2017
DOI: 10.1007/s10853-017-1859-y
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Prediction of Mode I interlaminar fracture toughness of stitched flax fiber composites

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Cited by 24 publications
(20 citation statements)
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References 41 publications
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“…Figure 9b confirms unique behavior for all of the DCB specimens and shows good repeatability of the tests for a NFRPC. This behavior of the DCBs perfectly agrees with the observations of Ravanid et al [62][63][64] for woven and UD-FFREC DCBs, which were stiffened by GFRP/CFRP tabs on both sides, as well as with those of Bensadoun et al [57] for cross-ply (UD [0 90]4s) FFRECs laminate stiffened likewise and those of Saidaine et al [68] for woven flax/epoxy composite. Investigating woven/vinyl-ester DCB specimens, Almansour et al [47] also observed an initial linear response followed by a nonlinear curve up to the peak load.…”
Section: Mode I Interlaminar Fracture Toughnesssupporting
confidence: 88%
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“…Figure 9b confirms unique behavior for all of the DCB specimens and shows good repeatability of the tests for a NFRPC. This behavior of the DCBs perfectly agrees with the observations of Ravanid et al [62][63][64] for woven and UD-FFREC DCBs, which were stiffened by GFRP/CFRP tabs on both sides, as well as with those of Bensadoun et al [57] for cross-ply (UD [0 90]4s) FFRECs laminate stiffened likewise and those of Saidaine et al [68] for woven flax/epoxy composite. Investigating woven/vinyl-ester DCB specimens, Almansour et al [47] also observed an initial linear response followed by a nonlinear curve up to the peak load.…”
Section: Mode I Interlaminar Fracture Toughnesssupporting
confidence: 88%
“…It should be noted that they have used Modified Compliance Calibration method but have stated that used Modified Beam Theory (MBT). Ravandi et al [62][63][64] conducted experimental investigations, according to ASTM D5528, and numerical analysis, using FEM, to study and predict the effects of through-the-thickness stitching and reinforcement architecture on the G IC of the UD (V f ≈ 0.31) and woven fabric (V f ≈ 0.40) FFRECs. The authors tested double cantilever beams (DCBs), according to ASTM D5528, to determine the G IC of the FFRECs as well as UD-glass/epoxy (V f = 0.60) composites, and observed that average G IC of the UD-glass/epoxy was less than half of that of unstitched UD-FFRECs (G IC ≈ 1.3 kJ/m 2 ).…”
Section: Introductionmentioning
confidence: 99%
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“…The cohesive zone length is generally smaller under Mode I loading condition. 32,33 Therefore, in this study, the mesh size is chosen based on the cohesive zone length for Mode I loading. Additionally, a mesh refinement study is conducted with three different meshes, 0.75 mm, 0.60 mm and 0.5 mm to ensure the accuracy and convergence of results.…”
Section: Fem Simulation and Resultsmentioning
confidence: 99%
“…In this technique, the composite can be fabricated by (i) reinforcement of un-cured pre-preg (pre-impregnated) laminates in the direction of a thickness (Z-pinning technique) ( Figure 9 a), and (ii) employment of dry fabric preforms that already includes the through-thickness reinforcement before the resin infusion (stitching). Modified lockstitch, lockstitch, and chain stitch are commonly used stitching techniques ( Figure 9 b–d) [ 190 , 191 , 192 , 193 ]. As for the weave preform, the best structural arrangement is the twill weave fabric due to its having the highest impact strength, which results in higher required force to pull out or break the fibers [ 194 ].…”
Section: Mechanical Properties Of Hybrid Biocompositesmentioning
confidence: 99%