2015
DOI: 10.1016/j.compositesa.2014.09.009
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Characterization of strain-softening behavior and failure mechanisms of composites under tension and compression

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Cited by 85 publications
(52 citation statements)
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“…in coupon tests [2][3][4][5][6][7] and observed in full-scale composite structural tests [8]. On the other hand, many existing approaches for modelling Mode I trans-laminar fracture [9][10][11][12] do not directly address R-curves and assume a constant Mode I trans-laminar fracture toughness value during fracture propagation.…”
Section: Introductionmentioning
confidence: 99%
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“…in coupon tests [2][3][4][5][6][7] and observed in full-scale composite structural tests [8]. On the other hand, many existing approaches for modelling Mode I trans-laminar fracture [9][10][11][12] do not directly address R-curves and assume a constant Mode I trans-laminar fracture toughness value during fracture propagation.…”
Section: Introductionmentioning
confidence: 99%
“…Catalanotti et al [18] also applied their method to QI CP-T700/ACE Non-Crimp Fabrics. The approaches [6,10,11,18] to determine trans-laminar fracture toughness either rely on inputs from modelled notched tests [10,11], or the results from separate sets of scaled notched tensile tests [18]. The numerical prediction of R-curves for QI laminates without input parameters from the modelled fracture tests has not been reported before.…”
Section: Introductionmentioning
confidence: 99%
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“…Furthermore, addition of HGB particles results in the fading of strain softening and disappearance of cold drawing. Fragmentation of large crystallites and their deformation/reorientation were the main cause of the strain softening accompanied with a localization of the plastic deformation in post‐yield behavior of PP . The results reveal the reduction in the ductility of the polymer is accompanied with the incorporation of HGB particles.…”
Section: Resultsmentioning
confidence: 90%
“…Failure of these materials involves evolution of various damage mechanisms, such as fibre breakage and matrix cracks [38,14], where the debonding of adjacent laminate layers, also known as delamination, is considered to be one of the most dominant damage mechanisms affecting the behaviour of composite laminates. Delamination will usually lead to a reduction in structural stiffness and load carrying capability, and can also lead to instability and premature structural failure under compressive loading [2].…”
Section: Introductionmentioning
confidence: 99%