Issue 36

F.A. Stuparu et alii, Frattura ed Integrità Strutturale, 36 (2016) 69-77; DOI: 10.3221/IGF-ESIS.36.08 69 Focused on Fracture Mechanics in Central and East Europe Failure analysis of dissimilar single-lap joints F.A. Stuparu, D.A. Apostol, D.M. Constantinescu, M. Sandu, S. Sorohan University POLITEHNICA of Bucharest, Romania stuparu.florin@gmail.com, apostolda@yahoo.com, dan.constantinescu@upb.ro , marin.sandu@upb.ro, stefan.sorohan@upb.ro A BSTRACT . Single-lap joints made of aluminium and carbon fibre adherends of different thickness are tested to understand better the behaviour of such dissimilar joints. The overlap length and the thickness of the adhesive are kept constant. Local deformation fields are monitored by using the digital image correlation method. Peeling and shearing strains are investigated, emphasizing that peeling is important in the region where failure is initiated, towards an extremity of the overlap region. The use of only carbon fibre adherends is not recommended for a smaller thickness as an additional interface failure is produced and compromises the integrity of the lap joint. However, a dissimilar joint (aluminium-carbon) with smaller thickness adherends succeeds to maintain the stiffness of the assembly, but its strength is diminished. The obtained results are suggesting that a complete monitoring of the failure processes in the overlap region can be fully understood only if local deformation measurements are possible. K EYWORDS . Sigle-lap joints; Dissimilar adherends; Digital image correlation; Peeling and shearing. I NTRODUCTION eronautical, automotive or naval structural integrity is of great importance and any presence of imperfections can reduce significantly the load bearing capacity. Without a better understanding of progressive failure, the fracture criteria and predictive capabilities will be limited. In many cases adhesive joints have to be used and single-lap joints are of particular interest. Several parameters have a significant influence as: the thickness of the adherends, the overlap length, and the adhesive thickness. On the other hand, the use of dissimilar materials in such joints represent new challenges and the complete understanding of the local phenomena deserve further investigations. In many engineering applications the gluing of metallic and composite materials starts to be a necessity. It is known that the thickness of the adhesive influences the strength of the assembly but its effect is not completely understood. Experimental results have shown that the strength of the joint decreases with the increase of the adhesive thickness. Gleich et al. [1] showed that the interface stresses grow proportionally with the thickness, and Grant et al. [2] pointed out through experimental testing that the strength decreases due to the increase of the bending moment. The increase of the thickness leads to the increase of the arm of the force and therefore of the bending moment. It looks like the optimum strength of an epoxy adhesive is to be obtained when its thickness is between 0.1 and 0.5 mm. However, as pointed by Banea and da Silva [3], the results may vary due to the type of loading, the ductile or fragile behaviour of the adhesive and the rigidity of the adherends. Opposite to what was expected, they showed that for a fragile adhesive a better performance of the lap-joint was obtained for the thicker adhesive. An explanation of the peculiar behaviour relied on the different thermal inertia of the thicknesses which resulted after the thermal cycle. The contradiction between the classical A