Gümüşhane ÜniversitesiGümüşhane ÜniversitesiAçık Erişim Arşivi · RDL Open

Thermal buckling load optimization of laminated composite plates

MakaleYalnız künye

Özet

In this study, the applicability of the Modified Feasible Direction (MFD) method on the thermal buckling optimization of laminated plates subjected to uniformly distributed temperature load is investigated. The objective function is to maximize the critical temperature capacity of laminated plates and the fiber orientation is considered as design variable. The first-order shear deformation theory is used in the mathematical formulation. For this purpose, a program based on FORTRAN is used for the optimization of laminated plates. Finally, the effect of aspect ratio, antisymmetric lay-up, boundary condition, material anisotropy, ratio of coefficients of thermal expansion, and hybrid laminates on the results is investigated and the results are compared.

Anahtar Kelimeler

Laminated composite platesModified Feasible Direction methodOptimal designsThermal buckling
RDL Kalıcı Bağlantı (PID)
https://rdlopen.rawdatalibrary.net/r/gumushane/14156Resmi atıflarda kullanılan kalıcı adres
DOI
https://doi.org/10.1016/j.tws.2007.11.005Yayıncı resmi DOI adresi
Tam Kayıt
AlanDeğerDil
dc.contributor.authorTopal, U.
dc.contributor.authorUzman, Ü.
dc.date.accessioned2026-10-22T10:22:19.346992380Z
dc.date.available2026-10-22T10:22:19.346992380Z
dc.date.issued2008
dc.description.abstractIn this study, the applicability of the Modified Feasible Direction (MFD) method on the thermal buckling optimization of laminated plates subjected to uniformly distributed temperature load is investigated. The objective function is to maximize the critical temperature capacity of laminated plates and the fiber orientation is considered as design variable. The first-order shear deformation theory is used in the mathematical formulation. For this purpose, a program based on FORTRAN is used for the optimization of laminated plates. Finally, the effect of aspect ratio, antisymmetric lay-up, boundary condition, material anisotropy, ratio of coefficients of thermal expansion, and hybrid laminates on the results is investigated and the results are compared.
dc.identifier.doi10.1016/j.tws.2007.11.005
dc.identifier.endpage675
dc.identifier.issn0263-8231
dc.identifier.issue6
dc.identifier.scopus2-s2.0-42649128035
dc.identifier.startpage667
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/gumushane/14156
dc.identifier.volume46
dc.language.isoen
dc.relation.ispartofThin-Walled Structures
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.subjectLaminated composite plates
dc.subjectModified Feasible Direction method
dc.subjectOptimal designs
dc.subjectThermal buckling
dc.subject.otherBoundary conditions
dc.subject.otherBuckling
dc.subject.otherLaminated composites
dc.subject.otherOptimization
dc.subject.otherThermal effects
dc.subject.otherModified Feasible Direction (MFD)
dc.subject.otherThermal buckling
dc.subject.otherPlates (structural components)
dc.titleThermal buckling load optimization of laminated composite plates
dc.typeArticle
dspace.entity.typePublication
rdl.citation.openalex67
rdl.citation.scopus67
rdl.oa.statusclosed
rdl.source.indexSCOPUS