A generalized micromechanical approach for the analysis of transverse crack and induced delamination in composite laminates

The previously developed micromechanical approaches for the analysis of transverse cracking and induced delamination are limited for laminates with specific lay-ups such as cross-ply and specific loading conditions In this paper a new micromechanical approach is developed to overcome such shortcomings For this purpose a unit cell in the ply level of composite laminate including transverse cracking and delamination is considered Then the governing equations for the stress and displacement fields of the unit cell are derived The obtained approximate stress field is used to calculate the energy release rate for the propagation of transverse cracking and induced delamination To show the capability of the new method It is employed for the analyses of general laminates with [0/90](s) [45/-45](s) [30/-30](s) and [90/45/0/-45](s) lay-ups under combined loadings to calculate the energy release rate due to the transverse cracking and induced delamination It is shown that the obtained energy release rates for transverse cracking and delamination initiation are in good agreement with the available results in the literature and finite element method Furthermore the occurrence priority of further transverse cracks and/or delamination at each damage state of the laminates will be discussed (C) 2010 Elsevier Ltd All rights reserved