Aeroelastic analysis of turboprop commuter aircraft with tip-tanks

dc.contributor.authorČečrdle, J.
dc.contributor.authorVích, O.
dc.contributor.editorAdámek, Vítězslav
dc.contributor.editorJonášová, Alena
dc.contributor.editorPlánička, Stanislav
dc.contributor.editorZajíček, Martin
dc.date.accessioned2019-01-16T06:20:41Z
dc.date.available2019-01-16T06:20:41Z
dc.date.issued2018
dc.description.abstract-translatedThis paper deals with aeroelastic (flutter) analysis of an aircraft with unconventional wing structure, which is specific by the installation of wing-tip tanks. The subjected aircraft is twin wing-mounted tractor turboprop commuter aircraft for 19 passengers, with a wingspan of 9.6 m and a maximal take-off weight of 7000 kg. The paper is focused on the assessment of specific flutter issue, originating from the unconventional wing configuration. Further, another flutter issues related to elevator flutter and rudder flutter are described.en
dc.format2 s.cs
dc.format.mimetypeapplication/pdf
dc.identifier.citationComputational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 7-8.en
dc.identifier.isbn978-80-261-0819-1
dc.identifier.urihttp://hdl.handle.net/11025/30781
dc.language.isoenen
dc.publisherZápadočeská univerzita v Plznics
dc.relation.ispartofseriesComputational Mechanicsen
dc.rightsCopyright © 2018 University of West Bohemia, Plzeň, Czech Republicen
dc.rights.accessopenAccessen
dc.subjectaeroelastická analýzacs
dc.subjectturbovrtulové dopravní letadlocs
dc.subjectkřídlové nádržecs
dc.subject.translatedaeroelastic analysisen
dc.subject.translatedturboprop commuter aircraften
dc.subject.translatedwing-tip tanksen
dc.titleAeroelastic analysis of turboprop commuter aircraft with tip-tanksen
dc.typekonferenční příspěvekcs
dc.typeconferenceObjecten
dc.type.statusPeer-revieweden
dc.type.versionpublishedVersionen

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