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基于高温气体效应的磁流体流动控制研究进展 期刊论文
力学学报, 2021, 卷号: 53, 期号: 06, 页码: 1515-1531
作者:  罗凯;  汪球;  李逸翔;  李进平;  赵伟
Adobe PDF(12949Kb)  |  收藏  |  浏览/下载:266/71  |  提交时间:2021/11/12
高超声速  高温真实气体效应  磁流体动力学  流动控制  气动力/热  
Space-Time Conservation Element and Solution Element Method and Its Applications 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 12, 页码: 5408-5430
作者:  Jiang YZ;  Wen CY;  Zhang DL(张德良)
Adobe PDF(6207Kb)  |  收藏  |  浏览/下载:242/97  |  提交时间:2021/02/09
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:255/98  |  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:247/70  |  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:411/103  |  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:319/86  |  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:276/86  |  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:421/189  |  提交时间:2020/03/21
Hypersonic vehicle  Six sigma robust optimization  Successive response surface  Thermal protection system  Uncertainty  
Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules 期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198
作者:  Zhong K;  Yan C;  Chen SS;  Wang XY(王小永);  Ju SJ
浏览  |  Adobe PDF(8635Kb)  |  收藏  |  浏览/下载:213/71  |  提交时间:2019/05/29
Aeroheating  Heatshield configuration  Sphere-cone angle  Mars  Turbulent  
Spectral measurements of hypervelocity flow in an expansion tunnel 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
作者:  Yuan CK(苑朝凯);  Zhou K(周凯);  Liu YF(刘云峰);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1468Kb)  |  收藏  |  浏览/下载:328/95  |  提交时间:2019/04/11
Spectral measurement  Hypervelocity flow  Radiation  Expansion tunnel