Yayın:
Buckling Delamination of a Rectangular Viscoelastic Sandwich Plate Containing Interface Inner Cracks

dc.contributor.authorAkbarov, S. D.
dc.contributor.authorYahnioglu, N.
dc.contributor.authorTekin, A.
dc.contributor.institutionauthorYAHNİOĞLU, Nazmiye
dc.date.accessioned2026-06-27T13:31:17Z
dc.date.issued2014
dc.description.abstractIn this paper, buckling delamination around interface inner cracks contained within the simply supported elastic and viscoelastic rectangular sandwich plate under biaxial loading is studied. It is assumed that the materials of the face layers are viscoelastic and the material of the core layer is pure elastic. Moreover, it is assumed that the material of the core layer is stiffer than the materials of the face layers. Within these assumptions it is supposed that between the face and core layers there are rectangular inner cracks, the locations of which are symmetric with respect to the plate geometry. The edge surfaces of the cracks have insignificant initial imperfections before the loading. The evolution of these initial imperfections with the flow of time is investigated within the scope of the three-dimensional (3D) geometrically nonlinear field equations of the theory of viscoelasticity. For determination of the values of the critical parameters (buckling force, time, and buckling mode), the initial imperfection criterion (i.e., the case where the size of the initial imperfection starts to increase and grows indefinitely) is used. Mathematical modeling of the corresponding boundary value problem is formulated within the framework of the piecewise homogeneous body model. To solve the corresponding boundary-value problems, boundary form perturbation techniques, the Laplace transform, 3D FEM modeling and the Schapery method are used. The numerical results related to the influence of the materials or geometrical parameters of the plate on the critical parameters and critical time are presented and analyzed.en
dc.description.urihttps://doi.org/10.1061/(asce)em.1943-7889.0000656
dc.identifier.doi10.1061/(asce)em.1943-7889.0000656
dc.identifier.eissn1943-7889
dc.identifier.endpage148
dc.identifier.issn0733-9399
dc.identifier.issue1
dc.identifier.startpage134
dc.identifier.urihttps://hdl.handle.net/20.500.14981/53500
dc.identifier.volume140
dc.identifier.wos000328556600013
dc.language.isoeng
dc.publisherASCE-AMER SOC CIVIL ENGINEERS
dc.relation.ispartofJOURNAL OF ENGINEERING MECHANICS
dc.subjectBuckling delamination
dc.subjectCritical buckling mode
dc.subjectCritical strain
dc.subjectCritical time
dc.subjectInterface inner crack
dc.subjectSandwich plate
dc.subjectViscoelastic material
dc.subjectThree-dimensional finite-element method (3D FEM)
dc.subjectSTABILITY LOSS
dc.subjectHALF-SPACE
dc.subjectCOMPOSITE
dc.subjectFRACTURE
dc.subjectFAILURE
dc.subjectPROPAGATION
dc.subjectELEMENTS
dc.subjectGROWTH
dc.subjectLAYERS
dc.subjectEngineering
dc.titleBuckling Delamination of a Rectangular Viscoelastic Sandwich Plate Containing Interface Inner Cracks
dc.typeArticle
dspace.entity.typePublication
local.import.sourceWOS

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