Numerical Analysis of Dynamic Response of Corrugated Core Sandwich Panels Subjected to Near-Field Air Blast Loading

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/sv/volume-2014/180674/figures/180674.fig.008a.svgz" name="180674.fig.008a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Front face</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/sv/volume-2014/180674/figures/180674.fig.008b.svgz" name="180674.fig.008b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Back face</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/sv/volume-2014/180674/figures/180674.fig.008c.svgz" name="180674.fig.008c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Corrugated core</td></tr></table>

<div>Deformation and failure patterns of a sandwich panel (case number S20-1). (For interpretation of the references to colour in this figure legend, the reader is referred to the web version of this paper.)</div>

Shock and Vibration

fig8

Figure 8

Figure 8: Numerical Analysis of Dynamic Response of Corrugated Core Sandwich Panels Subjected to Near-Field Air Blast Loading 