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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
作者:
Wang RX(王睿星)
;
Luo, Yan
Adobe PDF(6087Kb)
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浏览/下载:277/90
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提交时间: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
作者:
Luo, Yan
;
Wang, Zhiyuan
;
Zhu, Jiamin
;
Lu, Tao
;
Xiao, Gang
;
Chu, Fengming
;
Wang RX(王睿星)
Adobe PDF(2614Kb)
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浏览/下载:515/133
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提交时间: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
作者:
Zhang W
;
Wang S
;
Wang Q
;
Ju SJ(鞠胜军)
;
Yan C
Adobe PDF(2859Kb)
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浏览/下载:366/133
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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./通讯作者:Wang, Xiaojun, Wang, Ruixing
作者:
Jiang WT
;
Wang XJ
;
Wang RX(王睿星)
;
Shi QH
;
Zhu JJ
Adobe PDF(6028Kb)
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浏览/下载:364/97
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提交时间:2020/11/30
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
作者:
Wang RX(王睿星)
;
Luo Y
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Adobe PDF(4483Kb)
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浏览/下载:316/102
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提交时间: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
作者:
Shi QH
;
Wang XJ
;
Wang RX(王睿星)
;
Chen X
;
Ma YJ
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Adobe PDF(1806Kb)
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浏览/下载:319/92
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提交时间: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
作者:
Song X(宋鑫)
;
Zheng GN(郑冠男)
;
Yang GW(杨国伟)
收藏
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浏览/下载:172/0
  |  
提交时间: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
作者:
Wang XJ
;
Wang RX(王睿星)
;
Wang L
;
Chen XJ
;
Geng XY
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Adobe PDF(3200Kb)
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浏览/下载:544/120
  |  
提交时间: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
作者:
Li WH(李文皓)
;
Xiao XX(肖歆昕)
;
Zhang H(张珩)
;
Xiao XX(肖歆昕)
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Adobe PDF(1066Kb)
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浏览/下载:498/114
  |  
提交时间: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
作者:
Wang Q(汪球)
;
Li JW
;
Lu P
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
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Adobe PDF(679Kb)
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浏览/下载:477/91
  |  
提交时间:2018/01/16
Calibration
Detonation
Heat Transfer
Nozzles
Spacecraft
Supersonic Aerodynamics
Thermodynamics
Uncertainty Analysis