Three-dimensional failure criteria for fiber-reinforced laminates

By G. Catalanotti, Pedro P. Camanho, António Torres Marques. 2013

203 citations recorded by the source corpus.

Subfields: Building and Construction, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/771afd730ed5073782f078cb42b4d68ee8abb300

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In Building and Construction

In Mechanics of Materials

Citations in the corpus

Micro-mechanical analysis of the in situ effect in polymer composite laminates (2014, methodology): “On the other hand, assuming that kink bands(1) are triggered by localised matrix failure in the vicinity of misaligned fibres, the in situ effect must have a direct, positive influence on the resistance to fibre kinking [42], therefore affecting the longitudinal compressive behaviour of laminated co”
Computational micromechanics of the transverse and shear behavior of unidirectional fiber reinforced polymers including environmental effects (2017, background): “Constitutive modelling, International463 Journal of Solids and Structures 50 (2013) 1897–1905.464 [15] K. Marlett, Y. Ng, J. Tomblin, E. Hooper, NCAMP Test Report: CAM-RP-2010-002 Rev A,465 Technical Report, National Institute for Aviation Research, 2011.466 [16] C. Lopes, S. Sádaba, C. González, ”
Experimental and numerical studies on the impact response of damage-tolerant hybrid unidirectional/woven carbon-fibre reinforced composite laminates (2018, unknown): “Parameters λ and κ are defined by λ = 2μLNS23 A /S12 A − κ ,and κ = (S12 A 2 − (YT) (2))/S23 A YT [52], where S12 A and S23 A are the shear strengths.”
Three-dimensional invariant-based failure criteria for fibre-reinforced composites (2015, methodology): “(2006) and Catalanotti et al. (2013).”
Notched response of non-crimp fabric thin-ply laminates (2013, background): “behavior (indicating that the in situ effect plays a role not only in tension, but also in compression, as 229 proposed in [10]), although it may also conduct to higher notch sensitivity.”
The role of interfacial properties on the intralaminar and interlaminar damage behaviour of unidirectional composite laminates: Experimental characterization and multiscale modelling (2018, methodology): “[27], was used for predicting matrix damage behaviour.”
Predicting low velocity impact damage and Compression-After-Impact (CAI) behaviour of composite laminates (2015, methodology): “[25], overcomes this limitation and was adopted in the damage model.”