Optimal design of composite laminates with and without cutout undergoing free vibration

被引:0
作者
Iyengar N.G.R. [1 ]
Prasad A.B. [2 ]
机构
[1] Department of Aerospace Engineering, Jain University, Bangalore
[2] General Motors India Pvt. Ltd, Bangalore
关键词
Composite laminate; Finite element; Genetic algorithm; Optimum design; Vibration;
D O I
10.1080/19373260.2010.496147
中图分类号
学科分类号
摘要
In this article, the optimal designs of freely vibrating composite laminates with and without cutout undergoing are investigated. A simple higher order shear deformation theory (HSDT) with four unknown displacements (u0, v0, wb, ws) is employed to obtain the vibration response. A C1 continuity shear flexible element based on HSDT using the Hermite cubic polynomial is used for the rectangular element. The optimisation exercise is performed using genetic algorithms to maximise the fundamental frequency of vibration. The aspect ratio of the laminate, fibre orientation, thickness of plies, modulus are treated as design variables. On the basis of the investigation, it is observed that the non-dimensional frequency of the laminate with cutout can be higher or lower than those of the laminate without cutout depending on the size of the cutout. The presence of cutout significantly affects the frequency. © 2010 The Institution of Engineers, Singapore.
引用
收藏
页码:161 / 167
页数:6
相关论文
共 50 条
  • [21] A trace-based approach to design for manufacturing of composite laminates
    Tsai, Stephen W.
    Arteiro, Albertino
    Melo, Jose D. D.
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2016, 35 (07) : 589 - 600
  • [22] Influence of Trapezoidal Shapes and Cutout Sizes on the Buckling Behaviour of Composite Laminates Under Thermally Induced Loads
    Maharudra
    Rajanna, T.
    Arya, Bheemsha
    LATIN AMERICAN JOURNAL OF SOLIDS AND STRUCTURES, 2021, 18 (03)
  • [23] MULTI-OBJECTIVE OPTIMAL DESIGN OF SANDWICH COMPOSITE LAMINATES USING SIMULATED ANNEALING AND FEM
    Sarhadi, A.
    Tahani, M.
    Kolahan, F.
    Sarhadi, M.
    PROCEEDINGS OF THE ASME PRESSURE VESSELS AND PIPING CONFERENCE, VOL 3, 2009, : 599 - 608
  • [24] Modeling vibration behavior of delaminated composite laminates using meshfree method in Hamilton system
    Jie CHEN
    Hai WANG
    Guanghui QING
    Applied Mathematics and Mechanics(English Edition), 2015, 36 (05) : 633 - 654
  • [25] Modeling vibration behavior of delaminated composite laminates using meshfree method in Hamilton system
    Chen, Jie
    Wang, Hai
    Qing, Guanghui
    APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2015, 36 (05) : 633 - 654
  • [26] Modeling vibration behavior of delaminated composite laminates using meshfree method in Hamilton system
    Jie Chen
    Hai Wang
    Guanghui Qing
    Applied Mathematics and Mechanics, 2015, 36 : 633 - 654
  • [27] A solution for the vibration and buckling of composite laminates with elastically restrained edges
    Setoodeh, AR
    Karami, G
    COMPOSITE STRUCTURES, 2003, 60 (03) : 245 - 253
  • [28] Design of Composite Laminates Using Enumeration Method
    Joung, Chanwoo
    Bae, Il-Joon
    Park, Young-Bin
    COMPOSITES RESEARCH, 2020, 33 (05): : 288 - 295
  • [29] Design of composite laminates with low thermal expansion
    Bressan, F
    De Bona, F
    Somá, A
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART L-JOURNAL OF MATERIALS-DESIGN AND APPLICATIONS, 2004, 218 (L3) : 201 - 209
  • [30] Free vibration analysis and design of an adhesively bonded composite single lap joint
    Apalak, M. Kemal
    Ekici, Recep
    Yildirim, Mustafa
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION 2007, VOL 1: ADVANCES IN AEROSPACE TECHNOLOGY, 2008, : 211 - 220