Abstract
Additive manufacturing technology has gained significant attention in recent years. However, due to lack of sufficient understanding of their fatigue behavior under service loading conditions, design of critical load carrying parts using this technique is still at early stages. These conditions include multiaxial stress states, notches and stress concentrations, and variable amplitude load cycles. Some of the distinguishing features of AM metals as compared to the conventionally fabricated metals include defects, surface roughness, anisotropy and build orientation effects, and residual stresses due to the fast solidification during the fabrication process. These factors resulting from AM processes may significantly affect the fatigue performance of AM parts under multiaxial variable amplitude loading. In this work, unnotched and notched fatigue behavior of two commonly used AM metals with different surface roughness conditions were studied under variable amplitude multiaxial loads. Both crack initiation approach using critical plane-based model and fracture mechanics approach using crack growth from the rough surface or surface defects at the notch were used to estimate the fatigue lives. Fatigue estimations are then compared to the experimental results.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.