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Aerodynamic-Aeroacoustic Optimization of a Baseline Wing and Flap Configuration 期刊论文
APPLIED SCIENCES-BASEL, 2022, 卷号: 12, 期号: 3, 页码: 19
作者:  Ju SJ(鞠胜军);  Sun ZX(孙振旭);  Guo DL(郭迪龙);  Yang GW(杨国伟);  Wang YT(王业腾);  Yan C(闫畅)
Adobe PDF(12043Kb)  |  收藏  |  浏览/下载:273/38  |  提交时间:2022/03/28
high-lift devices  computational fluid dynamics  computational aeroacoustics  Kriging surrogate model  optimization design  
Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260
作者:  Zhang W;  Wang S;  Wang Q;  Ju SJ(鞠胜军);  Yan C
Adobe PDF(2859Kb)  |  收藏  |  浏览/下载:264/102  |  提交时间:2021/02/09
Aerodynamic thermal  Opposing jets  Parametric sensitivity analysis  Uncertainty quantification  Analysis of Variance  Non-Intrusive Polynomial Chaos  
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
作者:  Jiang WT;  Wang XJ;  Wang RX(王睿星);  Shi QH;  Zhu JJ
Adobe PDF(6028Kb)  |  收藏  |  浏览/下载:261/76  |  提交时间:2020/11/30
Thermal protection system  Nonprobabilistic optimization  Sensitivity analysis  Uncertainty analysis  Model updating  
Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10
作者:  Ju SJ(鞠胜军);  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3818Kb)  |  收藏  |  浏览/下载:427/106  |  提交时间:2020/11/30
Optimization design  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 171, 页码: 300-310
作者:  Ju SJ;  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3216Kb)  |  收藏  |  浏览/下载:331/88  |  提交时间:2020/05/18
Computational fluid dynamics  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
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
作者:  Wang RX(王睿星);  Wang, ZW;  Zheng HW(郑洪伟);  Song HW(宋宏伟)
Adobe PDF(4182Kb)  |  收藏  |  浏览/下载:289/88  |  提交时间:2020/06/22
Coupled flow-thermal analysis  Thermal protection system  Basic direct correction method (BDCM)  Improved DCM (IDCM)  Iteration solution method (ISM)  
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
作者:  Zhu JJ;  Wang XJ;  Zhang HG;  Li YW;  Wang RX(王睿星);  Qiu ZP
浏览  |  Adobe PDF(2082Kb)  |  收藏  |  浏览/下载:432/192  |  提交时间:2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty  
High-power laser resistance of filled sandwich panel with truss cores: Ablation mechanisms and numerical simulation 期刊论文
COMPOSITE STRUCTURES, 2018, 卷号: 203, 页码: 574-584
作者:  Wang JT(王江涛);  Yuan W(袁武);  Liu YW;  Song HW(宋宏伟);  Huang CG(黄晨光)
浏览  |  Adobe PDF(4619Kb)  |  收藏  |  浏览/下载:335/80  |  提交时间:2018/10/30
Laser ablation  Sandwich structure  Ablative material  Thermal-physical-chemical process  Numerical simulation