We have developed physically-based failure models for different failure modes in composites, namely matrix cracking, fibre kinking and fibre tensile failure. These failure models were used in the participation of the group in the second World-wide Failure Exercise, a benchmark exercise where selected researchers were asked to provide blind predictions for several cases. The blind predictions from the models were ranked first both quantitatively and qualitatively.
Sample publications:
Pinho ST, Davila CG, Camanho PP, Iannucci L, Robinson P et al., 2005, Failure models and criteria for FRP under in-plane or three-dimensional stress states including shear non-linearity, Technical Memorandum, Langley, Publisher: National Aeronautics and Space Administration, Langley Research Center, NASA/TM-2005-213530
Pinho ST, Iannucci L, Robinson P, 2006, Physically-based failure models and criteria for laminated fibre-reinforced composites with emphasis on fibre-kinking. Part I: Development, Composites: Part A, Vol: 37, Pages: 63-73
Pinho ST, Darvizeh R, Robinson P, Schuecker C, Camanho PP et al., 2012, Material and structural response of polymer-matrix fibre-reinforced composites, JOURNAL OF COMPOSITE MATERIALS, Vol: 46, Pages: 2313-2341
Pimenta S, Pinho ST, 2013, Hierarchical scaling law for the strength of composite fibre bundles, Journal of the Mechanics and Physics of Solids, Vol: 61
Bullegas G, Moledo Lamela J, Pimenta S, Pinho STet al., 2020, On the role of dynamic stress concentrations and fracture mechanics in the longitudinal tensile failure of fibre-reinforced composites, Engineering Fracture Mechanics, Vol: 228, Pages: 1-31
In 2002-2004, when developing the first regularised smeared-crack model for laminated composites, we needed ply-level translaminar fracture toughness values. At the time, these toughnesses did not exist even as a concept. Since then, we have developed and perfected experimental tests to measure translaminar toughness in tension and compression, for UD and woven plies, for plies with fibres at an angle, and we have demonstrated how the toughness depends on the thickness of the plies.
Sample publications:
By noticing the key role played by hierarchy in the fibre tensile failure mode in UD plies, the group developed the first analytical model in the literature that is capable of predicting the translaminar fracture toughness of UD plies. This model can be used not only for structural design, but also for material development, since the predictions are obtained from fibre / matrix / interface properties.
Sample publications:
B. Yu, T.J. Katafiasz, S. Nguyen, G. Allegri, J. Finlayson, E.S. Greenhalgh, S.T. Pinho, S. Pimenta. Hygrothermal effects on the translaminar fracture toughness of a highly toughened aerospace CFRP: Experimental characterisation and model prediction,
Composites Part A: Applied Science and Manufacturing,
Volume 150,
2021,
106582
B. Yu, T. J. Katafiasz, S. Nguyen, G. Allegri, J. Finlayson,
E. S. Greenhalgh, S. T. Pinho, S. Pimenta. Characterising and predicting the relationship between
translaminar fracture toughness and pull-out length distributions
under distinct temperatures. Philosophical Transactions A, 2022
When analysing the mechanical response of recycled composites composed of short fibres and bundles dispersed stochastically in a resin matrix, we noticed that the hierarchy of bundles of different sizes was key in determining the energy dissipated during fracture of these materials. These bundles, which were until then considered to be a manufacturing defect in recycled composites, became a material design parameter which can be used to achieve desired damage tolerance, in both recycled and virgin discontinuous carbon fibre systems.
Sample publications:
Soraia Pimenta, Silvestre T. Pinho,
The influence of micromechanical properties and reinforcement architecture on the mechanical response of recycled composites,
Composites Part A: Applied Science and Manufacturing,
Volume 56,
2014,
Pages 213-225
We developed the first regularised smeared-crack model for laminated composite plies. The stability of smeared crack models made this model particularly well suited for structural design, and this model has now become available in a leading Finite Element software package. We have since developed a new floating node method which outperforms existing methods in simulating kinking cracks. Looking at a different scale, we have also developed a Molecular Dynamics Finite Element model for simulating large graphene-based structures from the underlying force fields.
Sample publications:
Nature does not design materials the way engineers and scientists do. There is much to benefit from learning why certain biological materials have evolved the way they did so that we can understand what failure mechanisms are responsables for their often outstanding properties. Equipped with this, we can then investigate whether we can create corresponding artificial materials that aim at exhibiting equivalent failure mechanisms.
Sample publications: