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.hindawi.com/articles/ijae/volume-2015/473926/figures/473926.fig.001a.svgz" name="473926.fig.001a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Structure-similarity scale model of composite wing</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2015/473926/figures/473926.fig.001b.svgz" name="473926.fig.001b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Cross section of the model</td></tr></table>

<div>Structure-similarity scale model of composite wing and cross section of the model.</div>

International Journal of Aerospace Engineering

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Figure 1

Figure 1: Effect of Interfacial Debonding on the Strength of Composite Structure-Similarity Scale Model for the Wing-Box 