Issue 47

S. Bressan et alii, Frattura ed Integrità Strutturale, 47 (2019) 126-140; DOI: 10.3221/IGF-ESIS.47.10 128 The aim of this study is to verify the influence of notch sensitivity and crack initiation site on non-proportional low cycle fatigue life. To achieve this purpose, strain controlled multiaxial low cycle fatigue tests under proportional and non- proportional conditions on materials with different notch sensitivity and additional hardening have been conducted. Circumferentially notched bars made by Al 6061 aluminum alloy and AISI 316L stainless steel has been employed. Experimental tests have been performed to quantify the reduction of fatigue life induced by the non-proportionality of the loading path. The crack initiation site has been observed on the notch surface both on steel and aluminum. Fatigue data have been firstly synthesized with the Itoh-Sakane parameter modified with K t,n . The static stress concentration factor evaluated in the elastic field have been replaced successively with K f . Finally, the effect of the crack initiation site has been taken into account through a parameter called K’ t . Evaluation of fatigue life employing the Itoh-Sakane parameter and crack initiation site are discussed throughout this study. M ATERIALS AND TEST PROCEDURE Material properties l uminum alloy Al 6061 (6061Al) and austenitic stainless steel AISI 316L (316LSS) are the materials used in this study. Static mechanical properties are listed in Tab. 1. Material σ Y0.2 E ε U σ U MPa GPa % MPa 6061Al 143 72.2 23 311 316LSS 356 178 55 518 Table 1 : Material mechanical properties. The results of a standard tensile test evidenced the superior mechanical properties of the steel compared to aluminum. However, the material cyclic curves obtained through a cyclic plastic deformation under proportional and non-proportional loading have been indispensable to describe the material behavior in the field of low cycle fatigue. Proportional loading is represented by a push-pull (PP) loading path while non-proportional loading is represented by a circle loading path (CI). The loading paths are shown in Fig. 1. Figure 1 : Applied strain paths. Cyclic stress-strain curves associated with proportional and non-proportional loading have been obtained by a step-up test [48]. Strain increment at each step was set at Δε eq /2=0.05% every 10 cycles from Δε eq /2=0% to Δε eq /2=1.0%. The dots constituting the curves shown in Fig. 2 represent the stress and strain amplitude values at the 10 th cycle of each step, assuming that the cyclic behavior of both steel and aluminum is stabilized. The cyclic curves of 6061Al and 316LSS in CI A