The structure of micromechanically based constitutive models for composite
laminates developing transverse matrix cracks, local delaminations, fibre/m
atrix debonding and fibre fractures is discussed. Nondimensional damage var
iables describing these four damage modes are introduced and the principal
form of a damage dependent constitutive law is formulated. As a special cas
e transverse matrix cracking is investigated in further detail. A previousl
y developed model for stiffness changes resulting from transverse matrix cr
acking is presented, and criteria for initiation and growth of transverse c
racks are discussed. In particular, limitations of the linear elastic fract
ure mechanics approach are investigated and a cohesive zone model capturing
crack bridging effects is suggested.