Abstract
The micro mechanisms of flexure damage at the notch tip in a three-dimensionally braided carbon/carbon composite (3D-C/C) were investigated in real-time through a Scanning Electron Microscopy. It was found that the damage was nucleated in the fibre bundle/matrix interface around the notch tip. The different damage modes were found in different directions of the 3D-C/C. The x-directional flexural specimens seem to be insensitive to the pre-notch while the z-directional flexural specimens seem to be sensitive to the pre-notch. Fibre yarns acted as an obstacle to crack propagation and it was necessary to increase the load to propagate the crack through the adjacent fibre yarn. Comparing with the x-directional flexural specimens, the forces could be better transmitted in z-directional flexural specimens because the fibres of z-direction bundles can tightly adjoin to each other.
| Original language | English |
|---|---|
| Pages (from-to) | 131-137 |
| Number of pages | 7 |
| Journal | Advanced Composites Letters |
| Volume | 18 |
| Issue number | 4 |
| DOIs | |
| State | Published - 2009 |
Keywords
- Carbon/carbon composites
- Damage
- Flexure fracture
- Microstructure
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