Mixed mode cohesive zone modelling and analysis of adhesively bonded composite T-joint under pull-out load
- 81 Downloads
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.
KeywordsCarbon fibre composite T-joint FE analysis Cohesive zone modelling Adhesive bonding
Authors wish to thank the support and encouragement provided by the Director, VNIT, The Head, Dept. of Mech. Engineering, VNIT, The Director, CSIR-NAL and The Head, STTD, CSIR-NAL.
- 10.ANSYS R (2013) 14.5. Academic, structural analysis guideGoogle Scholar
- 11.Sahoo P, Manjunatha C, Dattaguru B (2008) Failure prediction of adhesively bonded lap joints between metal and composite adherends, International Conference on Aerospace Science and Technology (INCAST-2008), IISc Bangalore, IndiaGoogle Scholar
- 13.Hexcel 319 adhesive data sheetGoogle Scholar