Effect of Interfacial Debonding on the Strength of Composite Structure-Similarity Scale Model for the Wing-Box

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2015/473926/figures/473926.fig.002a.svgz" name="473926.fig.002a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Wing-box structure</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2015/473926/figures/473926.fig.002b.svgz" name="473926.fig.002b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Wing-box cross section containing ribs</td></tr></table>

<div>Schematic diagram of composite wing-box. ① Skin. ② C beam. ③ Rib plate. ④ Bonding interface.</div>

International Journal of Aerospace Engineering

fig2

Figure 2

Figure 2: Effect of Interfacial Debonding on the Strength of Composite Structure-Similarity Scale Model for the Wing-Box 