Experimental and finite element studies of bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy panels used in aircraft structures

Published 2016 View Full Article

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Title
Experimental and finite element studies of bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy panels used in aircraft structures
Authors
Keywords
Carbon fibre, Damage tolerance, Finite element analysis (FEA), Joints/joining
Journal
COMPOSITES PART B-ENGINEERING
Volume 100, Issue -, Pages 68-77
Publisher
Elsevier BV
Online
2016-06-22
DOI
10.1016/j.compositesb.2016.06.061

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