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

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</svg> distribution of [PZT/0<sub>4</sub>/90<sub>4</sub>]s laminate at the free edge, under 0.1% uniaxial strain.</table>

The Scientific World Journal

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Figure 6

Figure 6: Reduction of Free Edge Peeling Stress of Laminated Composites Using Active Piezoelectric Layers 