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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
Authors:  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)
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high-lift devices  computational fluid dynamics  computational aeroacoustics  Kriging surrogate model  optimization design  
Vibrational Energy Transfer in CO+N-2 Collisions: A Database for V-V and V-T/R Quantum-Classical Rate Coefficients 期刊论文
MOLECULES, 2021, 卷号: 26, 期号: 23, 页码: 27
Authors:  Hong QZ(洪启臻);  Bartolomei, Massimiliano;  Coletti, Cecilia;  Lombardi, Andrea;  Sun QH(孙泉华);  Pirani, Fernando
Adobe PDF(735Kb)  |  Favorite  |  View/Download:279/20  |  Submit date:2022/03/05
vibrational energy transfer  inelastic scattering  potential energy surface  rate coefficients database  quantum-classical nuclear dynamics  quasi-classical trajectories  
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
Authors:  Jiang YZ;  Wen CY;  Zhang DL(张德良)
Adobe PDF(6207Kb)  |  Favorite  |  View/Download:265/102  |  Submit date: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
Authors:  Zhang W;  Wang S;  Wang Q;  Ju SJ(鞠胜军);  Yan C
Adobe PDF(2859Kb)  |  Favorite  |  View/Download:292/117  |  Submit date: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
Authors:  Jiang WT;  Wang XJ;  Wang RX(王睿星);  Shi QH;  Zhu JJ
Adobe PDF(6028Kb)  |  Favorite  |  View/Download:275/78  |  Submit date: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
Authors:  Ju SJ(鞠胜军);  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3818Kb)  |  Favorite  |  View/Download:445/114  |  Submit date: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
Authors:  Ju SJ;  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3216Kb)  |  Favorite  |  View/Download:352/91  |  Submit date: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
Authors:  Wang RX(王睿星);  Wang, ZW;  Zheng HW(郑洪伟);  Song HW(宋宏伟)
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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
Authors:  Zhu JJ;  Wang XJ;  Zhang HG;  Li YW;  Wang RX(王睿星);  Qiu ZP
View  |  Adobe PDF(2082Kb)  |  Favorite  |  View/Download:453/195  |  Submit date: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
Authors:  Zhong K;  Yan C;  Chen SS;  Wang XY(王小永);  Ju SJ
View  |  Adobe PDF(8635Kb)  |  Favorite  |  View/Download:242/73  |  Submit date:2019/05/29
Aeroheating  Heatshield configuration  Sphere-cone angle  Mars  Turbulent