Damage in single lap joints of woven fabric reinforced polymeric composites subjected to transverse impact loading

Journal article


Choudhry, Rizwan Saeed, Hassan, Syed F., Li, Shuguang and Day, Richard 2015. Damage in single lap joints of woven fabric reinforced polymeric composites subjected to transverse impact loading. International Journal of Impact Engineering. https://doi.org/10.1016/j.ijimpeng.2015.02.003
AuthorsChoudhry, Rizwan Saeed, Hassan, Syed F., Li, Shuguang and Day, Richard
Abstract

Single lap joints of woven glass fabric reinforced phenolic composites, having four different overlap widths, were impacted transversely using a hemispherical impactor with different velocities in the low velocity impact range. The resulting damage was observed at various length scales (from micro to macro) using transmission photography, ultrasonic c-scan and x-ray micro tomography (XMT), in support of each other. These experimental observations were used for classification of damage in terms of damage scale, location (i.e. ply, interfaces between plies or bond failure between the two adherends) and mechanisms, with changing overlap width and impact velocity. In addition, finite element analysis was used to simulate delamination and disbond failure. These simulations were used to further explain the observed dependence of damage on overlap width and impact velocity. The results from these experiments and simulations lead to the proposal of a concept of lower and upper characteristic overlap width. These bounds relate the dominant damage pattern (i.e. scale, location and mechanism) with overlap width of the joint for a given impact velocity range.

Single lap joints of woven glass fabric reinforced phenolic composites, having four different overlap
widths, were impacted transversely using a hemispherical impactor with different velocities in the low
velocity impact range. The resulting damage was observed at various length scales (from micro to macro)
using transmission photography, ultrasonic c-scan and x-ray micro tomography (XMT), in support of
each other. These experimental observations were used for classification of damage in terms of damage
scale, location (i.e. ply, interfaces between plies or bond failure between the two adherends) and
mechanisms, with changing overlap width and impact velocity. In addition, finite element analysis was
used to simulate delamination and disbond failure. These simulations were used to further explain the
observed dependence of damage on overlap width and impact velocity. The results from these experiments
and simulations lead to the proposal of a concept of lower and upper characteristic overlap width.
These bounds relate the dominant damage pattern (i.e. scale, location and mechanism) with overlap
width of the joint for a given impact velocity range.

KeywordsComposite joints; Impact damage; Delamination modelling; Disbond; X-ray tomography; Glass phenolic composites
Year2015
JournalInternational Journal of Impact Engineering
PublisherElsevier
ISSN0734743X
Digital Object Identifier (DOI)https://doi.org/10.1016/j.ijimpeng.2015.02.003
Web address (URL)http://hdl.handle.net/10545/621998
hdl:10545/621998
Publication dates16 Feb 2015
Publication process dates
Deposited29 Nov 2017, 16:23
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Archived with thanks to International Journal of Impact Engineering

ContributorsNational University of Sciences and Technology, University of Manchester, University of Nottingham and Glyndŵr University
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