NASA NTRS · 20170001032
Fracture-Based Mesh Size Requirements for Matrix Cracks in Continuum Damage Mechanics Models
Abstract
This paper evaluates the ability of progressive damage analysis (PDA) finite element (FE) models to predict transverse matrix cracks in unidirectional composites. The results of the analyses are compared to closed-form linear elastic fracture mechanics (LEFM) solutions. Matrix cracks in fiber-reinforced composite materials subjected to mode I and mode II loading are studied using continuum damage mechanics and zero-thickness cohesive zone modeling approaches. The FE models used in this study are built parametrically so as to investigate several model input variables and the limits associated with matching the upper-bound LEFM solutions. Specifically, the sensitivity of the PDA FE model results to changes in strength and element size are investigated.
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Leone, Frank A., Davila, Carlos G., Mabson, Gerald E., Ramnath, Madhavadas, Hyder, Imran. 2017-01-09. Fracture-Based Mesh Size Requirements for Matrix Cracks in Continuum Damage Mechanics Models. https://ntrs.nasa.gov/citations/20170001032
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