The Abaqus damage model for fiber reinforced plastics has been reimplemented as UMAT user material. As an extension, the plastic behavior of the matrix material is taken into account. Therefore, two modes are considered independently from each other: matrix shear and matrix compression. The original as well as the new material model have been verified by means of single element tests, mesh dependency tests, and the standard plate-with-a-hole problem. In addition, a shell-type structure, namely an industrial model of the Boeing-777 Winglet, has been analyzed.
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