The lifetimes of 316 stainless steel specimens are herein evaluated using the multiaxial critical plane-based criterion by Carpinteri et al. for high-cycle fatigue (HCF) loading with constant amplitude. In the present paper, the stress-based version of such a criterion is applied to assess the results of experimental tests under HCF triaxial loading, the hollow cylindrical dog-bone specimens being subjected to a quenching heat treatment. The analytical results of fatigue life and initial crack plane orientation are compared with the experimental data.
|Titolo:||Lifetime estimation for 316 stainless steel specimens by using a critical plane approach|
|Data di pubblicazione:||2020|
|Appare nelle tipologie:||1.1 Articolo in rivista|