Please use this identifier to cite or link to this item: https://hdl.handle.net/11147/4228
Full metadata record
DC FieldValueLanguage
dc.contributor.advisorArtem, Hatice Seçil-
dc.contributor.authorBoyacı, Hakan-
dc.date.accessioned2014-12-04T08:49:30Z-
dc.date.available2014-12-04T08:49:30Z-
dc.date.issued2014-03-
dc.identifier.urihttp://hdl.handle.net/11147/4228-
dc.descriptionThesis (Master)--Izmir Institute of Technology, Mechanical Engineering, Izmir, 2014en_US
dc.descriptionIncludes bibliographical references(leaves: 62-64)en_US
dc.descriptionText in English; Abstract: Turkish and Englishen_US
dc.descriptionFull text release delayed at author's request until 2016.04.17en
dc.description.abstractComposite materials have been increasingly used during the last decades due to their properties such as low weight, high stiffness, superior fatigue and corrosion resistance. They have been used in aerospace, automobile, marine applications and etc. Composite materials being an expensive but efficient technology to get minimum weight structures, it is logical to make an attempt to find out how to design properly optimum laminated composite plates with no reduction in their strength. The aim of the thesis is to find the optimum stacking sequence to obtain the minimum thickness (weight) of laminated composite plates in different loadings and plate dimensions under buckling constraint. Moreover, a comparison study of conventional and continuous designs are performed to determine the effect of stacking sequence on weight. The objective function is the critical buckling load factor. Fiber angles of the composite plates are taken as continuous design variables and the plate is assumed to be balance and symmetric. Composite plates made of graphite/epoxy have been considered in this thesis. A combination of Generalized Pattern Search Algorithm (GPSA) and Genetic Algorithm (GA) has been considered as an optimization method. All the results show that the loading conditions and dimensions of composite plates are significant in stacking sequences optimization of laminated composite materials in terms of maximum critical buckling load factor and minimum thickness.en_US
dc.language.isoenen_US
dc.publisherIzmir Institute of Technologyen_US
dc.rightsinfo:eu-repo/semantics/openAccessen_US
dc.subjectAlgorithmsen_US
dc.subjectGeneralized Pattern Search Algorithmen_US
dc.subject.lcshComposite materialsen_US
dc.subject.lcshLaminated materials--Mechanical propertiesen_US
dc.titleStacking sequence optimization of the anti-buckled graphite/epoxy laminated composites for minimum weight using generalized pattern search algorithmen_US
dc.title.alternativeGenelleştirilmiş model arama algoritması kullanılarak burkulmayan tabakalı grafit/epoksi kompozitlerin minimum ağırlık için tabaka dizilimlerinin optimizasyonuen_US
dc.typeMaster Thesisen_US
dc.institutionauthorBoyacı, Hakan-
dc.departmentIzmir Institute of Technology. Mechanical Engineeringen_US
dc.relation.publicationcategoryTezen_US
item.openairecristypehttp://purl.org/coar/resource_type/c_18cf-
item.openairetypeMaster Thesis-
item.grantfulltextopen-
item.fulltextWith Fulltext-
item.cerifentitytypePublications-
item.languageiso639-1en-
Appears in Collections:Master Degree / Yüksek Lisans Tezleri
Files in This Item:
File Description SizeFormat 
10013551.pdfMasterThesis1.75 MBAdobe PDFThumbnail
View/Open
Show simple item record

CORE Recommender

Page view(s)

102
checked on Nov 21, 2022

Download(s)

28
checked on Nov 21, 2022

Google ScholarTM

Check


Items in GCRIS Repository are protected by copyright, with all rights reserved, unless otherwise indicated.