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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)
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Shock interactions  Transitional configuration  Aerodynamic heating  Shear layer  Mach interaction  
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  
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:363/179  |  Submit date:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
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:333/100  |  Submit date:2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
Effects of dimensional wall temperature on velocity-temperature correlations in supersonic turbulent channel flow of thermally perfect gas 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2019, 卷号: 62, 期号: 6, 页码: AR64711
Authors:  Chen XP;  Li XL(李新亮);  Zhu ZC
View  |  Adobe PDF(1844Kb)  |  Favorite  |  View/Download:337/104  |  Submit date:2019/04/11
direct numerical simulation  velocity-temperature correlation  supersonic flow  channel flow  thermally perfect gas  strong Reynolds analogy  
Shock oscillation in highly underexpanded jets 期刊论文
CHINESE PHYSICS B, 2018, 卷号: 27, 期号: 9, 页码: 94705
Authors:  Li XP;  Zhou R;  Chen XP;  Fan XJ(范学军);  Xie GS
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highly underexpanded jets  shock oscillation  large eddy simulation  
Effect of uniform blowing or suction on hypersonic spatially developing turbulent boundary layers 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 6, 页码: 664702
Authors:  Chen Z(陈哲);  Yu ZP(于长平);  Li L(李理);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Influences of affiliated components and train length on the train wind 期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 2, 页码: 191-205
Authors:  Guo DL(郭迪龙);  Shang KM;  Zhang Y;  Yang GW(杨国伟);  Sun ZX(孙振旭);  Guo, DL
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Aerothermal characteristics of bleed slot in hypersonic flows 期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2015, 卷号: 58, 期号: 10, 页码: 104703
Authors:  Yue LJ(岳连捷);  Lu HB;  Xu X;  Chang XY;  Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View  |  Adobe PDF(3301Kb)  |  Favorite  |  View/Download:409/108  |  Submit date:2016/01/08
Boundary Layer Control  Boundary Layer Heat Flow  Shock Wave Interactions  Separated Flows  
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:  Zhao R(赵瑞);  Yan C(阎超);  Yu J(于剑);  Li XL(李新亮);  Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
Adobe PDF(1609Kb)  |  Favorite  |  View/Download:918/309  |  Submit date:2013/09/21
Baldwin-lomax Model  Boundary Layers  Computational Aerodynamics  Entropy  Supersonic Flows  Turbulence Models