Functional and Structural Fatigue of a Pseudoelastic NiTi Alloy within the Stress-Induced Transformation Regime
The first step was carried up to a stable mechanical response of the alloy and a variable strain ratio was adopted, in order to avoid compression stresses during unloading, due to the accumulation of residual deformations. The evolution of several functional damage parameters have been analyzed, such as the residual and recovery deformations, the dissipated and recovery energies, the direct transformation stresses and the Young’s modulus. The results revealed marked evolutions of these parameters but stabilization always occurs between 100 and 200 mechanical cycles. Subsequently, the stabilized specimens have been subjected to strain controlled fatigue tests, under a fixed strain ratio, up to complete failure.
The strain-life data have been analyzed within the framework of a recent phenomenological model, based on a modified Coffin-Manson approach [1]. Finally, the fracture surfaces have been analysed by scanning electron microscopy (SEM) in order to analyze the stable and unstable crack growth mechanisms.
[1] C. Maletta, E. Sgambitterra, F. Furgiuele, R. Casati2 and A. Tuissi, Fatigue of pseudoelastic NiTi within the stress-induced transformation regime: a modified Coffin–Manson approach, Smart Mater. Struct. 21 112001