Isogeometric Analysis for Buckling and Wrinkling of Variable-Stiffness Sandwich Plates Under Compression

被引:0
|
作者
Chen, Xiaodong [1 ]
Zhang, Fengjian [1 ]
Nie, Guojun [2 ,3 ]
机构
[1] Henan Univ Urban Construct, Sch Civil & Transportat Engn, Pingdingshan 467000, Peoples R China
[2] Tongji Univ, Sch Aerosp Engn & Appl Mech, Shanghai 200092, Peoples R China
[3] Shanghai Inst Aircraft Mech & Control, Shanghai 200092, Peoples R China
基金
中国国家自然科学基金;
关键词
Instability; sandwich plates; IGA; EHSAPT; variable angle tow; non-periodic wrinkling; COMPOSITE PANELS; FREE-VIBRATION; OPTIMIZATION; NURBS; CORE; BEHAVIOR; BEAMS;
D O I
10.1142/S1758825124500972
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In this paper, an isogeometric analysis (IGA) framework based on the high-order sandwich plate theory is developed for the first time to deal with both buckling and wrinkling problems of variable-stiffness sandwich plates under compression. The present sandwich plate model is formulated based on the extended high-order sandwich plate theory (EHSAPT). The weak-form governing equations are firstly derived from the principle of virtual work, and afterward the IGA formulations based on the Non-Uniform Rational B-Splines (NURBS) are applied to predict the instability loads and the corresponding instability modes. Both the membrane and non-membrane conditions are integrated into the linear buckling analysis. The novelty of this work lies in that the employment of high-order continuous NURBS basis functions can directly fulfill the C-1 continuity requirement inherent in the EHSAPT theory, which enables the EHSAPT-based IGA model to be formulated with fewer degrees of freedom. Besides, the developed EHSAPT-based IGA model has also the ability to capture the overall buckling or wrinkling modes of the sandwich plates. The accuracy and effectiveness of the proposed EHSAPT-based IGA model are verified by comparison with previously published results and those obtained using ABAQUS. Effects of the core thickness and fiber angle on the buckling behaviors of the sandwich plates are also studied in numerical examples. It is observed that the non-uniform in-plane pre-stress over the skin layers is the main reason for the non-periodic wrinkling of constant-stiffness sandwich constructions, whereas the non-uniformity of both the in-plane pre-stress and out-of-plane bending stiffness is responsible for the non-periodic wrinkling of variable-stiffness sandwich constructions. The results presented herein may be beneficial for the design of variable-stiffness sandwich constructions under compression.
引用
收藏
页数:37
相关论文
共 50 条
  • [1] Isogeometric buckling analysis of composite variable-stiffness panels
    Hao, Peng
    Yuan, Xiaojie
    Liu, Hongliang
    Wang, Bo
    Liu, Chen
    Yang, Dixiong
    Zhan, Shuangxi
    COMPOSITE STRUCTURES, 2017, 165 : 192 - 208
  • [2] Buckling analysis, design and optimisation of variable-stiffness sandwich panels
    Coburn, Broderick H.
    Weaver, Paul M.
    INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2016, 96 : 217 - 228
  • [3] Buckling optimization of variable-stiffness composite plates via variable stiffness optimization algorithm
    Jing, Zhao
    Duan, Lei
    Wang, Siqi
    Li, Biao
    COMPOSITE STRUCTURES, 2024, 327
  • [4] Buckling analysis of variable-stiffness composite truncated elliptical rotary shell under external hydrostatic compression
    Lu, Jiuru
    Xu, Luyao
    Xu, Haojie
    Li, Kangmei
    Hu, Jun
    COMPOSITE STRUCTURES, 2023, 307
  • [5] Isogeometric degenerated shell formulation for post-buckling analysis of composite variable-stiffness shells
    Hao, Peng
    Liao, Hewei
    Wu, Tao
    Huo, Zekai
    Wang, Bo
    COMPOSITE STRUCTURES, 2023, 321
  • [6] Buckling and wrinkling of anisotropic sandwich plates
    Vescovini, Riccardo
    D'Ottavio, Michele
    Dozio, Lorenzo
    Polit, Olivier
    INTERNATIONAL JOURNAL OF ENGINEERING SCIENCE, 2018, 130 : 136 - 156
  • [7] Manufacture and Buckling Test of a Variable-Stiffness, Variable-Thickness Composite Cylinder Under Axial Compression
    Lincoln, Reece L.
    Weaver, Paul M.
    Pirrera, Alberto
    Groh, Rainer M. J.
    Zympeloudis, Evangelos
    AIAA JOURNAL, 2023, 61 (04) : 1849 - 1862
  • [8] Efficient post-buckling analysis of variable-stiffness plates using a perturbation approach
    Vescovini, R.
    Spigarolo, E.
    Jansen, E. L.
    Dozio, L.
    THIN-WALLED STRUCTURES, 2019, 143
  • [9] Pre-buckling and Buckling Analysis of Variable-Stiffness, Curvilinearly Stiffened Panels
    R. Vescovini
    V. Oliveri
    D. Pizzi
    L. Dozio
    P. M. Weaver
    Aerotecnica Missili & Spazio, 2020, 99 (1): : 43 - 52
  • [10] Post-buckling analyses of variable-stiffness composite cylinders in axial compression
    White, Simon C.
    Weaver, Paul M.
    Wu, K. Chauncey
    COMPOSITE STRUCTURES, 2015, 123 : 190 - 203