Reduction of Free Edge Peeling Stress of Laminated Composites Using Active Piezoelectric Layers

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</svg> distribution of [PZT/45<sub>4</sub>/−45<sub>4</sub>]s laminate at the interface of <svg height="14.85" id="M142" style="vertical-align:-0.17555pt" version="1.1" viewbox="0 0 73.25 14.85" width="73.25" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg>, under −0.1% uniaxial strain.</table>

The Scientific World Journal

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Figure 10

Figure 10: Reduction of Free Edge Peeling Stress of Laminated Composites Using Active Piezoelectric Layers 