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Analytic investigation on error of heat flux measurement and data processing for large curvature models in hypersonic shock tunnels 期刊论文
APPLIED MATHEMATICS LETTERS, 2022, 卷号: 134, 页码: 8
Authors:  Han GL(韩桂来);  Qi L(齐力);  Jiang ZL(姜宗林)
Adobe PDF(1715Kb)  |  Favorite  |  View/Download：298/52  |  Submit date：2022/11/08
Heat flux  Measurement  Data processing  Error  Approximate solution  
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)
Adobe PDF(2954Kb)  |  Favorite  |  View/Download：303/74  |  Submit date：2021/11/15
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：364/103  |  Submit date：2021/08/03
Hypersonic boundary layer  Stability  Transition  Thermal protection  
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：357/178  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Study on turbulence drag reduction of riblet plate in hypersonic turbulent flows 期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS C, 2020, 卷号: 31, 期号: 3, 页码: 11
Authors:  Zhou H(周浩);  Li XL(李新亮);  Yu ZP(于长平)
Adobe PDF(3698Kb)  |  Favorite  |  View/Download：285/84  |  Submit date：2020/05/18
Hypersonic  turbulence control  numerical simulation  riblet plate  
Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
Authors:  Zhu JJ;  Wang XJ;  Zhang HG;  Li YW;  Wang RX(王睿星);  Qiu ZP
View  |  Adobe PDF(2082Kb)  |  Favorite  |  View/Download：459/196  |  Submit date：2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty