Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.14279/1616
DC FieldValueLanguage
dc.contributor.authorSaha, Gobinda-
dc.contributor.authorKalamkarov, Alexander L.-
dc.contributor.authorGeorgiades, Tasos-
dc.date.accessioned2013-03-06T16:24:40Zen
dc.date.accessioned2013-05-17T05:22:41Z-
dc.date.accessioned2015-12-02T10:01:55Z-
dc.date.available2013-03-06T16:24:40Zen
dc.date.available2013-05-17T05:22:41Z-
dc.date.available2015-12-02T10:01:55Z-
dc.date.issued2007-06-
dc.identifier.citationComposites Part A: Applied Science and Manufacturing, 2007, vol. 38, no. 6, pp.1533-1546.en_US
dc.identifier.issn1359835X-
dc.identifier.urihttps://hdl.handle.net/20.500.14279/1616-
dc.description.abstractThis paper works on the analytical development of the method of two-scale asymptotic homogenization. The technique is used to determine the effective elastic stiffnesses of hexagonal honeycomb-cored structural sandwich composite shells made of generally orthotropic materials. Orthotropy of the constituent materials leads to much more complex unit-cell problems and is considered in the present paper for the first time. At first, a 3D-to-2D general shell model based on a set of unit-cell problems is derived. This is followed by the exploitation of the model to the derivation of analytical estimate formulae; used to calculate the force and moment resultants present in the sandwich shell structure. The implication of the general shell model is further indicated by calculating similar design characteristics for a three-layered composite sandwich panel reinforced with hexagonal and triangular shaped cellular core made from the generally orthotropic material.en_US
dc.formatpdfen_US
dc.language.isoenen_US
dc.relation.ispartofComposites Part A: Applied Science and Manufacturingen_US
dc.rights© Elsevieren_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/3.0/us/*
dc.subjectMicromechanicsen_US
dc.subjectHoneycomb structuresen_US
dc.subjectElasticityen_US
dc.titleEffective elastic characteristics of honeycomb sandwich composite shells made of generally orthotropic materialsen_US
dc.typeArticleen_US
dc.affiliationDalhousie Universityen
dc.collaborationDalhousie Universityen_US
dc.journalsOpen Accessen_US
dc.countryCanadaen_US
dc.subject.fieldEngineering and Technologyen_US
dc.publicationPeer Revieweden_US
dc.identifier.doi10.1016/j.compositesa.2007.01.002en_US
dc.dept.handle123456789/54en
dc.relation.issue6en_US
dc.relation.volume38en_US
cut.common.academicyear2007-2008en_US
dc.identifier.spage1533en_US
dc.identifier.epage1546en_US
item.fulltextNo Fulltext-
item.cerifentitytypePublications-
item.grantfulltextnone-
item.openairecristypehttp://purl.org/coar/resource_type/c_6501-
item.openairetypearticle-
item.languageiso639-1en-
crisitem.journal.journalissn1359-835X-
crisitem.journal.publisherElsevier-
crisitem.author.deptDepartment of Mechanical Engineering and Materials Science and Engineering-
crisitem.author.facultyFaculty of Engineering and Technology-
crisitem.author.orcid0000-0002-8984-1011-
crisitem.author.parentorgFaculty of Engineering and Technology-
Appears in Collections:Άρθρα/Articles
CORE Recommender
Show simple item record

SCOPUSTM   
Citations

35
checked on Nov 9, 2023

WEB OF SCIENCETM
Citations

35
Last Week
0
Last month
1
checked on Oct 29, 2023

Page view(s)

542
Last Week
2
Last month
9
checked on May 17, 2024

Google ScholarTM

Check

Altmetric


This item is licensed under a Creative Commons License Creative Commons