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Micromechanics of reinforcement and damage initiation in carbon fibre/epoxy composites under fatigue loading

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TextSeries: ; Composites: Part A, 32A(3-4), p.457-471, 2001Contained works:

Koimtzoglou, C
Kostopoulos, V
Galiotis, C

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Abstract: A model single carbon fibre/epoxy composite geometry was subjected to cyclic loading at a maximum strain below the critical fatigue limit of the matrix material. The carbon fibres were pre-strained prior to incorporation in the resin to ensure that they were free of thermally induced compression stresses in the axial direction. A strain controlled cyclic experiment from 0 to 0.5

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A model single carbon fibre/epoxy composite geometry was subjected to cyclic loading at a maximum strain below the critical fatigue limit of the matrix material. The carbon fibres were pre-strained prior to incorporation in the resin to ensure that they were free of thermally induced compression stresses in the axial direction. A strain controlled cyclic experiment from 0 to 0.5

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