Title: Flutter boundary assessment for a blade cascade using developed discontinuous Galerkin code
Authors: Pecka, A.
Bublík, O.
Vimmr, J.
Citation: Computational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 83-84.
Issue Date: 2018
Publisher: Západočeská univerzita v Plzni
Document type: konferenční příspěvek
URI: http://hdl.handle.net/11025/30819
ISBN: 978-80-261-0819-1
Keywords: třepetající se hranice;interakce struktura tekutina;aeroelastická analýza;FlowPro;Galerkinův kód
Keywords in different language: flutter boundary;fluid-structure interaction;aeroelastic analysis;FlowPro;Galerkin code
Abstract in different language: This 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.
Rights: Copyright © 2018 University of West Bohemia, Plzeň, Czech Republic
Appears in Collections:Konferenční příspěvky / Conference papers (NTIS)
Konferenční příspěvky / Conference Papers (KME)
Computational mechanics 2018
Computational mechanics 2018

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