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NASA NTRS · 19810020628

Mathematical modeling of damage in unidirectional composites

Abstract

A review of some approximate analytical models for damaged, fiber reinforced composite materials is presented. Using the classical shear lag stress displacement assumption, solutions are presented for a unidirectional laminate containing a notch, a rectangular cut-out, and a circular hole. The models account for longitudinal matrix yielding and splitting as well as transverse matrix yielding and fiber breakage. The constraining influence of a cover sheet on the unidirectional laminate is also modeled.

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BibTeXRIS

Goree, J. G., Dharani, L. R., Jones, W. F.. 1981-08-01. Mathematical modeling of damage in unidirectional composites. https://ntrs.nasa.gov/citations/19810020628

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