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Effect of stacking sequence of the bonded composite patch on repair performance
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 Title & Authors
Effect of stacking sequence of the bonded composite patch on repair performance
Beloufa, Hadja Imane; Ouinas, Djamel; Tarfaoui, Mostapha; Benderdouche, Noureddine;
 Abstract
In this study, the three-dimensional finite element method is used to determine the stress intensity factor in Mode I and Mixed mode of a centered crack in an aluminum specimen repaired by a composite patch using contour integral. Various mesh densities were used to achieve convergence of the results. The effect of adhesive joint thickness, patch thickness, patch-specimen interface and layer sequence on the SIF was highlighted. The results obtained show that the patch-specimen contact surface is the best indicator of the deceleration of crack propagation, and hence of SIF reduction. Thus, the reduction in rigidity of the patch especially at adhesive layer-patch interface, allows the lowering of shear and normal stresses in the adhesive joint. The choice of the orientation of the adhesive layer-patch contact is important in the evolution of the shear and peel stresses. The patch will be more beneficial and effective while using the cross-layer on the contact surface.
 Keywords
composite bonded patch;sequence of ply;adjacent cross-layer;contact surface of repair;stress intensity factor (SIF);finite element analysis;
 Language
English
 Cited by
1.
Analysis of the adhesive damage between composite and metallic adherends: Application to the repair of aircraft structures,;;;;

Advances in materials Research, 2016. vol.5. 1, pp.11-20 crossref(new window)
1.
Analysis of the adhesive damage between composite and metallic adherends: Application to the repair of aircraft structures, Advances in materials Research, 2016, 5, 1, 11  crossref(new windwow)
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