Abstract
Adhesive bonding has a high potential for aerospace, automotive, and other structural applications. Adhesively bonded composite patches can be used to repair aerospace parts with minimum deterioration of aerodynamic contours. Although adhesive joints have been extensively studied during the past decades, the mechanisms of fatigue failure and life of joints are not yet sufficiently understood. The objective of this paper was to study mechanical behavior and mechanisms of damage and failure in single-lap composite joints under fatigue.
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.
