Modelling low velocity impact behaviour of composite laminates used in aerospace

Shi, Yu (2014) Modelling low velocity impact behaviour of composite laminates used in aerospace. PhD thesis, University of Sheffield.

Metadata

Supervisors: Soutis, Constantinos and Pinna, Christophe
Keywords: Composite materials, aerospace, finite element analysis, damage assessment, Non-destructive technique, Fibre metal laminates, Low velocity impact, Cohesive zone elements, matrix cracking, splitting, delamination
Awarding institution: University of Sheffield
Academic Units: The University of Sheffield > Faculty of Engineering (Sheffield) > Mechanical Engineering (Sheffield)
Depositing User: Dr Yu Shi
Date Deposited: 26 Sep 2014 15:09
Last Modified: 07 Jan 2015 09:13

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