2021
DOI: 10.1016/j.compstruct.2021.114406
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Guided wave scattering at a delamination in a quasi-isotropic composite laminate: Experiment and simulation

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Cited by 37 publications
(31 citation statements)
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References 43 publications
(60 reference statements)
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“…A 20mm diameter circular zero volume delamination was incorporated into the model by overwriting existing elements at the delamination location [19]. A square area of new nodes with approximate dimensions of the delamination, connected to one side of the plate, were defined.…”
Section: Finite Element Simulationsmentioning
confidence: 99%
See 1 more Smart Citation
“…A 20mm diameter circular zero volume delamination was incorporated into the model by overwriting existing elements at the delamination location [19]. A square area of new nodes with approximate dimensions of the delamination, connected to one side of the plate, were defined.…”
Section: Finite Element Simulationsmentioning
confidence: 99%
“…The amplitude of the forward scattered wave is dependent on the delamination size, shape, and thickness of the sub-laminate (i.e., delamination depth) [7,16,17]. Delaminations located at an asymmetric depth experience high trapped amplitude on top of the delamination, with some forward scattering occurring, whereas delaminations located towards the mid-plane experience a much greater forward scattered amplitude, but limited wave trapping [18,19]. Anisotropy of individual ply layers, and the layup of the laminate can influence guided wave propagation and scattering directivity [20].…”
Section: Introductionmentioning
confidence: 99%
“…Using ultrasonic guided waves is a common method for periodic inspection and monitoring of structural integrity of plate-like composite laminates, that offers large inspection areas and sensitivity to structural damage of various kinds [6][7][8]. To date, many studies are available that employ guided waves for the detection and quantification of impact damage [9][10][11][12], delaminations [13][14][15][16][17], and other defects in composite laminates. Guided wave propagation in composites is determined by many factors, including, but not limited to, multi-layered structure and anisotropy, object boundaries, dispersion, multiple co-existing modes, and mode conversion.…”
Section: Introductionmentioning
confidence: 99%
“…In thin composite structures, matrix cracking caused by impact is generated from the lowest ply layer because of bending stress. In addition, a reverse pine-tree pattern is formed, since intra-ply cracks and interface delamination propagate from the lowest surface to the impact surface [ 11 ]. In thick composite structures, the damage propagates away from the impact location in the shape of a cone and forms a pin-tree pattern [ 11 ].…”
Section: Introductionmentioning
confidence: 99%
“…In addition, a reverse pine-tree pattern is formed, since intra-ply cracks and interface delamination propagate from the lowest surface to the impact surface [ 11 ]. In thick composite structures, the damage propagates away from the impact location in the shape of a cone and forms a pin-tree pattern [ 11 ]. It is also demonstrated that thicker composite structures have higher bending stiffness and higher compression after impact strength [ 8 ].…”
Section: Introductionmentioning
confidence: 99%