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

Tipo de material: Texto

TextoSeries ; Composites: Part A, 32A(3-4), p.457-471, 2001Trabajos contenidos:

Koimtzoglou, C
Kostopoulos, V
Galiotis, C

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Resumen: 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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Previous	B-7548 The development of compression damage zones in fibrous composites	B-7549 Assessment of strains along fiber surface features in graphite/epoxy composites loaded in compression	B-755 Overall crystallization kinetics of thin polymer films. General theoretical approach. I. Volume nucleation	B-7550 Micromechanics of reinforcement and damage initiation in carbon fibre/epoxy composites under fatigue loading	B-7551 Micromechanical aspects of fibre/crack interactions in an aramid/epoxy composite	B-7552 Structure and deformation mechanisms in UHMWPE-fibres	B-7553 Characterization and micromechanical testing of the interphase of aramid-reinforced epoxy composites	Next

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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