Citation:
M. Boscolo, X. Zhang, A modelling technique for calculating stress intensity
factors for structures reinforced by bonded straps. Part I: Mechanisms and
formulation, Engineering Fracture Mechanics, Volume 77, Issue 6, April 2010,
Pages 883-895
Abstract:
This paper describes a 2D FE modelling technique for predicting fatigue crack
growth life of integral structures reinforced by bonded straps. This kind of
design offers a solution to the intrinsic lack of damage tolerance of integral
structures. Due to the multiple and complex failure mechanisms of bonded
structures, a comprehensive modelling technique is needed to evaluate important
design parameters. In this Part I of a two-part paper, the actions and
mechanisms involved in a bonded structure are discussed first, followed by
presenting the modelling approaches to simulate each mechanism. Delamination or
disbond of the strap from the substrate is modelled by computing the strain
energy release rate on the disbond front and applying a fracture mechanics
criterion. Thermal residual stresses arising from the adhesive curing process
and their redistribution with the substrate crack growth are calculated and
taken into account in the crack growth analysis. Secondary bending effect caused
by the un-symmetric geometry of one-sided strap is also modelled. In the classic
linear elastic fracture mechanics, a non-dimensional stress intensity factor,
i.e. the geometry factor β, depends only on the sample’s geometry. This β factor
cannot be found for this kind of bonded structures, since the magnitude of
disbond is related to the applied stress and the disbond size modifies the
geometry of the structure. Moreover, secondary bending effect is geometric
nonlinear thus the stress intensity factor cannot be normalised by the applied
stress. For these reasons an alternative technique has been developed, which
requires calculating the stress intensity factors at both the maximum and
minimum applied stresses for each crack length. This analysis technique is
implemented in a computer program that interfaces with the NASTRAN commercial
code to compute the fatigue crack growth life of strap reinforced structu