Structural optimization design of typical adhesive bonded sandwich T-joints based on progressive damage analysis and multi-island genetic algorithm

被引:8
作者
Niu, Yiran [1 ]
Xu, Xiwu [1 ]
Guo, Shuxiang [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, State Key Lab Mech & Control Mech Struct, Nanjing 210016, Peoples R China
关键词
Optimization; progressive damage analysis; adhesive bonded sandwich T-joints; MIGA algorithm; variable-thickness composite laminates; parametric modeling; DELAMINATION; COMPOSITES; BEHAVIOR; MODEL;
D O I
10.1177/1099636220962278
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper deals with the optimization of multi-laminate structures by Multi-Island Genetic Algorithm (MIGA) coupled with CAE solver. The optimization problem is a compound problem which relates to size optimization for object structure and stacking sequence optimization for variable-thickness composite laminates. Taking a typical adhesive bonded sandwich T-joint under a reference pull-off load as an instance object and establishing strength conditions on the basis of progressive damage analysis, optimum design is carried out with the total weight of joint as the target function. Progressive damage model (PDM) methodology and cohesive zone model (CZM) methodology are employed to develop an exact finite element model of the object structure. Classified failure criteria are chosen to investigate the capability of the joint in bearing the applied load. The optimization procedure on the typical adhesive bonded sandwich T-joint showed 34.24% weight reduction compared to the initial laminated structure. On the basis of history data, the study further brings out the influence of design variables on some main constraint variables.
引用
收藏
页码:3932 / 3965
页数:34
相关论文
共 22 条
  • [1] Novel design of foam core junctions in sandwich panels
    Bozhevolnaya, E.
    Lyckegaard, A.
    Thomsen, O. T.
    [J]. COMPOSITES PART B-ENGINEERING, 2008, 39 (01) : 185 - 190
  • [2] Camanho PP, 2003, J COMPOS MATER, V37, P1415, DOI [10.1177/0021998303034505, 10.1177/002199803034505]
  • [3] A progressive damage model for mechanically fastened joints in composite laminates
    Camanho, PP
    Matthews, FL
    [J]. JOURNAL OF COMPOSITE MATERIALS, 1999, 33 (24) : 2248 - 2280
  • [4] Optimum stacking sequence design of composite materials Part II: Variable stiffness design
    Ghiasi, Hossein
    Fayazbakhsh, Kazem
    Pasini, Damiano
    Lessard, Larry
    [J]. COMPOSITE STRUCTURES, 2010, 93 (01) : 1 - 13
  • [5] Optimum stacking sequence design of composite materials Part I: Constant stiffness design
    Ghiasi, Hossein
    Pasini, Damiano
    Lessard, Larry
    [J]. COMPOSITE STRUCTURES, 2009, 90 (01) : 1 - 11
  • [6] Numerical analysis and experiment of composite sandwich T-joints subjected to pulling load
    Guo, S.
    Morishima, R.
    [J]. COMPOSITE STRUCTURES, 2011, 94 (01) : 229 - 238
  • [7] Prediction of impact damage in composite plates
    Hou, JP
    Petrinic, N
    Ruiz, C
    Hallett, SR
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2000, 60 (02) : 273 - 281
  • [8] A delamination criterions for laminated composites under low-velocity impact
    Hou, JP
    Petrinic, N
    Ruiz, C
    [J]. COMPOSITES SCIENCE AND TECHNOLOGY, 2001, 61 (14) : 2069 - 2074
  • [9] Stacking sequence optimization of composite laminates for maximum buckling load using permutation search algorithm
    Jing, Zhao
    Fan, Xueling
    Sun, Qin
    [J]. COMPOSITE STRUCTURES, 2015, 121 : 225 - 236
  • [10] Behavior and Failure Modes of Sandwich T-Joint Using Cohesive Zone Material Model and Contact Elements
    Khalili, S. M. R.
    Ghaznavi, A.
    [J]. APPLIED COMPOSITE MATERIALS, 2013, 20 (01) : 41 - 54