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Uncertainty-Based Comprehensive Optimization Design for the Thermal Protection System of Hypersonic Wing Structure 期刊论文
APPLIED SCIENCES-BASEL, 2022, 卷号: 12, 期号: 21, 页码: 19./通讯作者：Wang, Ruixing, Luo, Yan
Authors:  Wang RX(王睿星);  Luo, Yan
Adobe PDF(6087Kb)  |  Favorite  |  View/Download：292/91  |  Submit date：2022/12/20
uncertainty-based optimization design  uncertainty propagation analysis  aerodynamic shape  multilayer TPS tile  hypersonic wing  
Multi-objective robust optimization of a solar power tower plant under uncertainty 期刊论文
ENERGY, 2022, 卷号: 238, 页码: 11./通讯作者：Chu, Fengming, Wang, Ruixing
Authors:  Luo, Yan;  Wang, Zhiyuan;  Zhu, Jiamin;  Lu, Tao;  Xiao, Gang;  Chu, Fengming;  Wang RX(王睿星)
Adobe PDF(2614Kb)  |  Favorite  |  View/Download：537/136  |  Submit date：2021/11/01
Solar power tower plant system  Uncertainty propagation  Multi-objective robust optimization  Global sensitivity analysis  Levelized cost of energy  
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./通讯作者：Yan, C
Authors:  Zhang W;  Wang S;  Wang Q;  Ju SJ(鞠胜军);  Yan C
Adobe PDF(2859Kb)  |  Favorite  |  View/Download：395/161  |  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./通讯作者：Wang, Xiaojun, Wang, Ruixing
Authors:  Jiang WT;  Wang XJ;  Wang RX(王睿星);  Shi QH;  Zhu JJ
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Thermal protection system  Nonprobabilistic optimization  Sensitivity analysis  Uncertainty analysis  Model updating  
Efficient strategy for reliability-based optimization design of multidisciplinary coupled system with interval parameters 期刊论文
APPLIED MATHEMATICAL MODELLING, 2019, 卷号: 75, 页码: 349-370./通讯作者：Luo, Yan
Authors:  Wang RX(王睿星);  Luo Y
View  |  Adobe PDF(4483Kb)  |  Favorite  |  View/Download：340/119  |  Submit date：2019/11/25
Multidisciplinary design optimization  Non-probabilistic reliability  Uncertainty propagation analysis  Gradient information  Interval reliability displacement  
An interval updating model for composite structures optimization 期刊论文
COMPOSITE STRUCTURES, 2019, 卷号: 209, 页码: 177-191./通讯作者：Wang, XJ, Wang, RX
Authors:  Shi QH;  Wang XJ;  Wang RX(王睿星);  Chen X;  Ma YJ
View  |  Adobe PDF(1806Kb)  |  Favorite  |  View/Download：322/95  |  Submit date：2019/04/11
Composite structural design  Model updating  Uncertainty  Progressive failure analysis  
A robust aerodynamic optimization design for airfoil based on interval uncertainty analysis method 会议论文
ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019, San Francisco, CA, United states, July 28, 2019 - August 1, 2019
Authors:  Song X(宋鑫);  Zheng GN(郑冠男);  Yang GW(杨国伟)
Favorite  |  View/Download：174/0  |  Submit date：2020/11/20
Adaptive MOPSO  DFFD  Geometric uncertainty  Interval analysis  Kriging model  Robust design optimization  
An efficient single-loop strategy for reliability-based multidisciplinary design optimization under non-probabilistic set theory 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 73, 页码: 148-163
Authors:  Wang XJ;  Wang RX(王睿星);  Wang L;  Chen XJ;  Geng XY
View  |  Adobe PDF(3200Kb)  |  Favorite  |  View/Download：565/139  |  Submit date：2018/10/30
Non-probabilistic reliability based  multidisciplinary design optimization  Single loop strategy  Uncertainty multidisciplinary analysis  Non-probabilistic reliability analysis  Translating distance calculation  
Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Li WH(李文皓);  Xiao XX(肖歆昕);  Zhang H(张珩);  Xiao XX(肖歆昕)
View  |  Adobe PDF(1066Kb)  |  Favorite  |  View/Download：519/132  |  Submit date：2018/01/16
Aerodynamics  Air Navigation  Angle Of Attack  Control Surfaces  Control Theory  Degrees Of Freedom (Mechanics)  Dynamic Models  Flight Control Systems  Flight Simulators  Monte Carlo Methods  Reentry  Spacecraft  Surface Reactions  Uncertainty Analysis  Vehicles  
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Wang Q(汪球);  Li JW;  Lu P;  Li JP(李进平);  Zhao W(赵伟);  Jiang ZL(姜宗林)
View  |  Adobe PDF(679Kb)  |  Favorite  |  View/Download：486/97  |  Submit date：2018/01/16
Calibration  Detonation  Heat Transfer  Nozzles  Spacecraft  Supersonic Aerodynamics  Thermodynamics  Uncertainty Analysis