Parallelized structural topology optimization and CFD coupling for design of aircraft wing structures

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dc.authoridAkay, Hasan U/0000-0003-2574-9942
dc.authorscopusid6701403522
dc.authorscopusid24532717000
dc.authorscopusid36806467100
dc.authorwosidAkay, Hasan U/ABI-3992-2020
dc.contributor.authorOktay, E.
dc.contributor.authorAkay, H. U.
dc.contributor.authorMerttopcuoglu, O.
dc.contributor.otherAutomotive Engineering
dc.date.accessioned2024-07-05T15:10:36Z
dc.date.available2024-07-05T15:10:36Z
dc.date.issued2011
dc.departmentAtılım Universityen_US
dc.department-temp[Akay, H. U.] Atilim Univ, Dept Mech Engn, Ankara, Turkey; [Oktay, E.] EDA Engn Design & Anal Ltd, Ankara, Turkey; [Merttopcuoglu, O.] Roketsan, Ankara, Turkeyen_US
dc.descriptionAkay, Hasan U/0000-0003-2574-9942en_US
dc.description.abstractA set of structural optimization tools are presented for topology optimization of aircraft wing structures coupled with Computational Fluid Dynamics (CFD) analyses. The topology optimization tool used for design is the material distribution technique. Because reducing the weight requires numerous calculations, the CFD and structural optimization codes are parallelized and coupled via a code/mesh coupling scheme. In this study, the algorithms used and the results obtained are presented for topology design of a wing cross-section under a given critical aerodynamic loading and two different spar positions to determine the optimum rib topology. (C) 2011 Elsevier Ltd. All rights reserved.en_US
dc.identifier.citation44
dc.identifier.doi10.1016/j.compfluid.2011.05.005
dc.identifier.endpage145en_US
dc.identifier.issn0045-7930
dc.identifier.issn1879-0747
dc.identifier.issue1en_US
dc.identifier.scopus2-s2.0-79960893593
dc.identifier.startpage141en_US
dc.identifier.urihttps://doi.org/10.1016/j.compfluid.2011.05.005
dc.identifier.urihttps://hdl.handle.net/20.500.14411/1341
dc.identifier.volume49en_US
dc.identifier.wosWOS:000293941100012
dc.identifier.wosqualityQ2
dc.institutionauthorAkay, Hasan Umur
dc.language.isoenen_US
dc.publisherPergamon-elsevier Science Ltden_US
dc.relation.ispartof22nd International Conference on Parallel Computational Fluid Dynamics (ParCFD) -- APR 30-30, 2010 -- Kaohsiung, TAIWANen_US
dc.relation.publicationcategoryKonferans Öğesi - Uluslararası - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectStructural topology optimizationen_US
dc.subjectAircraft structural analysisen_US
dc.subjectParallel CFDen_US
dc.subjectMesh couplingen_US
dc.subjectCode couplingen_US
dc.subjectParallelized solversen_US
dc.titleParallelized structural topology optimization and CFD coupling for design of aircraft wing structuresen_US
dc.typeConference Objecten_US
dspace.entity.typePublication
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relation.isAuthorOfPublication.latestForDiscovery94f6c6fc-365d-4875-b446-2ad82c1cc745
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relation.isOrgUnitOfPublication.latestForDiscovery7d024e9b-1f00-4f1d-a95a-f448a474eea9

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