COMPOSITES SCIENCE AND ENGINEERING ›› 2022, Vol. 0 ›› Issue (1): 5-12.DOI: 10.19936/j.cnki.2096-8000.20220128.001

• BASIC STUDY •     Next Articles

Research on crack propagation of composite materials based on cohesive zone model

HE Zhen-peng1, DENG Dian-kai1, LIU Guo-feng1, SUN Ai-jun1, QIAN Jun-ze1, LI Bai-chun1, HU Yi-xin2, YANG Fan3   

  1. 1. Aeronautical Engineering Institute, Civil Aviation University of China, Tianjin 300300, China;
    2. Engineering Training Centre, Civil Aviation University of China, Tianjin 300300, China;
    3. Shenyang Maintenance Base China Southern Airlines Co., Ltd., Shenyang 110000, China
  • Received:2021-04-12 Online:2022-01-28 Published:2022-02-10

Abstract: Based on the cohesive zone model, this paper develops the numerical calculation method of the three-dimensional zero-thickness cohesive element, and combines the finite element theory to derive the finite element format of the bilinear cohesive zone model and the PPR cohesive zone model. By using the ABAQUS-UEL subroutine module, a three-dimensional eight-node cohesive zone element was developed. Compared with the actual composite material layering test results and the simulation results in ABAQUS, it is proved that it can simulate the problem of composite material delamination damage accurately. The numerical program is applied to the study of the delamination damage mechanism of composite materials. The results show that the PPR cohesive zone model based on potential energy has lower computational cost, higher convergence for calculating delamination damage, higher accuracy. What's more, it further clarifies the influence of peak strength, cohesion zone length, and composite layering angle on the numerical convergence and calculation accuracy of the cohesion model.

Key words: composite laminate, ABAQUS-UEL subroutine, Fortran language, cohesive zone model, delamination damage

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