Bonded joints used in wing sections and frames of aircraft structures are mostly exposed to cyclic loadings instead static ones during their services. Bending types dynamic encountered. In this study, the fatigue response a single lap joint (SLJ) bending loading was studied with developed advanced finite-element (FE) model. The cohesive zone model describing behaviour adhesive layer damage mech...

Modelling of the deformation process Al85Y8Ni5Co2 amorphous alloys was carried out under simultaneous application cyclic mechanical load (at 0.3 or 3 Hz frequencies) and continuously increasing temperature (heating rate 5 K/min). It is shown that specimens occurs by hyperbolic temporal dependence. analytically determined experimentally proved for non-isothermal deformation, wave effects take pl...