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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：217/51  |  Submit date：2021/06/07
Direct numerical simulation  Low-frequency unsteadiness  Shock waves  Turbulent boundary layer  Wavy-wall  
Multi-scale molecular dynamics simulations and applications on mechanosensitive proteins of integrins* 期刊论文
CHINESE PHYSICS B, 2021, 卷号: 30, 期号: 3, 页码: 8
Authors:  Lv SQ(吕守芹);  Ding QH(丁奇寒);  Zhang MK(张明坤);  Long M(龙勉)
Adobe PDF(834Kb)  |  Favorite  |  View/Download：282/88  |  Submit date：2021/04/19
molecular dynamics simulations  mechanosensitive protein  allosteric dynamics  integrin  
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：347/176  |  Submit date：2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Rejuvenation in Hot-Drawn Micrometer Metallic Glassy Wires* 期刊论文
CHINESE PHYSICS LETTERS, 2020, 卷号: 37, 期号: 1, 页码: 4
Authors:  Dong J(董杰);  Feng YH(冯义辉);  Huan Y(郇勇);  Yi J;  Wang WH;  Bai HY;  Sun BA
Adobe PDF(1084Kb)  |  Favorite  |  View/Download：402/89  |  Submit date：2020/03/11
71  23  Cq  
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：442/192  |  Submit date：2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty