Abstract
For structures that require high performance, dissimilar materials can be joined to achieve desirable strength-to-weight ratios. Unlike traditional mechanical joints, adhesive joints allow dissimilar materials to be joined by means of an adhesive. This method creates more uniform stress distribution while maintaining desired strength-toweight ratios. This work numerically studies adhesive joints between Titanium and Carbon Fiber Reinforced Plastic (CFRP). Finite Element Analysis is performed utilizing Abaqus® paired with Cohesive Zone Modeling to observe a comprehensive stress analysis and damage evolution of a Titanium and CFRP Tubular-Lap Joint (TLJ). By understanding the damage criteria, the properties of the TLJ can be altered to increase the strength of the joint. The failure mode of the TLJ is directly related to the mechanical properties and geometry of the adhesive which is validated numerically. This study verifies the importance of geometry considerations for adhesive joints and provides solutions to increase joint strength by utilizing a hybrid adhesive approach.
Sign-in/Register to access full text options 
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.
