Finite element analysis of cohesive element for glass epoxy composite fuselage model

In this research, a numerical simulation on a newly introduced fabrication miniature composite fuselage structure - a glass epoxy composite laminated with adhesively bonded butt joint under axial compression loading is presented. A FEA via ABAQUS/Explicit is utilized to capture the complete compress...

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Détails bibliographiques

Auteur principal:	Ng, Wei Sim
Format:	Thèse
Langue:	anglais
Publié:	2011
Sujets:	Finite element method (Engineering analysis) Laminated materials
Accès en ligne:	http://psasir.upm.edu.my/id/eprint/41770/1/FK%202011%202R.pdf