Show simple item record

Optimal Topology of Aircraft Rib and Spar Structures Under Aeroelastic Loads

dc.contributor.authorStanford, Bret K.
dc.contributor.authorDunning, Peter D.
dc.date.accessioned2016-01-29T14:44:03Z
dc.date.available2016-01-29T14:44:03Z
dc.date.issued2015-07
dc.identifier.citationStanford , B K & Dunning , P D 2015 , ' Optimal Topology of Aircraft Rib and Spar Structures Under Aeroelastic Loads ' , Journal of Aircraft , vol. 52 , no. 4 , pp. 1298-1311 . https://doi.org/10.2514/1.C032913en
dc.identifier.issn0021-8669
dc.identifier.otherPURE: 56462797
dc.identifier.otherPURE UUID: 86165309-645d-437f-b263-7cbb17943d56
dc.identifier.otherRIS: urn:BD4D736D66C8814D9136B171826A24B0
dc.identifier.otherScopus: 84945955805
dc.identifier.otherORCID: /0000-0002-7645-7598/work/26019353
dc.identifier.urihttp://hdl.handle.net/2164/5460
dc.descriptionThis work is funded by the Fixed Wing Project under NASA’s Fundamental Aeronautics Program.en
dc.format.extent14
dc.language.isoeng
dc.relation.ispartofJournal of Aircraften
dc.rights©2015 AIAAen
dc.subjectTL Motor vehicles. Aeronautics. Astronauticsen
dc.subject.lccTLen
dc.titleOptimal Topology of Aircraft Rib and Spar Structures Under Aeroelastic Loadsen
dc.typeJournal articleen
dc.contributor.institutionUniversity of Aberdeen.Engineeringen
dc.description.statusPeer revieweden
dc.description.versionPostprinten
dc.identifier.doihttps://doi.org/10.2514/1.C032913
dc.identifier.vol52en
dc.identifier.iss4en


Files in this item

Thumbnail
Name:
Bret_Stanford_AIAAJ_2014_topol ...
Size:
12.69Mb
Format:
PDF
View/Open

This item appears in the following Collection(s)

Show simple item record