Orthotropic material orientation optimization method in composite laminates

被引:0
|
作者
Mario Petrovic
Tsuyoshi Nomura
Takayuki Yamada
Kazuhiro Izui
Shinji Nishiwaki
机构
[1] Kyoto University,
[2] Toyota Central R & D Labs.,undefined
[3] Inc.,undefined
关键词
Computational methods; Optimization; Orthotropic material; Composite;
D O I
暂无
中图分类号
学科分类号
摘要
This paper proposes a optimization method that is capable of simultaneous design of multiple layers in a composite laminate with respect to multiple objective functions. The optimization process obtains a continuous orientation of an orthotropic material for each layer of the laminate. Each layer by itself is a single design domain, which allows multiple domains to be stacked in various orientations. Multiple optimization objectives are considered resulting in layers that perform different functions. The layers are modeled within a three-dimensional structure and by discretizing the structure using three-dimensional elements, the interaction between individual layers can be modeled. This also allows the optimization method to obtain a three-dimensional orientation vector. In this study, the individual layers are assumed to be thin, limiting the orientation vector to the mid-plane of the layer. The optimization model is tested on a two-layer laminate in which one layer is optimized for thermal control by directing heat toward specified sections while shielding other sections and the second layer is optimized to reduce the total deformation of the laminate structure that results from the thermal load. The results of simultaneous optimization for both layers are shown for several different configurations of boundary conditions.
引用
收藏
页码:815 / 828
页数:13
相关论文
共 50 条
  • [41] A Multi-Level Optimization Method for Elastic Constants Identification of Composite Laminates
    Huang, Chien Yang
    Kam, Tai Yan
    APPLIED SCIENCES-BASEL, 2019, 9 (20):
  • [42] Inverse design of bistable composite laminates with switching tunneling method for global optimization
    Katherine S. Riley
    Mark H. Jhon
    Hortense Le Ferrand
    Dan Wang
    Andres F. Arrieta
    Communications Engineering, 3 (1):
  • [43] Effects of orientation errors on stiffness properties of composite laminates
    Vincenti, A
    Vannucci, P
    Verchery, G
    Belaïd, F
    REPAIRING STRUCTURES USING COMPOSITE WRAPS, 2003, : 333 - 341
  • [44] A method of layout optimization for MFC actuators in active vibration control of composite laminates
    Zhang, Hui
    Sun, Wei
    Luo, Haitao
    Shen, Jia
    Zhang, Rongfei
    APPLIED ACOUSTICS, 2024, 220
  • [45] MATERIAL CONSTANTS OF FILAMENTARY-COMPOSITE LAMINATES
    ZAGHLOUL, SA
    KENNEDY, JB
    AERONAUTICAL JOURNAL, 1974, 78 (766): : 464 - 467
  • [46] Shear Buckling Analysis and Optimization of Composite Laminates Using Perturbation GDQ Method
    Sun S.
    Zhang B.
    Hu Z.
    Zhongguo Jixie Gongcheng/China Mechanical Engineering, 2019, 30 (16): : 1931 - 1939and1949
  • [47] Effect of fibre orientation on damage resistance of composite laminates
    Khan, Sanan H.
    Khan, Ateeb Ahmad
    Husain, Afsar
    INTERNATIONAL JOURNAL OF CRASHWORTHINESS, 2021, 26 (03) : 270 - 282
  • [48] Material parameter optimization of flax/epoxy composite laminates under low-velocity impact
    Giammaria, Valentina
    Del Bianco, Giulia
    Raponi, Elena
    Fiumarella, Dario
    Ciardiello, Raffaele
    Boria, Simonetta
    Duddeck, Fabian
    Belingardi, Giovanni
    COMPOSITE STRUCTURES, 2023, 321
  • [49] A bimodular material model for orthotropic composite thin plates
    Abu-Farsakh, Ghazi
    Journal of Composites Technology and Research, 1992, 14 (04): : 31 - 36
  • [50] A BIMODULAR MATERIAL MODEL FOR ORTHOTROPIC COMPOSITE THIN PLATES
    ABUFARSAKH, G
    JOURNAL OF COMPOSITES TECHNOLOGY & RESEARCH, 1992, 14 (01): : 31 - 36