Title of article :
Statistical model of the transverse ply cracking in cross-ply laminates by strength and fracture toughness based failure criteria
Author/Authors :
Andersons، نويسنده , , J. and Joffe، نويسنده , , R. and Sp?rni??، نويسنده , , E.، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2008
Pages :
15
From page :
2651
To page :
2665
Abstract :
Cross-ply laminate subjected to tensile loading provides a relatively well understood and widely used model system for studying progressive cracking of the transverse ply. This test allows to identify material strength and/or toughness characteristics as well as to establish relation between damage level and the composite stiffness reduction. The transverse ply cracking is an inherently stochastic process due to the random variability of local material properties of the plies. The variability affects both crack initiation (governed by the local strength) and propagation (governed by the local fracture toughness). The primary aim of the present study is elucidation of the relative importance of these phenomena in the fragmentation process at different transverse and longitudinal ply thickness ratios. The effect of the random crack distribution on the mechanical properties reduction of the laminate is also considered. Transverse ply cracking in glass fiber/epoxy cross-ply laminates of the lay-ups [02/902]s, [0/902]s, and [0/904]s is studied. Several specimens of each lay-up were subjected to uniaxial quasistatic tension to obtain crack density as a function of applied strain. Crack spacing distributions at the edge of the specimen also were determined at a predefined applied strain. Statistical model of the cracking process is derived, calibrated using crack density vs. strain data, and verified against the measured crack spacing distributions.
Keywords :
Polymer–matrix composites , Cross-ply laminate , cracking , Stiffness reduction
Journal title :
ENGINEERING FRACTURE MECHANICS
Serial Year :
2008
Journal title :
ENGINEERING FRACTURE MECHANICS
Record number :
2342317
Link To Document :
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