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Aerodynamic Optimization of a UAV Wing subject to Weight, Geometric, Root Bending Moment, and Performance Constraints

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dc.contributor.authorKorpe, DS
dc.contributor.authorKanat, OO
dc.date.accessioned2023-04-18T02:56:45Z
dc.date.available2023-04-18T02:56:45Z
dc.date.issued2019.01.01
dc.identifier.doi10.1155/2019/3050824
dc.identifier.eissn1687-5974
dc.identifier.endpage
dc.identifier.issn1687-5966
dc.identifier.issue
dc.identifier.startpage
dc.identifier.urihttps://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=dspace_ku&SrcAuth=WosAPI&KeyUT=WOS:000493095700001&DestLinkType=FullRecord&DestApp=WOS
dc.identifier.urihttps://hdl.handle.net/20.500.12597/10275
dc.identifier.volume2019
dc.identifier.wosWOS:000493095700001
dc.relation.ispartofINTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING
dc.titleAerodynamic Optimization of a UAV Wing subject to Weight, Geometric, Root Bending Moment, and Performance Constraints
dc.typeArticle
dspace.entity.typeWos
relation.isPublicationOfWos996212fd-6a6c-4418-b2fa-acc26d351ad0
relation.isPublicationOfWos.latestForDiscovery996212fd-6a6c-4418-b2fa-acc26d351ad0

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