Effect of rectangular/circular cutouts on thermal buckling load optimization of angle-ply laminated thin plates

MakaleAçık Erişim

Özet

This paper deals with thermal buckling load optimization of symmetrically laminated angle-ply thin plates with centrally located different cutouts subjected to a uniform temperature load rise. The optimum results are given for maximum buckling temperature and the fibre orientation is adopted as design variable. The results are obtained for the various cutout geometries such as rectangle and circle. The modified feasible direction (MFD) method is used for the optimization routine. Therefore a program based on FORTRAN is used. Finally, the effects of cutout areas, plate aspect ratios and boundary conditions on the optimum results are demonstrated.

Anahtar Kelimeler

RDL Kalıcı Bağlantı (PID)
https://rdlopen.rawdatalibrary.net/r/gumushane/13117Resmi atıflarda kullanılan kalıcı adres
DOI
https://doi.org/10.1515/secm.2010.17.2.93Yayıncı resmi DOI adresi
İndeks kayıtları
Kaydın indeks veri tabanlarındaki sayfası (aktarımda alınan kayıt numarasıyla). Erişim, indeksin kendi koşullarına bağlıdır.
Atıflar
Scopus
6
WoS
4
OpenAlex
5
Her kaynağın kendi saydığı toplam atıf; aktarım ve zenginleştirme sırasında alındı.
Tam Kayıt
AlanDeğerDil
dc.contributor.authorTopal, Umut
dc.contributor.authorUzman, Ümit
dc.date.accessioned2026-10-22T10:20:56.970853199Z
dc.date.available2026-10-22T10:20:56.970853199Z
dc.date.issued2010
dc.description.abstractThis paper deals with thermal buckling load optimization of symmetrically laminated angle-ply thin plates with centrally located different cutouts subjected to a uniform temperature load rise. The optimum results are given for maximum buckling temperature and the fibre orientation is adopted as design variable. The results are obtained for the various cutout geometries such as rectangle and circle. The modified feasible direction (MFD) method is used for the optimization routine. Therefore a program based on FORTRAN is used. Finally, the effects of cutout areas, plate aspect ratios and boundary conditions on the optimum results are demonstrated.
dc.identifier.doi10.1515/secm.2010.17.2.93
dc.identifier.endpage110
dc.identifier.issn0334-181X
dc.identifier.issue2
dc.identifier.scopus2-s2.0-79952907152
dc.identifier.startpage91
dc.identifier.urihttps://rdlopen.rawdatalibrary.net/r/gumushane/13117
dc.identifier.volume17
dc.identifier.wosWOS:000282931300002
dc.language.isoen
dc.publisherWalter de Gruyter GmbH
dc.relation.ispartofScience and Engineering of Composite Materials
dc.rightsinfo:eu-repo/semantics/openAccess
dc.subjectCutouts
dc.subjectLaminated composite plates
dc.subjectModified feasible direction method
dc.subjectOptimal design
dc.subjectThermal buckling
dc.subject.classificationMaterials Science, Composites
dc.subject.classificationMaterials Science
dc.subject.otherAspect ratio
dc.subject.otherGeometry
dc.subject.otherLaminated composites
dc.subject.otherLaminating
dc.subject.otherCutouts
dc.subject.otherLaminated composite plates
dc.subject.otherModified feasible direction method
dc.subject.otherOptimal design
dc.subject.otherThermal buckling
dc.subject.otherBuckling
dc.titleEffect of rectangular/circular cutouts on thermal buckling load optimization of angle-ply laminated thin plates
dc.typeArticle
rdl.citation.openalex5
rdl.citation.scopus6
rdl.citation.wos4
rdl.oa.statushybrid
rdl.oa.statusclosed
rdl.oa.urlhttps://www.degruyter.com/document/doi/10.1515/SECM.2010.17.2.93/pdf
rdl.source.indexSCOPUS
rdl.source.indexWOS
rdl.wos.indexScience Citation Index Expanded (SCI-EXPANDED)