2001
DOI: 10.1016/s0020-7225(00)00013-6
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A micro-mechanical model of woven fabric and its application to the analysis of buckling under uniaxial tension. Part 2: buckling analysis

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Cited by 22 publications
(6 citation statements)
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“…For densely woven fabrics substantial shear brings the yarns into contact laterally. This causes a pronounced increase in the effective shear stiffness which in turn generates compressive stresses that promote out-of-plane buckling [8]. To describe this effect quantitatively, appeal should be made to a suitable plate theory incorporating local bending resistance.…”
Section: Constitutive Equations and Materials Symmetrymentioning
confidence: 99%
See 1 more Smart Citation
“…For densely woven fabrics substantial shear brings the yarns into contact laterally. This causes a pronounced increase in the effective shear stiffness which in turn generates compressive stresses that promote out-of-plane buckling [8]. To describe this effect quantitatively, appeal should be made to a suitable plate theory incorporating local bending resistance.…”
Section: Constitutive Equations and Materials Symmetrymentioning
confidence: 99%
“…We are adapting the procedure used in [15]. From (8) it follows that f is the resultant force on the upper edge of the sheet generated by the statically admissible stress. (82) furnishes a lower bound on this force, denoted by f L .…”
Section: Conventional Position/traction Problemsmentioning
confidence: 99%
“…Xu et al (2006) investigated on the buckling analysis of triaxial woven fabric composite structures subjected to uniaxial loading numerically. Zhang and Fu (2000) made a micro mechanical model of woven fabric and its application to the analysis of buckling under uniaxial tension. In the present study, the influences of various parameters like effects of delamination area, number of layers, ply orientation and aspect ratios on the buckling load of industry driven practically important woven roving delaminated glass/epoxy composite plates are investigated under clamped-free-clamped-free (CFCF) boundary condition.…”
Section: Introductionmentioning
confidence: 99%
“…The specimen indicates pure shear deformation in zone A related to the crosshead displacement “ d ” as: where D is the length of the central zone A and θ is the angle between yarns. The stretching of the specimen leads to shear strain in zone B that is the half of that in the zone A 19–22 …”
Section: Theoretical Backgroundmentioning
confidence: 99%