Ply cracking and property degradations of symmetric balanced laminates under general in-plane loading

Abstract The authors have previously proposed a method of using a resistance curve to characterize transverse crack multiplication in balanced symmetric laminates. The method was based on the concept of a through-the-thickness inherent flaw and energy balance principle. In the present paper, this model is further extended to shear and general in-plane loading conditions. The corresponding mechanical property degradations due to transverse ply cracking are also investigated. The effective longitudinal modulus and Poisson's ratio depend not only on the crack density but also on the thermal residual and applied stresses. The reason is that the cracks do not close tightly even upon unloading due to the residual stress. Experimental results for the mechanical property degradations correlate well with the analysis except for the shear modulus. The nonlinear behavior of the shear modulus should be considered for better correlation.

[1]  M. Kural,et al.  Experimental Determination of the In Situ Transverse Lamina Strength in Graphite/Epoxy Laminates , 1982 .

[2]  J. E. Bailey,et al.  Multiple transverse fracture in 90° cross-ply laminates of a glass fibre-reinforced polyester , 1977 .

[3]  Jacob Aboudi,et al.  Stiffness reduction of cracked solids , 1987 .

[4]  H. T. Hahn,et al.  A simplified analysis of transverse ply cracking in cross-ply laminates , 1988 .

[5]  A. S. Wang Fracture Analysis of Matrix Cracking in Laminated Composites. , 1985 .

[6]  Ramesh Talreja,et al.  Transverse Cracking and Stiffness Reduction in Composite Laminates , 1985 .

[7]  David H. Allen,et al.  A thermomechanical constitutive theory for elastic composites with distributed damage. II: Application to matrix cracking in laminated composites , 1987 .

[8]  Isaac M Daniel,et al.  Damage Mechanisms and Accumulation in Graphite/Epoxy Laminates, , 1986 .

[9]  Kenneth Reifsnider,et al.  Stiffness-reduction mechanisms in composite laminates , 1982 .

[10]  Hisao Fukunaga,et al.  Probabilistic Failure Strength Analyses of Graphite/Epoxy Cross-Ply Laminates , 1984 .

[11]  D.L. Flaggs,et al.  Prediction of Tensile Matrix Failure in Composite Laminates , 1985 .

[12]  V. Vasil’ev,et al.  Analysis of the tensile deformation of glass-reinforced plastics , 1970 .

[13]  H. T. Hahn,et al.  A Mixed-Mode Fracture Criterion for Composite Materials , 1983 .

[14]  Norman Laws,et al.  Analysis of Progressive Matrix Cracking In Composite Laminates II. First Ply Failure , 1987 .

[15]  Z. Hashin Analysis of stiffness reduction of cracked cross-ply laminates , 1986 .

[16]  R. Nuismer,et al.  THE ROLE OF MATRIX CRACKING IN THE CONTINUUM CONSTITUTIVE BEHAVIOR OF A DAMAGED COMPOSITE PLY , 1983 .

[17]  Charles E. Harris,et al.  An experimental and analytical treatment of matrix cracking in cross-ply laminates , 1987 .

[18]  R. Nuismer,et al.  Constitutive Relations of a Cracked Composite Lamina , 1988 .