Abstract
In the present study, the mixed-mode fracture toughness of three composite joint systems (2 secondary bonded and 1 co-cured) was investigated. The two secondary bonded systems predominantly resulted in cohesive failure with occasional interlaminar failure during mixed-mode loading while the co-cured system failed adhesively. This was attributed to moisture stored in the prepreg being released during the co-cure process.The mode II toughness was consistently 5-6 times that of the corresponding mode I case for each system. The increased toughness was due to a combination of an increased fracture surface area and a larger damage zone.
Original language | English |
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Pages (from-to) | 148-167 |
Number of pages | 20 |
Journal | Engineering Fracture Mechanics |
Volume | 134 |
DOIs | |
Publication status | Published - 1 Jan 2015 |
Externally published | Yes |
Keywords
- Aerospace vehicles
- Composites
- Fractography
- Fracture mechanics
- Mixed-mode fracture