Abstract
The residual mechanical properties and damage tolerance of carbon fibre-reinforced composites containing unmodified and rubber-modified epoxy resins were evaluated after drop-weight impact damage. It is shown that the residual flexural strength and modulus (normalized to those without prior damage) are slightly higher for the modified matrix system than for the unmodified control, which is consistent with a smaller stiffness reduction for the modified matrix system evaluated from the compliance analysis against instantaneous crack length. Furthermore, the residual Mode I interlaminar fracture toughness (as determined by the potential energy release rates and the stress intensity factors) is significantly higher (by up to 80%, depending on the crack length) for the modified matrix system. The impact energy threshold is also evaluated based on a simple residual strength model to support the observed results.
Original language | English |
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Pages (from-to) | 485-494 |
Number of pages | 10 |
Journal | Composites |
Volume | 24 |
Issue number | 6 |
DOIs | |
Publication status | Published - Sept 1993 |
Externally published | Yes |
Keywords
- carbon fibres
- damage resistance
- damage tolerance
- epoxy
- impact energy threshold
- Mode I interlaminar fracture toughness
- residual stiffness
- residual strength and modulus
- rubber-modified epoxy
ASJC Scopus subject areas
- General Materials Science