Abstract
The failure mechanisms of two short-alumina-fibre-reinforced epoxy resin composites (with and without rubber) have been investigated over a range of temperatures (-70°C to 100°C) and displacement rates (5 × 10-2 mm/min to 1·8 × 105 mm/min.). The fracture toughness, KIC, of these materials is highly rate dependent but is insensitive to temperature below 50°C. Addition of alumina fibres to the epoxy matrix significantly improves the low-temperature fracture toughness. High displacement rates and low temperatures tend to promote brittle fracture with little fibre debonding and fibre pull-out. However, low displacement rates and high temperatures lead to the formation of highly non-planar fracture surfaces with extensive fibre debonding, fibre pull-out and substantial plastic shear flow of the matrix material. A qualitative model in terms of residual stresses at the fibre-matrix interface is presented to describe the temperature-dependent failure mechanisms in these composite materials.
Original language | English |
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Pages (from-to) | 3-12 |
Number of pages | 10 |
Journal | Composites Science and Technology |
Volume | 43 |
Issue number | 1 |
DOIs | |
Publication status | Published - 1992 |
Externally published | Yes |
Keywords
- alumina fibre toughened epoxies
- failure mechanisms
- fibre debond/pullout
- fracture toughness
- residual stresses
- shear matrix flow
- temperature rate effects
ASJC Scopus subject areas
- Ceramics and Composites
- General Engineering