A thermo-viscoelastic analysis of process-induced residual stress in fibre-reinforced polymer–matrix composites

• Published in: Materials science & engineering. A, Structural materials : properties, microstructure and processing Vol. 452; pp. 483 - 498
• Main Authors: Zhao, L.G., Warrior, N.A., Long, A.C.
• Format: Journal Article
• Language: English
• Published: Amsterdam Elsevier B.V 15.04.2007; Elsevier
• Subjects: Applied sciences; Composites; Cure; Damage and failure; Exact sciences and technology; Finite element analysis; Forms of application and semi-finished materials; Mechanical properties; Physical properties; Polymer industry, paints, wood; Properties and testing; Relaxation; Residual stress; Technology of polymers; Thermo-viscoelastic; Relaxation; Damage and failure; Thermo-viscoelastic; Finite element analysis; Cure; Residual stress; Viscoelasticity; Unidirectional fiber material; Thermoviscoelasticity; Fiber reinforced material; Elasticity; Epoxy resin; Thermosetting plastics; Composite material; Micromechanics; Finite element method; Thermal expansion; Stress relaxation; Stiffness; Glass fiber; Microstructure
• ISSN: 0921-5093; 1873-4936
• DOI: 10.1016/j.msea.2006.10.060

Process-induced residual stress in fibre-reinforced thermoset polymer–matrix composites was analysed using a thermo-viscoelastic micromechanical model and the finite element method. A three-dimensional unit cell with glass fibre and epoxy polymer–matrix, representing the periodic microstructure of unidirectional fibre-reinforced composites, was considered to compute cure residual stress of fibre composites induced by chemical shrinkage of the epoxy resin and thermal cooling contraction of the whole fibre and resin system. The constitutive behaviour of the epoxy matrix was described by a cure and temperature-dependent viscoelastic material model. Compared to an elasticity solution, a reduction in residual stress was predicted due to the stress-relaxation caused by the viscoelastic behaviour of the epoxy matrix. Calculated residual stress shows strong dependency on the fibre volume fraction and fibre packing. After the cure process is complete, residual stress tends to relax to a constant value. The effect of residual stress on damage and failure of the model was also studied using the maximum stress failure criterion combined with a post-failure stiffness reduction technique. Damage onset, in terms of the location and the load level, was shown to be clearly influenced by the residual stress for both normal and shear loading. Initial and final failure envelopes, predicted for biaxial normal (longitudinal and transverse) loading and combined shear (longitudinal) and normal (transverse) loading, were shown to be shifted and contracted by the inclusion of residual stress. For final failure, residual stress was seen to have little effect on the load levels for longitudinal failure but greatly affected the load levels for transverse and shear failure. Residual stress could be detrimental or beneficial depending on the state of existing residual stress and the loading conditions.