Evaluation of Defects in Multilayer Carbon Fibre Epoxy for Aeronautics Applications

<table class="table-group" width="800px"><tr class="fig-image" id="a"><td><img alt="647658.fig.001a" src="https://static.hindawi.com/articles/aav/volume-2009/647658/figures/647658.fig.001a.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(a) </b> Specific Young modulus is plotted versus specific strength.</td></tr></table></td></tr><tr class="fig-image" id="b"><td><img alt="647658.fig.001b" src="https://static.hindawi.com/articles/aav/volume-2009/647658/figures/647658.fig.001b.jpg"/></td></tr><tr class="fig-caption"><td align="center"><table><tr><td><b>(b) </b>Fracture toughness is plotted versus density.</td></tr></table></td></tr></table>

Advances in Acoustics and Vibration

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Figure 1

Figure 1: Evaluation of Defects in Multilayer Carbon Fibre Epoxy for Aeronautics Applications 