Abstract
Models for simulating interlaminar crack growth in composites under static and fatigue loads are rarely validated with experimental data different from simple standard tests where the crack front propagates with a uniform shape. The underlying reason for not making use of more realistic experimental data, where the crack front shape changes during the delamination growth, is the lack of well-controlled benchmark cases. This work introduces a comprehensive benchmark case consisting of a double cantilever beam (DCB)-like specimen with partially reinforced arms. A complete set of elastic and fracture properties for the material and a detailed description of load-displacement curves and crack front geometries, monitored with X-ray radiography, is provided. The benchmark case generates a rich phenomenology of crack advance in terms of varying crack growth rate and front shape, while being geometrically simple enough to be simulated.
Original language | English |
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Journal | Composite Structures |
Volume | 210 |
Pages (from-to) | 932-941 |
Number of pages | 10 |
ISSN | 0263-8223 |
DOIs | |
Publication status | Published - 15 Feb 2019 |
Keywords
- 3D analysis
- Benchmarking
- Delamination
- Fatigue