Failure analysis using X-ray computed tomography of composite sandwich panels subjected to full-scale blast loading
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Published version
Accepted version
Author(s)
Rolfe, E
Kelly, M
Arora, H
Hooper, PA
Dear, JP
Type
Journal Article
Abstract
The tailorable mechanical properties and high strength-to-weight ratios of composite sandwich panels make them of interest to the commercial marine and naval sector, however, further investigation into their blast resilience is required. The experiments performed in this study aimed to identify whether alterations to the composite skins or core of a sandwich panel can yield improved blast resilience both in air and underwater. Underwater blast loads using 1.28 kg TNT equivalent charge at a stand-off distance of 1 m were performed on four different composite sandwich panels. Results revealed that implementing a stepwise graded density foam core, with increasing density away from the blast, reduces the deflection of the panel and damage sustained. Furthermore, the skin material affects the extent of panel deflection and damage, the lower strain to failure of carbon-fibre reinforced polymer (CFRP) skins reduces deflection but increases skin debonding. A further two panels were subjected to a 100 kg TNT air blast loading at a 15 m stand-off to compare the effect of a graded density core and the results support the underwater blast results. Future modelling of these experiments will aid the design process and should aim to include material damage mechanisms to identify the most suitable skins.
Date Issued
2017-07-20
Date Acceptance
2017-07-18
Citation
Composites Part B: Engineering, 2017, 129, pp.26-40
ISSN
1359-8368
Publisher
Elsevier
Start Page
26
End Page
40
Journal / Book Title
Composites Part B: Engineering
Volume
129
Copyright Statement
© 2017 The Authors. Published by Elsevier Ltd. This is an open access article under the CC BY license
(http://creativecommons.org/licenses/by/4.0/).
(http://creativecommons.org/licenses/by/4.0/).
License URL
Sponsor
Office Of Naval Research Global
Grant Number
N62909-15-1-2004
Subjects
09 Engineering
Materials
Publication Status
Published