Abstract
This work is based on the investigation, both experimentally and numerically, of the
Mode II fracture process and bond strength of bondlines formed in co-cured composite/metal
joints. To this end, GFRP-to-steel double strap joints were tested in tension, so that the bimaterial
interface was subjected to shear with debonding occurring under Mode II conditions.
The study of the debonding process and thus failure of the joints was based both on stress and
energy considerations. Analytical formulas were utilized for the derivation of the respective
shear strength and fracture toughness measures which characterize the bi-material interface, by
considering the joint’s failure load, geometry and involved materials. The derived stress and
toughness magnitudes were further utilized as the parameters of an extrinsic cohesive law,
applied in connection with the modeling the bi-material interface in a finite element simulation
environment. It was concluded that interfacial fracture in the considered joints was driven by
the fracture toughness and not by strength considerations, and that LEFM is well suited to
analyze the failure of the joint. Additionally, the double strap joint geometry was identified and
utilized as a characterization test for measuring the Mode II fracture toughness of brittle bimaterial
interfaces.
| Original language | English |
|---|---|
| Journal | Applied Composite Materials |
| Volume | 21 |
| Pages (from-to) | 905–919 |
| ISSN | 0929-189X |
| DOIs | |
| Publication status | Published - 2014 |
Keywords
- Fracture characterization
- Cohesive law
- Interfacial debonding
- Composite-to-metal
- Bi-material interface
- LEFM
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