Cyclic plasticity of aerospace metals: I. Modelling of aluminium 7075-T6 for structural fatigue analysis, II. Experimental characterisation and modelling of additively manufactured Ti-6Al-4V

Aircraft structures, as is the case for many engineering structures, contain discontinuities such as holes and notches, which harbour the potential for fatigue crack initiation. At the root of such discontinuities, localised plasticity can occur even thou