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Experimental study of the high-power laser resistance of ablative material-filled sandwich panels with truss cores under hypersonic airflow 期刊论文
COMPOSITE STRUCTURES, 2022, 卷号: 301, 页码: 116139
Authors:  Yuan W(袁武);  Wang JT(王江涛);  Wang RX(王睿星);  Wang Z(王喆);  Song HW(宋宏伟);  Huang CG(黄晨光)
Adobe PDF(9765Kb)  |  Favorite  |  View/Download：201/58  |  Submit date：2022/10/23
Sandwich panel  Thermal insulation  Lightweight structure  Failure point  
Nonprobabilistic uncertain model updating and optimization design of thermal protection system 期刊论文
APPLIED THERMAL ENGINEERING, 2020, 卷号: 180, 页码: 14
Authors:  Jiang WT;  Wang XJ;  Wang RX(王睿星);  Shi QH;  Zhu JJ
Adobe PDF(6028Kb)  |  Favorite  |  View/Download：279/80  |  Submit date：2020/11/30
Thermal protection system  Nonprobabilistic optimization  Sensitivity analysis  Uncertainty analysis  Model updating  
Comparison of Strategies for Coupled Flow-Thermal Analysis of Thermal Protection System at Hypersonic Flight Condition 期刊论文
INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2020, 卷号: 21, 期号: 2, 页码: 347-362
Authors:  Wang RX(王睿星);  Wang, ZW;  Zheng HW(郑洪伟);  Song HW(宋宏伟)
Adobe PDF(4182Kb)  |  Favorite  |  View/Download：306/89  |  Submit date：2020/06/22
Coupled flow-thermal analysis  Thermal protection system  Basic direct correction method (BDCM)  Improved DCM (IDCM)  Iteration solution method (ISM)  
Performance improvement of integrated thermal protection system using shaped-stabilized composite phase change material 期刊论文
APPLIED THERMAL ENGINEERING, 2020, 卷号: 164, 页码: 14
Authors:  Cao CY;  Wang RX(王睿星);  Xing XD(邢晓冬);  Liu WF(刘文峰);  Song HW(宋宏伟);  Huang CG(黄晨光)
Adobe PDF(3976Kb)  |  Favorite  |  View/Download：494/126  |  Submit date：2020/03/11
Corrugated core integrated thermal protection system  Thermal bridge phenomenon  Shaped-stabilized composite phase change materials  Heat insulating property  Thermal-mechanical coupling analysis  Global optimization procedure  
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：457/196  |  Submit date：2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty