Numerical Analysis on Process-Induced Residual Stress in Thick Semi-Cylindrical Composite Shell Using a State-Dependent Viscoelastic Model

被引:0
作者
Jiangtao Zhang
Yanliang Qiao
Mei Zhang
Haixiao Hu
Pengcheng Zhai
Shuxin Li
机构
[1] Wuhan University of Technology,Hubei Key Laboratory of Theory and Application of Advanced Materials Mechanics, School of Science
[2] University of Bristol,Department of Mechanical Engineering
来源
Applied Composite Materials | 2019年 / 26卷
关键词
Polymer-matrix composites (PMCs); Finite element analysis (FEA); Viscoelastic constitutive model; Residual stress; Spring-in;
D O I
暂无
中图分类号
学科分类号
摘要
A two-step state-dependent analysis model corresponding to the flow state before gelation and the viscoelastic state after gelation was proposed for the prediction of the residual stresses developed in polymer matrix composites (PMCs) during cure. The evolution of the viscoelasticity of PMCs during cure was analyzed based on the non-dimensional viscoelasticity parameters 1/Dem, and the gelation time was determined at the condition of Min(1/Dem) = 102. The proposed model was used to predict the process-induced residual stress and distortion in a thick semi-cylindrical composite shell. By comparing the predictions with those of the original cure-dependent viscoelastic model, the proposed model was verified and the computing time and memory storage were significantly reduced. The results show that during the cure of thick semi-cylindrical composite shell, the residual stresses caused by the cure shrinkage at high cure temperature are quickly relaxed, and most of the residual stress develops during cool-down. The spring-in deformation of the semi-cylindrical shell when release from the mould is mainly caused by the significant hoop stress gradient in the thickness direction developed during cure. Obvious warpage is not present in the composite semi-cylindrical shell due to the high bending stiffness.
引用
收藏
页码:519 / 532
页数:13
相关论文
共 131 条
  • [1] Kim YK(1997)Viscoelastic analysis of processing-induced residual stresses in thick composite laminates Mech. Compos. Mater. Struct. 4 361-387
  • [2] White SR(2017)Curing of thick thermoset composite laminates: multiphysics modeling and experiments Appl. Compos. Mater. 11 1-14
  • [3] Anandan S(1999)Optimum design of thick-walled multi-layered cfrp pipes to reduce process-induced residual stresses Appl. Compos. Mater. 6 289-307
  • [4] Dhaliwal GS(2016)Effect of curing overheating on interlaminar shear strength and its modelling in thick FRP laminates Int. J. Adv. Manuf. Technol. 87 2213-2220
  • [5] Huo Z(1989)Residual stress development during processing of graphite/epoxy composites Compos. Sci. Technol. 36 121-132
  • [6] Chandrashekhara K(2017)Reduction of composite deformation based on tool-part thermal expansion matching and stress-free temperature theory Int. J. Adv. Manuf. Technol. 88 1703-1710
  • [7] Apetre N(2017)A review on the mechanical modeling of composite manufacturing processes Arch. Computat. Methods Eng. 24 365-395
  • [8] Iyyer N(1992)Process-induced stress and deformation in thick-section thermoset composite laminates J. Compos. Mater. 26 626-660
  • [9] Sekine H(2016)3D finite element model for predicting manufacturing distortions of composite parts J. Compos. Mater. 50 1-17
  • [10] Shin ES(2001)A plane strain model for process-induced deformation of laminated composite structures J. Compos. Mater. 35 1435-1469