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Computational Mechanics &
Advanced Materials Group
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Plate Figure 1. Out of plane shear stresses ?xz and ?yz evaluated for 3 layers, non homogeneous, orthotropic, square, and simply supported plate, fiber orientation 0/90/0, distribution along the thickness. Elasticity is the analytical solution (see Pagano 1970), FSDT in the First Order Deformation Theory, Current Work is the proposed model |
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