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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.

The full text of this thesis is not available.
Item Type: Thesis (PhD)
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
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
URI: http://etheses.whiterose.ac.uk/id/eprint/6978

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