Failure Mode Analysis of Carbon Fiber Composite Laminates by Acoustic Emission Signals

<div>The time curve of maximum loading force and displacement. (a) [0<sub>8</sub>]<sub><i>s</i></sub>. (b) [0/45/0/- 45/0<sub>4</sub>]<sub><i>s</i></sub>.</div>

Advances in Materials Science and Engineering

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Figure 7

Figure 7: Failure Mode Analysis of Carbon Fiber Composite Laminates by Acoustic Emission Signals 