COMPOSITES SCIENCE AND ENGINEERING ›› 2026, Vol. 0 ›› Issue (8): 109-114.DOI: 10.19936/j.cnki.2096-8000.20260828.014

• DESIGN AND TECHNIQUE • Previous Articles     Next Articles

Ply angle optimization of composite shell structure based on lamination parameters

LIU Xingwei1, SUN Wenbo2, HOU Jiaqi3, ZHANG Lanting1, JIA Chunxiao4, SUN Pengwen1*   

  1. 1. School of Mechanical Engineering, Inner Mongolia University of Technology, Hohhot 010051, China;
    2. Department of Science and Technology Innovation, Inner Mongolia Power (Group) Co., Ltd.,Hohhot 010020, China;
    3. The Xilingol Branch of Inner Mongolia Autonomous Region Special Equipment Inspection and Research Institute, Xilinhot 026000, China;
    4. Hohhot Shijie Gas Co., Ltd., Hohhot 010080, China
  • Received:2025-08-20 Online:2026-08-28 Published:2026-09-24

Abstract: Optimizing composite laminates with ply angle as a design variable poses challenges such as multiple design variables, susceptibility to local optima, and multiple solutions. To address the problems, a fiber ply angle optimization method based on lamination parameters is proposed in this paper. The method consists of two stages: optimizing of lamination parameters and converting the optimized lamination parameters into the corresponding fiber angle distribution. The relationship between lamination parameters and fiber ply angle and feasible region of lamination parameters are given, and the optimization mathematical models are established respectively. Numerical examples show that the fiber ply angle is improved, the stiffness and strength of the shell structure are enhanced. The feasibility and effectiveness of the method have been verified.

Key words: composite shell structure, lamination parameters, ply angle optimization, Lobatto polynomial

CLC Number: