Effect of fibre/matrix adhesion on residual strength of notched composite laminates

Effects of fibre/matrix adhesion and residual strength of notched polymer matrix composite laminates (PMCLs) and fibre reinforced metal laminates (FRMLs) were investigated. Two different levels of adhesion between fibre and matrix were achieved by using the same carbon fibres with or without surface treatments. After conducting short-beam shear and transverse tension tests for fibre/matrix interface characterisation, residual strength tests were performed for PMCLs and FRMLs containing a circular hole/sharp notch for the two composite systems. It was found that laminates with poor interfacial adhesion between fibre and matrix exhibit higher residual strength than those with strong fibre/matrix adhesion. Major failure mechanisms and modes in two composite systems were studied using SEM fractography. The effective crack growth model (ECGM) was also applied to simulate the residual strength and damage growth of notched composite laminates with different fibre/matrix adhesion. Predictions from the ECGM were well correlated with experimental data.

[1]  Iwona M Jasiuk,et al.  Effect of interface on the elastic stiffness of composites , 1989 .

[2]  Yiu-Wing Mai,et al.  Effects of fibre/matrix adhesion on carbon-fibre-reinforced metal laminates—I.: Residual strength , 1998 .

[3]  M. Piggott The effect of the interface/interphase on fiber composite properties , 1987 .

[4]  Lin Ye,et al.  An Effective Crack Growth Model for Residual Strength Evaluation of Composite Laminates with Circular Holes , 1996 .

[5]  K. Sahre,et al.  Parameters affecting the interface properties in carbon fibre/epoxy systems , 1995 .

[6]  Y. Mai,et al.  Effective Crack Growth and Residual Strength of Composite Laminates with a Sharp Notch , 1996 .

[7]  Y. Mai,et al.  Micromechanical characterisation of fibre/matrix interfaces , 1992 .

[8]  Lawrence T. Drzal,et al.  Fiber-Matrix Adhesion and Its Effect on Composite Mechanical Properties: II. Longitudinal (0°) and Transverse (90°) Tensile and Flexure Behavior of Graphite/Epoxy Composites , 1991 .

[9]  Yiu-Wing Mai,et al.  Effects of fibre/matrix adhesion on carbon-fibre-reinforced metal laminates—II. impact behaviour , 1998 .

[10]  Carl-Gustaf Aronsson,et al.  Strength of Tensile Loaded Graphite/Epoxy Laminates Containing Cracks, Open and Filled Holes , 1990 .

[11]  Yiu-Wing Mai,et al.  Evaluations of effective crack growth and residual strength of fibre-reinforced metal laminates with a sharp notch , 1996 .

[12]  L. J. Ebert,et al.  Theoretical Modelling of the Effect of the Interfacial Shear Strength on the Longitudinal Tensile Strength of Unidirectional Composites , 1987 .

[13]  J. Gérard,et al.  The adhesion of elastomer-coated glass fibers to an epoxy matrix. Part I: The effect of the surface treatments on the tensile strength of the glass fibers , 1995 .

[14]  J. Whitney,et al.  Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations , 1974 .