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An analytical solution for pre-crack behaviour of laminated glass under blast loading
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1-s2.0-S026382231630099X-main.pdf | Published version | 2.06 MB | Adobe PDF | View/Open |
Title: | An analytical solution for pre-crack behaviour of laminated glass under blast loading |
Authors: | Del Linz, P Liang, X Hooper, PA Wang, LZ Dear, JP |
Item Type: | Journal Article |
Abstract: | Laminated glazing is often employed to minimise damage and injuries during blast events. In this work, the von Karman theory for large deflections of plates was used to simulate the effect of large explosions on laminated glazing. Linear material properties were assumed for both the glass and Polyvinyl Butyral layers. The glass and PVB layers were assumed to act fully compositely during the pre-crack phase of the deformation. A higher order deflection function was employed to represent the complex deformed shape observed in DIC blast test data collected by Hooper et al. [1]. The deflection results showed that the method developed could produce accurate estimates of the glazing deformation history during a blast event. The analytical solution was also used to compute the reaction forces acting on the window supports, which were found to be of a similar magnitude to those calculated from experimental data. In addition, crack densities were predicted, which were found to follow a pattern similar to those seen in blast experiments. The analytical approach developed is valuable for risk assessment engineers and façade designers who much prefer analytically based models over full-scale FE analysis, as FEA is often too time consuming for design assessments. |
Issue Date: | 26-Feb-2016 |
Date of Acceptance: | 19-Feb-2016 |
URI: | http://hdl.handle.net/10044/1/45101 |
DOI: | https://dx.doi.org/10.1016/j.compstruct.2016.02.058 |
ISSN: | 0263-8223 |
Publisher: | Elsevier |
Start Page: | 156 |
End Page: | 164 |
Journal / Book Title: | Composite Structures |
Volume: | 144 |
Copyright Statement: | © 2016 The Authors. Published by Elsevier Ltd. This is an open access article under the CC-BY license (http://creativecommons.org/licenses/by/4.0/) |
Sponsor/Funder: | Office Of Naval Research Global Beijing Institute of Aeronautical Materials (BIAM) Office Of Naval Research Global Engineering and Physical Sciences Research Council |
Funder's Grant Number: | N00014-12-1-0403 N/A N62909-15-1-2004 10001118 |
Keywords: | Science & Technology Technology Materials Science, Composites Materials Science Laminated glass Blast Large deflections Nonlinear STRAIN RATES 09 Engineering Materials |
Publication Status: | Published |
Appears in Collections: | Mechanical Engineering Faculty of Engineering |