Please use this identifier to cite or link to this item: https://hdl.handle.net/11147/10354
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dc.contributor.authorAkçaır, Mehmet-
dc.contributor.authorSavran, Melih-
dc.contributor.authorAydın, Levent-
dc.contributor.authorAyakdaş, Ozan-
dc.contributor.authorÖztürk, Savaş-
dc.contributor.authorKüçükdoğan, Nilay-
dc.date.accessioned2021-01-24T18:34:07Z-
dc.date.available2021-01-24T18:34:07Z-
dc.date.issued2019-
dc.identifier.issn2148-9807-
dc.identifier.issn2149-4088-
dc.identifier.urihttps://doi.org/10.17515/resm2019.66is0909-
dc.identifier.urihttps://hdl.handle.net/11147/10354-
dc.identifier.urihttps://search.trdizin.gov.tr/yayin/detay/347783-
dc.description.abstractStacking sequence design and optimization of 64 layered symmetric-balance graphite/epoxy laminated composite have been performed. The optimization problems aim to find the optimum stacking sequence maximizing the critical buckling load by single objective optimization approach. Differential Evolution (DE) and Simulated Annealing (SA) optimization algorithms are proposed to solve the problems. The effect of the aspect ratios (a/b) and in-plane biaxial compressive loading ratios (Nx/Ny) on critical buckling load are investigated. In order to see the effect of discrete increments of fiber orientation angle on critical buckling load, 1°, 5°, 15°, 30° and 45° fiber angle increments are also considered. The results show that (i) the proposed algorithms DE and SA exhibit comparable performance in terms of critical buckling load when compared Genetic algorithm (GA) and Generalized pattern search algorithm (GPSA), (ii) DE and SA find distinct stacking sequence configurations in terms of buckling load for the same laminated structure design problems.en_US
dc.language.isoenen_US
dc.publisherMIM Research Groupen_US
dc.relation.ispartofResearch on Engineering Structures and Materialsen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectLaminated compositeen_US
dc.subjectStochastic optimizationen_US
dc.subjectBucklingen_US
dc.titleOptimum design of anti-buckling behavior of graphite/epoxy laminated composites by differential evolution and simulated annealing methoden_US
dc.typeArticleen_US
dc.institutionauthorAyakdaş, Ozan-
dc.departmentİzmir Institute of Technology. Mechanical Engineeringen_US
dc.identifier.volume5en_US
dc.identifier.issue2en_US
dc.identifier.startpage175 - 188en_US
dc.relation.publicationcategoryMakale - Ulusal Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.identifier.doi10.17515/resm2019.66is0909-
dc.relation.doi10.17515/resm2019.66is0909en_US
dc.coverage.doi10.17515/resm2019.66is0909en_US
dc.identifier.trdizinid347783en_US
dc.identifier.wosqualityN/A-
dc.identifier.scopusqualityQ3-
item.fulltextWith Fulltext-
item.grantfulltextopen-
item.languageiso639-1en-
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.cerifentitytypePublications-
item.openairetypeArticle-
Appears in Collections:Mechanical Engineering / Makina Mühendisliği
TR Dizin İndeksli Yayınlar / TR Dizin Indexed Publications Collection
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