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dc.contributor.authorPecka, A.
dc.contributor.authorBublík, O.
dc.contributor.authorVimmr, J.
dc.contributor.editorAdámek, Vítězslav
dc.contributor.editorJonášová, Alena
dc.contributor.editorPlánička, Stanislav
dc.contributor.editorZajíček, Martin
dc.date.accessioned2019-01-17T11:54:36Z-
dc.date.available2019-01-17T11:54:36Z-
dc.date.issued2018
dc.identifier.citationComputational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 83-84.en
dc.identifier.isbn978-80-261-0819-1
dc.identifier.urihttp://hdl.handle.net/11025/30819
dc.identifier.urihttps://www.zcu.cz/export/sites/zcu/pracoviste/vyd/online/FAV_Computational_Mechanics_2018.pdf
dc.description.sponsorshipThe authors appreciate the kind support of the grant GA 16-04546S Aero-elastic couplings and dynamic behaviour of rotational periodic bodies´ of the Czech Science Foundation and of the student grant project SGS-2016-038.en
dc.format2 s.cs
dc.format.mimetypeapplication/pdf
dc.language.isoenen
dc.publisherZápadočeská univerzita v Plznics
dc.relation.ispartofseriesComputational Mechanicsen
dc.rightsCopyright © 2018 University of West Bohemia, Plzeň, Czech Republicen
dc.subjecttřepetající se hranicecs
dc.subjectinterakce struktura tekutinacs
dc.subjectaeroelastická analýzacs
dc.subjectFlowProcs
dc.subjectGalerkinův kódcs
dc.titleFlutter boundary assessment for a blade cascade using developed discontinuous Galerkin codeen
dc.typekonferenční příspěvekcs
dc.typeconferenceObjecten
dc.rights.accessopenAccessen
dc.type.versionpublishedVersionen
dc.description.abstract-translatedThis contribution builds on the last year contribution, where the flutter boundary was assessed for a single aerofoil with the aid of the fluid-structure interaction (FSI) code developed for the purpose of aeroelastic flutter analysis as a part of FlowPro. FlowPro is a multipurpose numerical software developed by the authors of this contribution. Flutter boundary established in was compared with the results of Kirshmann and Hall. Since the results agreed reasonably well to say the least, the FSI code is now considered as validated. The aim of this contribution is to establish the flutter boundary for a blade cascade.en
dc.subject.translatedflutter boundaryen
dc.subject.translatedfluid-structure interactionen
dc.subject.translatedaeroelastic analysisen
dc.subject.translatedFlowProen
dc.subject.translatedGalerkin codeen
dc.type.statusPeer-revieweden
Appears in Collections:Konferenční příspěvky / Conference papers (NTIS)
Konferenční příspěvky / Conference Papers (KME)
Computational mechanics 2018
Computational mechanics 2018

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