Structural integrity of shot peened Ti6Al4V specimens under fretting fatigue

Abstract

In the present paper, an experimental campaign performed on shot peened Ti6Al4V specimens under fretting fatigue, available in the literature, is simulated by using the Carpinteri et al. criterion. The experiments examined were carried out using a standard configuration, that is, a cylinder against a flat specimen. The fretting loading is a combination of low-cycle fatigue and high-cycle fatigue, and the corresponding stress field is determined by a FE analysis. A theoretical law is applied to describe the relaxed residual stress produced by shot peening treatment and fatigue loading.

Influence of normal load frequency on fretting fatigue behaviour by a critical plane-based approach

“…In the last decades, many researchers have focused on fretting fatigue behaviour of different materials, tested by considering both a constant normal load and in-phase fretting fatigue loading [35][36][37][38][39][40][41][42][43][44][45] more complex loading conditions generally affect in-service engineering components. In such a context, some papers concerning complex loading configurations have been recently proposed.…”