Evaluation of Defects in Multilayer Carbon Fibre Epoxy for Aeronautics Applications

<table>Example of the architecture of MLFs. Layers of unidirectional oriented fibres, made of adjacent spread tows, are stacked together automatically and then fixed with stitching.</table>

Advances in Acoustics and Vibration

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Figure 2

Figure 2: Evaluation of Defects in Multilayer Carbon Fibre Epoxy for Aeronautics Applications 