Definitions
The modeling and simulation of the nonlinear mechanical response of laminated composites is treated. In the present context, a laminate consists of several stacked plies. Here, the smallest entities of consideration are the plies and their interfaces. Both are described by nonlinear elasto-damage constitutive laws. A number of approaches are introduced at material and interface level. Their utilization for structural simulations is discussed, including predictions for the response beyond peak load.
Introduction and Motivation
Laminated composites are widely used in lightweight design, typically in the form of shell structures. A number of plies with direction-dependent behavior are stacked together in various orientations to achieve preferable...
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Pettermann, H.E., Schuecker, C. (2019). Damage and Failure in Layered Composite Structures. In: Altenbach, H., Öchsner, A. (eds) Encyclopedia of Continuum Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-53605-6_11-1
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DOI: https://doi.org/10.1007/978-3-662-53605-6_11-1
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