Data-driven approach for uncertainty quantification and risk analysis of composite cylindrical shells for underwater vehicles

被引:6
作者
Chen, Ming [1 ,2 ]
Zhang, Xinhu [1 ,2 ]
Pan, Guang [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Sch Marine Sci & Technol, Xian, Peoples R China
[2] Key Lab Unmanned Underwater Vehicle, Xian, Peoples R China
基金
中国国家自然科学基金; 中国博士后科学基金;
关键词
data-driven; sparse polynomial chaos expansion; uncertainty quantification; global sensitivity analysis; risk analysis; composite material; POLYNOMIAL CHAOS; PRESSURE-VESSEL; BURST PRESSURE; RELIABILITY; OPTIMIZATION; PREDICTION; CYLINDERS; DESIGN; MODEL; LOAD;
D O I
10.1080/15376494.2023.2190762
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Designing underwater vehicles considering uncertainties in mechanical properties of composites is computationally expensive. In this paper, inexpensive-to-evaluate sparse polynomial chaos expansion (PCE) based on small data is employed to alleviate computational burden arising in uncertainty analysis. Experiments and finite element analysis for buckling are performed. Relative contribution of mechanical properties to critical buckling pressure is quantified. Distribution function histogram and risk of structral failure are obtained by performing Monte Carlo simulation (MCS) on inexpensive-to-evaluate sparse PCE. Mean of critical buckling pressure is 8.27 MPa, with coefficient of variation 8.59%. 95% confidence interval is 6.86 MPa-9.65 MPa.
引用
收藏
页码:4116 / 4130
页数:15
相关论文
共 51 条
  • [1] Modeling and analysis of composite laminates in the presence of uncertainties
    Alazwari, Mashhour A.
    Rao, Singiresu S.
    [J]. COMPOSITES PART B-ENGINEERING, 2019, 161 : 107 - 120
  • [2] Data-driven inverse uncertainty quantification in the transverse tensile response of carbon fiber reinforced composites
    Balokas, Georgios
    Kriegesmann, Benedikt
    Rolfes, Raimund
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2021, 211 (211)
  • [3] Buckling Analysis of Ring-Stiffened Laminated Composite Cylindrical Shells by Fourier-Expansion Based Differential Quadrature Method
    Barani, Saeed
    Poorveis, Davood
    Moradi, Shapoor
    [J]. AEROTECH IV: RECENT ADVANCES IN AEROSPACE TECHNOLOGIES, 2012, 225 : 207 - +
  • [4] Efficient computation of global sensitivity indices using sparse polynomial chaos expansions
    Blatman, Geraud
    Sudret, Bruno
    [J]. RELIABILITY ENGINEERING & SYSTEM SAFETY, 2010, 95 (11) : 1216 - 1229
  • [5] Load sharing in single-lap bonded/bolted composite joints. Part II: Global sensitivity analysis
    Bodjona, Kobye
    Lessard, Larry
    [J]. COMPOSITE STRUCTURES, 2015, 129 : 276 - 283
  • [6] Safety factors in civil aircraft design requirements
    Bristow, John W.
    Irving, P. E.
    [J]. ENGINEERING FAILURE ANALYSIS, 2007, 14 (03) : 459 - 470
  • [7] Probabilistic analysis of composite pressure vessel for subsea blowout preventers
    Cai, Baoping
    Liu, Yonghong
    Liu, Zengkai
    Tian, Xiaojie
    Ji, Renjie
    Zhang, Yanzhen
    [J]. ENGINEERING FAILURE ANALYSIS, 2012, 19 : 97 - 108
  • [8] Reliability-based load and resistance factor design of composite pressure vessel under external hydrostatic pressure
    Cai, Baoping
    Liu, Yonghong
    Liu, Zengkai
    Tian, Xiaojie
    Ji, Renjie
    Li, Hang
    [J]. COMPOSITE STRUCTURES, 2011, 93 (11) : 2844 - 2852
  • [9] Calvário M, 2018, PROGRESS IN MARITIME TECHNOLOGY AND ENGINEERING, P395
  • [10] Spectral stochastic finite element analysis for laminated composite plates
    Chen, Nian-Zhong
    Soares, C. Guedes
    [J]. COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 2008, 197 (51-52) : 4830 - 4839