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Optimum design of shell structures with stiffening beams

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dc.contributor.author Lagaros, ND en
dc.contributor.author Fragiadakis, M en
dc.contributor.author Papadrakakis, M en
dc.date.accessioned 2014-03-01T01:21:11Z
dc.date.available 2014-03-01T01:21:11Z
dc.date.issued 2004 en
dc.identifier.issn 0001-1452 en
dc.identifier.uri https://dspace.lib.ntua.gr/xmlui/handle/123456789/16127
dc.relation.uri http://www.scopus.com/inward/record.url?eid=2-s2.0-0842268581&partnerID=40&md5=f4cff238334c968c3144c5b24cf48d39 en
dc.subject.classification Engineering, Aerospace en
dc.subject.other Evolutionary algorithms en
dc.subject.other Optimization en
dc.subject.other Structural design en
dc.subject.other Topology en
dc.subject.other Beam composites en
dc.subject.other Eurocode en
dc.subject.other Natural mode triangular composites en
dc.subject.other Shell structures en
dc.subject.other Stiffening beams en
dc.subject.other Shells (structures) en
dc.title Optimum design of shell structures with stiffening beams en
heal.type journalArticle en
heal.language English en
heal.publicationDate 2004 en
heal.abstract The optimum design of stiffened shell structures is investigated using a robust and efficient optimization algorithm where the total weight of the structure is to be minimized subject to behavioral constraints imposed by structural design codes. Evolutionary algorithms and more specifically the evolution strategies (ES) method specially tailored for this type of problems is implemented for the solution of the structural optimization problem. The discretization of the stiffened shell is performed by means of cost-effective and reliable shell and beam elements that incorporate the natural mode concept. Three types of design variables are considered: sizing, shape, and topology. A benchmark test example is examined where the efficiency and robustness of ES over other optimization methods is investigated. Two case studies of stiffened shells are subsequently presented, where a parametric study is undertaken to obtain the most efficient design compatible with the regulations suggested by design codes such as Eurocode. The important role of the stiffeners and how they can be optimally chosen to improve the performance of shell structures in terms of carrying capacity and economy is demonstrated. en
heal.publisher AMER INST AERONAUT ASTRONAUT en
heal.journalName AIAA Journal en
dc.identifier.isi ISI:000188248000019 en
dc.identifier.volume 42 en
dc.identifier.issue 1 en
dc.identifier.spage 175 en
dc.identifier.epage 184 en


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