1998
DOI: 10.1016/s0266-3538(97)00229-7
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On the effects of stitching in CFRPs—I. mode I delamination toughness

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Cited by 259 publications
(154 citation statements)
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“…When a composite structure is impacted, delamination often occurs, which seriously reduces the load bearing capacity of the laminate especially under compressive loads [5]. Therefore, several methods have been developed to improve the interlaminar strength and interlaminar fracture toughness of composite laminates, such as matrix toughening [6][7][8][9], through-thickness stitching [10][11][12][13][14], Z-pinning [15,16], and interleaving [17][18][19][20][21][22][23][24][25] and short-fibre interlaminar reinforcement [25]. Most of the above mentioned methods have been reviewed by Kim and Mai [26], who also pointed out the key role played by the fibre-matrix interfacial shear strength in determining the interlaminar resistance of composite laminates.…”
Section: Introductionmentioning
confidence: 99%
“…When a composite structure is impacted, delamination often occurs, which seriously reduces the load bearing capacity of the laminate especially under compressive loads [5]. Therefore, several methods have been developed to improve the interlaminar strength and interlaminar fracture toughness of composite laminates, such as matrix toughening [6][7][8][9], through-thickness stitching [10][11][12][13][14], Z-pinning [15,16], and interleaving [17][18][19][20][21][22][23][24][25] and short-fibre interlaminar reinforcement [25]. Most of the above mentioned methods have been reviewed by Kim and Mai [26], who also pointed out the key role played by the fibre-matrix interfacial shear strength in determining the interlaminar resistance of composite laminates.…”
Section: Introductionmentioning
confidence: 99%
“…The gradient in the linear region for sample group A1 (0) was bigger than that for all the MLS groups. MLS; for the MLS groups: B1 [20], C1 [10], D1 [5], E1 (10 × 10), and F1 (5 × 5), the NL displacement points are close to each other and appear near the maximum load point. The crack propagation proceeded steadily as shown in Fig.…”
Section: Load-displacement Curvesmentioning
confidence: 78%
“…Hence, these groups' load-displacement curves have a characteristic jagged shape and the average maximum load and displacement values were variable. In general, sample groups B1 [20], C1 [10], and D1 [5] which were stitched in one column have low values of load and displacement. Amongst these groups, B1 [20] and C1 [10] have the lowest maximum average load of 311.6 N with displacements of 16.3 and 17.0 mm respectively.…”
Section: Load-displacement Curvesmentioning
confidence: 97%
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“…Stitching improved the damage resistance properties of woven composite structure under blast load and ballistic impact load [24]. It was reported that stitching fiber base composites in the through-the-thickness direction enhanced the Mode I and Mode II interlaminar fracture toughness, which was experimentally determined by using double cantilever beam and an end-notched flexure test, respectively [25,26]. The critical strain-energy release rate increased because the stitching bridge the delamination [27,28].…”
Section: Methodsmentioning
confidence: 97%