Titlebook: Composite Mechanics; Andreas ?chsner Book 2023 The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature

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Composite Mechanics978-3-031-32390-4Series ISSN 1869-8433 Series E-ISSN 1869-8441

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Noorizam Daud,Kamarulzaman IbrahimThis chapter provides a very brief introduction to a user-friendly computational tool, which allows the application of the classical laminate theory to different problems of composite laminates. The Python-based tool?allows for classical stress and strain analyses, the generation of pole diagrams, and various approaches to the failure analysis.

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Introduction,rties than a single component for itself. The focus is on fiber-reinforced composites where a single layer has unidirectionally aligned reinforcing fibers. The second part of this chapter introduces to major idea and the continuum mechanical background to model structural members. It is explained th

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Micromechanics,stituents, i.e., fibers and matrix. The focus is on unidirectional lamina which can be described based on orthotropic constitutive equations. In detail, predictions for the modulus of elasticity in and transverse to the fiber direction, the major Poisson’s ratio, as well as the in-plane shear modulu

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Macromechanics of a Lamina,called lamina. It is shown that a lamina can be treated as a combination of a plane elasticity element and a classical plate element. For both classical structural elements and their combination, the continuum mechanical modeling based on the three basic equations, i.e., the kinematics relationship,

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,Macromechanics of?a?Laminate,laminate theory, a simplified stress analysis, a subsequent failure analysis is derived, without the solution of the system of coupled differential equations for the unknown displacements in the three coordinate directions. This theory provides the solution of the statically indeterminate system bas

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Example Problems,tep approach in order to present all the details of the solution procedure. The presented problems comprise the calculation of stresses and strains in symmetric and asymmetric laminates, the application of failure criteria, and the ply-by-ply failure of laminates. In addition, the characterization o

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