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The failure behaviour of three different configurations of adhesively bonded carbon fibre composite T-joints subjected to pull-out load is investigated. Finite element analysis is carried out on the carbon fibre… Click to show full abstract
The failure behaviour of three different configurations of adhesively bonded carbon fibre composite T-joints subjected to pull-out load is investigated. Finite element analysis is carried out on the carbon fibre composite T-joint models. A non-linear, contact target-based cohesive zone model with appropriate traction separation law is selected to simulate the pull-out test condition in FE package ANSYS®. The FE analysis results are in close agreement with available experimental results.
Keywords:
pull load;
composite joint;
adhesively bonded;
cohesive zone;
analysis
Journal Title: Journal of the Brazilian Society of Mechanical Sciences and Engineering
Year Published: 2018
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Journal Title: Journal of the Brazilian Society of Mechanical Sciences and Engineering
Year Published: 2018
Link to full text (if available)
Share on Social Media: Sign Up to like & get
recommendations!