In this study, the adhesive damage in bonded composite repair of aircraft structures is
analyzed using a three dimensional finite element method. Four different patch shapes were …

The objective of this study was to compare the performance of the repaired longitudinal
cracks in API X65 pipelines under two different conditions: with patches (ie, single and …

In this study, a new approach is applied to compare the performances of single sided and
double-sided symmetric composite patch with circular shape for repairing cracked aircraft …

In this study the three-dimensional nonlinear finite element method is used to determine the
J integral variation along the front of repaired crack with bonded composite patch in aircraft …

The aim of this study is to investigate the failure of cracked aluminum plates repaired by one-
side composite patches under fatigue loading using Acoustic Emission (AE) and …

The optimization of the patch shape of bonded composite repair in aircraft structures is a
good way to improve the repair performance. In this study, the three-dimensional finite …

In this work the finite element method was used to analyse the composite patch shape effect
of the repair performance. Unlike all the works done conducted so far in this domain, this …

The fatigue performance of rubber composite cannot be ignored in the field of engineering.
Fatigue crack growth rate (FCGR) test by using a planar tensile specimen with a crack or …

In this study, the finite element method is used to analyze the effect of the thermal residual
stresses resulting from adhesive curing on the performances of the bonded composite repair …

Material fracture by opening (mode I) is not the only failure criteria responsible for fracture
propagation. Many industrial examples show the presence of mode II and mixed mode I+ II …