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Composites modelling is made easier in COMSOL® by using the layered material technology, a micromechanics model of a single carbon fiber in epoxy is used to estimate the elastic properties of a single layer which in turn is applied along with orientation for many layers of the laminated composite. we have available a free trial for 30 days of the Composite Materials Module. You can find out more by following the hyperlink to the COMSOL® website.

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  • Thermal Expansion of a Laminated Composite Shell

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    The effect of the position of a heat source on the stress and deformation profiles is studied. The example also demonstrates the computation of homogenized thermal expansion coefficients of individual laminae.

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  • Stress Analysis of a Composite Cylinder

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    The composite material is typically a laminate of individual layers, where the fibers in each layer are uni-directional. In this model, we perform a stress analysis of a laminated composite cylinder.

    Modeling individual fibers in every layer in the laminate is unfeasible. A simplified micromechanics model of a single carbon fiber in epoxy is instead used to estimate the elastic properties of a single layer. These properties are then used in the homogenized model of the laminated composite cylinder.

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  • Layered Material Technology

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    Composite laminates are made up of several layers of different materials, fiber orientations, thickness, and so on. In order to visualize the layup and provide the information in a convenient manner, the Composite Materials Module offers a set of specialized tools.

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