Parametric study on cohesive element for composite fuselage model

Parametric study on cohesive element for composite fuselage model

In this paper, a numerical simulation on a new fabrication miniature composite fuselage structure- a woven composite laminated with an adhesively bonded butt joint under the axial compression loading is presented. A FEA via Abaqus/Explicit was utilized to capture the complete compressive responses t...

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Bibliographic Details
Main Authors: Ng, Wei Sim, Mustapha, Faizal, Varatharajoo, Renuganth, Zahari, Rizal, Abang Abdul Majid, Dayang Laila
Format: Article
Language:English
Published: Trans Tech Publications 2011
Online Access:http://psasir.upm.edu.my/id/eprint/23081/
http://psasir.upm.edu.my/id/eprint/23081/1/Parametric%20study%20on%20cohesive%20element%20for%20composite%20fuselage%20model.pdf

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