Web of Science:
Maximum lift/drag ratio improvement of TUAVs via small aerodynamic modifications

dc.contributor.authorOktay, T
dc.contributor.authorUzun, M
dc.contributor.authorKanat, OO
dc.date.accessioned2023-04-18T02:42:29Z
dc.date.available2023-04-18T02:42:29Z
dc.date.issued2018.01.01
dc.identifier.doi10.1108/AEAT-07-2017-0175
dc.identifier.eissn1758-4213
dc.identifier.endpage1444
dc.identifier.issn1748-8842
dc.identifier.issue9
dc.identifier.startpage1438
dc.identifier.urihttps://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=dspace_ku&SrcAuth=WosAPI&KeyUT=WOS:000450861500015&DestLinkType=FullRecord&DestApp=WOS
dc.identifier.urihttps://hdl.handle.net/20.500.12597/9953
dc.identifier.volume90
dc.identifier.wosWOS:000450861500015
dc.relation.ispartofAIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
dc.titleMaximum lift/drag ratio improvement of TUAVs via small aerodynamic modifications
dc.typeArticle
dspace.entity.typeWos
relation.isPublicationOfWos62593d40-b8e0-40f4-acb6-1cff6a8bf962
relation.isPublicationOfWos.latestForDiscovery62593d40-b8e0-40f4-acb6-1cff6a8bf962

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