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.identifier56462797
dc.identifier86165309-645d-437f-b263-7cbb17943d56
dc.identifier84945955805
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.otherRIS: urn:BD4D736D66C8814D9136B171826A24B0
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.format.extent13311479
dc.language.isoeng
dc.relation.ispartofJournal of Aircraften
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.identifier.doi10.2514/1.C032913


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