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Evaluation of the strain gradient effect on compressive failure of CRFP composites
Tobias Bianchi  1, 2@  , Christophe Bouvet * , Joël Serra  3, *@  , Léon Ratsifandrihana  4, *@  
1 : Institut Supérieur de lÁéronautique et de lÉspace
ICA (Institut Clément Ader)
2 : Segula Technologies [France]
Segula Techologies, ZAC des Ramassiers, Equinox, 24 Boulevard Deodat de Séverac, 31770 Colomiers
3 : Institut Clément Ader
Institut Supérieur de l'Aéronautique et de l'Espace, Institut National des Sciences Appliquées - Toulouse, Université Toulouse III - Paul Sabatier, Centre National de la Recherche Scientifique, IMT École nationale supérieure des Mines d'Albi-Carmaux
4 : Ségula Technologie
Ségula Technologie
* : Corresponding author

A pin-ended buckling test, inspired by Wisnom (M. Wisnom, 1992), was designed to examine the influence of strain gradients on the compressive failure strain of composite laminates. The study focused on unidirectional (UD) carbon/epoxy AS4/8552, with strain measurements obtained via digital image correlation. Cross-ply stacking sequences—[(0/90)₂]s, [(0/90)₄]s, [(0/90)₈]s—as well as unidirectional configurations [0]₈ and [0]₁₆ were tested to explore the impact of specimen thickness on compressive failure strain. Most specimens failed on the tension side, driven by the high compressive strength induced by the strain gradient, while the tensile failure strain remained unaffected. To provoke failure on the compression side, an innovative approach was employed by adding an aluminum 2024 ply to the top tension side of bi-material specimens, resulting in all specimens failing on the compression side. The findings revealed a non-linear relationship between compressive failure strain and the strain gradient, contrasting with Wisnom's linear trend. Furthermore, we've obtained for the thinner specimens, values that go up to -33000 micro strains, which is more than 2.5 times the compressive failure of -12500 micro strains.

Wisnom, M. 1992. « On the High Compressive Strains Achieved in Bending Tests on Unidirectional Carbon-Fibre/Epoxy ». Composites Science and Technology 43 (3): 229‑35. https://doi.org/10.1016/0266-3538(92)90093-I.


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