Abstract
Stitching advanced carbon-fibre composites in the through-thickness direction enhances the interlaminar fracture toughness. The mode I delamination toughness of a carbon/epoxy composite, both unstitched and stitched, was experimentally determined by using double-cantilever beam specimens. Specimens with varying stitch density, thread diameter and thread type were studied. The steady-state toughnesses, GIRs, of unstitched and stitched specimens have been compared. The addition of stitching was found to create an improvement in toughness of up to 15 times. The energy-dissipating crack propagation processes were determined and critical parameters identified. In addition, experimental results were compared with theoretical predictions from a micromechanics-based model developed previously and good agreement was found.
Original language | English |
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Pages (from-to) | 815-827 |
Number of pages | 13 |
Journal | Composites Science and Technology |
Volume | 58 |
Issue number | 6 |
DOIs | |
Publication status | Published - 1998 |
Externally published | Yes |
Keywords
- A. textile composites
- B. fracture toughness
- C. delamination
- C. fibre bridging
- E. resin transfer moulding (RTM)
ASJC Scopus subject areas
- Ceramics and Composites
- General Engineering