Thermal buckling load optimization of laminated skew plates

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Özet

In this study thermal buckling load optimization of laminated skew plates subjected to uniformly distributed temperature load is investigated. All of the laminates considered are assumed to have fully clamped boundary conditions, though the general boundary conditions may also be studied without any difficulty. The objective function is to maximize the critical temperature capacity of the laminated skew plates and the fibre orientation is considered as design variable. The first-order shear deformation theory is used in the mathematical formulation. Nine-node Lagrangian rectangular plate element is used for the finite element solution of the skew laminates. The temperature field is assumed to be uniform over the plate surface and varies in the thickness direction only. Modified feasible direction method (MFD) is used for the optimization routine. A program based on FORTRAN is used for the optimization problem. Finally, the effect of number of layers, skew angles, aspect ratios, width-to-thickness ratios and antisymmetric lay-up on the optimal designs is investigated and the results are compared.

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RDL Kalıcı Bağlantı (PID)
https://rdlopen.rawdatalibrary.net/r/gumushane/14040Resmi atıflarda kullanılan kalıcı adres
Tam Kayıt
AlanDeğerDil
dc.contributor.authorTopal, U.
dc.contributor.authorUzman, Ü.
dc.date.accessioned2026-10-22T10:22:08.621921480Z
dc.date.available2026-10-22T10:22:08.621921480Z
dc.date.issued2009
dc.description.abstractIn this study thermal buckling load optimization of laminated skew plates subjected to uniformly distributed temperature load is investigated. All of the laminates considered are assumed to have fully clamped boundary conditions, though the general boundary conditions may also be studied without any difficulty. The objective function is to maximize the critical temperature capacity of the laminated skew plates and the fibre orientation is considered as design variable. The first-order shear deformation theory is used in the mathematical formulation. Nine-node Lagrangian rectangular plate element is used for the finite element solution of the skew laminates. The temperature field is assumed to be uniform over the plate surface and varies in the thickness direction only. Modified feasible direction method (MFD) is used for the optimization routine. A program based on FORTRAN is used for the optimization problem. Finally, the effect of number of layers, skew angles, aspect ratios, width-to-thickness ratios and antisymmetric lay-up on the optimal designs is investigated and the results are compared.
dc.identifier.doi10.1016/j.matdes.2008.09.025
dc.identifier.eissn1873-4197
dc.identifier.endpage2575
dc.identifier.issn0264-1275
dc.identifier.issue7
dc.identifier.scopus2-s2.0-67349286795
dc.identifier.startpage2569
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/gumushane/14040
dc.identifier.volume30
dc.identifier.wosWOS:000266784700038
dc.language.isoen
dc.publisherELSEVIER SCI LTD
dc.relation.ispartofMaterials and Design
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectB. Laminates
dc.subjectE. Mechanical
dc.subject.classificationMaterials Science, Multidisciplinary
dc.subject.classificationMaterials Science
dc.subject.otherAspect ratio
dc.subject.otherBoundary conditions
dc.subject.otherBuckling
dc.subject.otherElectric load management
dc.subject.otherLaminates
dc.subject.otherLaminating
dc.subject.otherOptimization
dc.subject.otherShear deformation
dc.subject.otherAnti-symmetric
dc.subject.otherB. Laminates
dc.subject.otherCritical temperatures
dc.subject.otherDesign variables
dc.subject.otherE. Mechanical
dc.subject.otherFibre orientations
dc.subject.otherFinite element solutions
dc.subject.otherFirst-order shear deformation theories
dc.subject.otherFortrans
dc.subject.otherFully clamped boundaries
dc.subject.otherGeneral boundary conditions
dc.subject.otherLagrangian
dc.subject.otherMathematical formulations
dc.subject.otherModified feasible direction methods
dc.subject.otherNumber of layers
dc.subject.otherObjective functions
dc.subject.otherOptimal designs
dc.subject.otherOptimization problems
dc.subject.otherOptimization routines
dc.subject.otherPlate surfaces
dc.subject.otherRectangular plates
dc.subject.otherSkew angles
dc.subject.otherSkew plates
dc.subject.otherTemperature fields
dc.subject.otherTemperature loads
dc.subject.otherThermal buckling
dc.subject.otherThickness directions
dc.subject.otherWidth-to-thickness ratios
dc.subject.otherPlates (structural components)
dc.titleThermal buckling load optimization of laminated skew plates
dc.typeArticle
dspace.entity.typePublication
rdl.citation.openalex11
rdl.citation.scopus10
rdl.citation.wos11
rdl.oa.statusclosed
rdl.source.indexSCOPUS
rdl.source.indexWOS
rdl.wos.indexScience Citation Index Expanded (SCI-EXPANDED)