Abstract
A new criterion is proposed for evaluating the multiaxial high-cycle fatigue limit of components with notches and superficial small holes. Two parameters are specified: (1) one governing crack initiation and (2) the other governing initial crack growth. The new criterion is based on the multiaxial fatigue criterion for smooth components previously proposed by the authors. The accuracies of the proposed and conventional criteria are evaluated using experimentally determined fatigue limit data of notches and superficial small holes under combined bending and torsion stresses and combined axial and torsion stresses. The error of the proposed criterion is approximately 10%.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: 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.
