipation  
Shock wave and turbulent boundary layer interaction in a double compression ramp 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 229, 页码: 15
Authors:  Tong FL(童福林);  Duan JY(段俊亦);  Li XL(李新亮)
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Shock wave  Turbulent boundary layer  Double compression ramp  Direct numerical simulation  
Statistical characteristics of turbulent mixing in spherical and cylindrical converging Richtmyer-Meshkov instabilities 期刊论文
JOURNAL OF FLUID MECHANICS, 2021, 卷号: 928, 页码: 32
Authors:  Li XL(李新亮);  Fu YW(符耀威);  Yu ZP(于长平);  Li, Li
Adobe PDF(1452Kb)  |  Favorite  |  View/Download:231/40  |  Submit date:2022/01/12
compressible turbulence  shock waves  turbulent mixing  
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:  Yao W(姚卫);  Liu H(刘杭);  Yue LJ(岳连捷);  Xiao YB(肖雅彬)
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Hypersonic combustion  Hydrogen  Improved Delayed Detached Eddy  Simulation (IDDES)  Dynamic zone flamelet model  Scramjet  
Theoretical, numerical and experimental study of hypersonic boundary layer transition: Blunt circular cone 期刊论文
APPLIED THERMAL ENGINEERING, 2021, 卷号: 194, 页码: 14
Authors:  Chen, Jianqiang;  Yi, Shihe;  Li XL(李新亮);  Han GL(韩桂来);  Zhang, Yifeng;  Yang, Qiang;  Yuan, Xianxu
Adobe PDF(11175Kb)  |  Favorite  |  View/Download:342/96  |  Submit date:2021/08/03
Hypersonic boundary layer  Stability  Transition  Thermal protection  
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)
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Direct numerical simulation  Low-frequency unsteadiness  Shock waves  Turbulent boundary layer  Wavy-wall  
Subgrid-scale helicity equation model for large-eddy simulation of turbulent flows 期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 3, 页码: 13
Authors:  Qi H(齐涵);  Li XL(李新亮);  Yu ZP(于长平)
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Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  Favorite  |  View/Download:339/173  |  Submit date:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique