High-Velocity Impact Behaviour of Prestressed Composite Plates under Bird Strike Loading

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="372167.fig.006a" src="https://static.hindawi.com/articles/ijae/volume-2012/372167/figures/372167.fig.006a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b>No cohesive interfaces</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="372167.fig.006b" src="https://static.hindawi.com/articles/ijae/volume-2012/372167/figures/372167.fig.006b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>2 cohesive interfaces</td></tr></table></td></tr><tr class="fig-image" id="c"><td><img alt="372167.fig.006c" src="https://static.hindawi.com/articles/ijae/volume-2012/372167/figures/372167.fig.006c.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(c) </b>6 cohesive interfaces</td></tr></table></td></tr><tr class="fig-image" id="d"><td><img alt="372167.fig.006d" src="https://static.hindawi.com/articles/ijae/volume-2012/372167/figures/372167.fig.006d.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(d) </b>12 cohesive interfaces</td></tr></table></td></tr></table>

<table>Illustration of investigated delamination modelling approaches.</table>

International Journal of Aerospace Engineering

fig6

Figure 6

Figure 6: High-Velocity Impact Behaviour of Prestressed Composite Plates under Bird Strike Loading 