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NASA NTRS · 19930031732

Three-dimensional finite element simulation of intermingled-fiber hybrid composite behavior

Abstract

Three-dimensional finite element methods and the intraply hybrid micromechanics equations are used to predict composite properties for a unidirectional graphite-epoxy primary composite with S-glass fibers used as hybridizing fibers. The micromechanics equations are embedded in a computer code ICAN (Integrated Composites Analyzer). The three-dimensional finite element model consists of three-by-three unit cell array, with a total fiber volume ratio of 0.54. There is a good agreement between the composite properties and microstresses obtained from both methods. The results indicate that the finite element methods and micromechanics equations can be used to obtain the properties of intermingled hybrid composites needed for analysis/design of hybrid composite structures.

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BibTeXRIS

Mital, Subodh K., Chamis, Christos C.. 1992-01-01. Three-dimensional finite element simulation of intermingled-fiber hybrid composite behavior. https://ntrs.nasa.gov/citations/19930031732

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