COMPOSITES SCIENCE AND ENGINEERING ›› 2023, Vol. 0 ›› Issue (1): 5-15.DOI: 10.19936/j.cnki.2096-8000.20230128.001

• BASIC STUDY •     Next Articles

Angle optimization analysis of variable stiffness laminates based on ant colony algorithm

ZHANG Guiming1, SHEN Zhiqiang1, ZU Lei1,2*, WANG Huabi1, ZHANG Qian1, XIA Xianzhao1, GENG Hongbo3, PAN Jie4, ZOU Liqing1   

  1. 1. School of Mechanical Engineering, Hefei University of Technology, Hefei 230009, China;
    2. Anhui Province Key Laboratory of Aerospace Structural Parts Forming Technology and Equipment, Hefei 230009, China;
    3. Inner Mongolia Aerospace Honggang Machinery Co., Hohhot 010000, China;
    4. COMAC Composites Center, Shanghai 200126, China
  • Received:2022-04-29 Online:2023-01-28 Published:2023-02-24

Abstract: In order to perform stiffness analysis of variable stiffness composite laminates, a discrete unitisation of the laminate vibration equation was carried out based on the differential quadrature method (DQM) in this study, which can facilitate frequency analysis. Meanwhile, the fundamental frequency is an essential research parameter of vibration. The ant colony algorithm (ACA) is used in conjunction with DQM to generate the initial angle randomly by the ACA to improve the frequency values calculated by DQM in the evolutionary iteration process. The results show that the evolutionary iteration process of ACA can optimize the selection of the beginning and termination angles of the pavement very well. Through updating the pheromone generation by generation and improving the ACA appropriately to achieve the final angle convergence, the optimal pavement start and end angles are found to be [<38°|62.75°>,<90°|72°>,<0°|5°>,<0°|5°>]S. Moreover, the corresponding frequency value is 11.712 57 Hz. Also, the data statistics show that the initial angles are mainly concentrated around 0°, 38°and 90°, and the termination angles are loosely distributed but mainly concentrated around 10°~90°.

Key words: ant colony algorithm, differential quadrature method, variable stiffness, frequency, angle distribution, composites

CLC Number: