FEA - Abaqus Tutorials - Lateral deflection with different lamina layers

Consider a simply supported square plate a=2000mm, laminated with different layers. the laminate thickness is 10mm. the plate is compression with an edge load N=1N/mm. Tabulate the central deflection perpendicular to the plate surface when the number of layers is n=1,5,10,15 and 20.

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