Optimal Topology of Aircraft Rib and Spar Structures Under Aeroelastic Loads

dc.contributor.author	Stanford, Bret K.
dc.contributor.author	Dunning, Peter D.
dc.contributor.institution	University of Aberdeen.Engineering	en
dc.date.accessioned	2016-01-29T14:44:03Z
dc.date.available	2016-01-29T14:44:03Z
dc.date.issued	2015-07
dc.description	This work is funded by the Fixed Wing Project under NASA’s Fundamental Aeronautics Program.	en
dc.description.status	Peer reviewed	en
dc.format.extent	14
dc.format.extent	13311479
dc.identifier	56462797
dc.identifier	86165309-645d-437f-b263-7cbb17943d56
dc.identifier	84945955805
dc.identifier.citation	Stanford, 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.C032913	en
dc.identifier.doi	10.2514/1.C032913
dc.identifier.iss	4	en
dc.identifier.issn	0021-8669
dc.identifier.other	RIS: urn:BD4D736D66C8814D9136B171826A24B0
dc.identifier.other	ORCID: /0000-0002-7645-7598/work/26019353
dc.identifier.uri	http://hdl.handle.net/2164/5460
dc.identifier.vol	52	en
dc.language.iso	eng
dc.relation.ispartof	Journal of Aircraft	en
dc.subject	TL Motor vehicles. Aeronautics. Astronautics	en
dc.subject.lcc	TL	en
dc.title	Optimal Topology of Aircraft Rib and Spar Structures Under Aeroelastic Loads	en
dc.type	Journal article	en

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