Vibration and stability analysis of functionally graded sandwich beams by a multi-layer finite element

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This paper presents a finite element model based on the first-order shear deformation theory for free vibration and buckling analyses of functionally graded (FG) sandwich beams. The present element has 3 N + 7 degrees-of-freedom for an N-layer beam. Lagrange's equations are employed for derivation of the equations of motion. Two types of FG sandwich beams are considered: (a) Type A with FG faces and homogeneous ceramic core, and (b) Type B with homogeneous ceramic and metal faces and FG core. Natural frequencies and buckling loads are calculated numerically for different boundary conditions, power-law indices, and span-to-height ratios. Accuracy of the present element is demonstrated by comparisons with the results available, and discussions are made on the results given in graphs and tables for the sandwich beams considered.

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dc.contributor.authorKahya, Volkan
dc.contributor.authorTuran, Muhittin
dc.date.accessioned2026-10-29T19:11:27.098878535Z
dc.date.available2026-10-29T19:11:27.098878535Z
dc.date.issued2018
dc.description.abstractThis paper presents a finite element model based on the first-order shear deformation theory for free vibration and buckling analyses of functionally graded (FG) sandwich beams. The present element has 3 N + 7 degrees-of-freedom for an N-layer beam. Lagrange's equations are employed for derivation of the equations of motion. Two types of FG sandwich beams are considered: (a) Type A with FG faces and homogeneous ceramic core, and (b) Type B with homogeneous ceramic and metal faces and FG core. Natural frequencies and buckling loads are calculated numerically for different boundary conditions, power-law indices, and span-to-height ratios. Accuracy of the present element is demonstrated by comparisons with the results available, and discussions are made on the results given in graphs and tables for the sandwich beams considered.
dc.identifier.doi10.1016/j.compositesb.2018.04.011
dc.identifier.eissn1879-1069
dc.identifier.endpage212
dc.identifier.issn1359-8368
dc.identifier.scopus2-s2.0-85045678213
dc.identifier.startpage198
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/bayburt/13784
dc.identifier.volume146
dc.identifier.wosWOS:000436224500021
dc.language.isoen
dc.publisherElsevier Ltd
dc.relation.ispartofComposites Part B: Engineering
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectBuckling
dc.subjectFinite element method
dc.subjectFirst-order shear deformation theory
dc.subjectFree vibration
dc.subjectFunctionally graded material
dc.subject.classificationEngineering, Multidisciplinary
dc.subject.classificationMaterials Science, Composites
dc.subject.classificationEngineering
dc.subject.classificationMaterials Science
dc.subject.otherBuckling
dc.subject.otherCeramic materials
dc.subject.otherComposite beams and girders
dc.subject.otherDegrees of freedom (mechanics)
dc.subject.otherEquations of motion
dc.subject.otherFunctionally graded materials
dc.subject.otherPlates (structural components)
dc.subject.otherSandwich structures
dc.subject.otherShear deformation
dc.subject.otherVibration analysis
dc.subject.otherBuckling analysis
dc.subject.otherDifferent boundary condition
dc.subject.otherFirst-order shear deformation theory
dc.subject.otherFree vibration
dc.subject.otherFunctionally graded
dc.subject.otherHomogeneous ceramics
dc.subject.otherLagrange's equation
dc.subject.otherStability analysis
dc.subject.otherFinite element method
dc.titleVibration and stability analysis of functionally graded sandwich beams by a multi-layer finite element
dc.typeArticle
rdl.citation.openalex81
rdl.citation.scopus89
rdl.citation.wos81
rdl.oa.statusclosed
rdl.scopus.quartileQ1
rdl.source.indexSCOPUS
rdl.source.indexWOS
rdl.wos.indexScience Citation Index Expanded (SCI-EXPANDED)