Part I of this SpringerBrief presents the problem of a crack between two
dissimilar isotropic materials and describes the mathematical
background. A fracture criterion is discussed and Methods for
calculating fracture parameters such as stress intensity factors using
the finite element method and three post-processors are considered.
Actual test data and both deterministic and statistical failure curves
are presented.In Part II of the book, similar descriptions are given for
delaminations in composite laminates. The mathematical treatment of this
type of damage including the first term of the asymptotic expansion of
the stress and displacement fields is considered. Numerical
post-processors for determining stress intensity factors for these cases
are reviewed. Two examples of specific laminates are presented: one with
a failure curve and the other with a failure surface. Finally, beam
specimens used for testing such failures are discussed.