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NASA NTRS · 19940012388

Stochastic damage evolution in textile laminates

Abstract

A probabilistic model utilizing random material characteristics to predict damage evolution in textile laminates is presented. Model is based on a division of each ply into two sublaminas consisting of cells. The probability of cell failure is calculated using stochastic function theory and maximal strain failure criterion. Three modes of failure, i.e. fiber breakage, matrix failure in transverse direction, as well as matrix or interface shear cracking, are taken into account. Computed failure probabilities are utilized in reducing cell stiffness based on the mesovolume concept. A numerical algorithm is developed predicting the damage evolution and deformation history of textile laminates. Effect of scatter of fiber orientation on cell properties is discussed. Weave influence on damage accumulation is illustrated with the help of an example of a Kevlar/epoxy laminate.

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BibTeXRIS

Dzenis, Yuris A., Bogdanovich, Alexander E., Pastore, Christopher M.. 1993-08-01. Stochastic damage evolution in textile laminates. https://ntrs.nasa.gov/citations/19940012388

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