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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 |