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Fracture mechanism of unidirectional carbon-fibre reinforced epoxy resin composite
The fatigue cracking characteristics of a unidirectional carbon-fiber reinforced epoxy resin composite (CFRP) were examined experimentally. Specimens 3- and 1-mm thick were subjected to three-point bending while being monitored for acoustic emissions (AE), using polarized transmission optical micros...
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Published in: | Journal of materials science 1986-03, Vol.21 (3), p.1005-1010 |
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Main Authors: | , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | The fatigue cracking characteristics of a unidirectional carbon-fiber reinforced epoxy resin composite (CFRP) were examined experimentally. Specimens 3- and 1-mm thick were subjected to three-point bending while being monitored for acoustic emissions (AE), using polarized transmission optical microscopy, and by SEM techniques. Failure occurred in four stages: (1) fiber breaking at a load of 60 percent of the failure load; (2) plastic deformation at the broken fiber tip, along the fiber sides, then matrix cracking in the plastic region; (3) partial delamination just before failure; and (4) catastrophic crack propagation from the site of delamination. Plastic deformation of the matrix around the broken tip of a fiber was attributed to shear stress concentration. Low amplitude AE signals were highly correlated by fiber breaking and matrix cracking. Higher amplitude AE were associated with the onset of delamination. (M.S.K.) |
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ISSN: | 0022-2461 1573-4803 |
DOI: | 10.1007/BF01117386 |