Full metadata record
| DC pole | Hodnota | Jazyk |
|---|---|---|
| dc.contributor.author | Pecka, A. | |
| dc.contributor.author | Bublík, O. | |
| dc.contributor.author | Vimmr, J. | |
| dc.contributor.editor | Adámek, Vítězslav | |
| dc.contributor.editor | Jonášová, Alena | |
| dc.contributor.editor | Plánička, Stanislav | |
| dc.contributor.editor | Zajíček, Martin | |
| dc.date.accessioned | 2019-01-17T11:54:36Z | - |
| dc.date.available | 2019-01-17T11:54:36Z | - |
| dc.date.issued | 2018 | |
| dc.identifier.citation | Computational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 83-84. | en |
| dc.identifier.isbn | 978-80-261-0819-1 | |
| dc.identifier.uri | http://hdl.handle.net/11025/30819 | |
| dc.identifier.uri | https://www.zcu.cz/export/sites/zcu/pracoviste/vyd/online/FAV_Computational_Mechanics_2018.pdf | |
| dc.description.sponsorship | The 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.format | 2 s. | cs |
| dc.format.mimetype | application/pdf | |
| dc.language.iso | en | en |
| dc.publisher | Západočeská univerzita v Plzni | cs |
| dc.relation.ispartofseries | Computational Mechanics | en |
| dc.rights | Copyright © 2018 University of West Bohemia, Plzeň, Czech Republic | en |
| dc.subject | třepetající se hranice | cs |
| dc.subject | interakce struktura tekutina | cs |
| dc.subject | aeroelastická analýza | cs |
| dc.subject | FlowPro | cs |
| dc.subject | Galerkinův kód | cs |
| dc.title | Flutter boundary assessment for a blade cascade using developed discontinuous Galerkin code | en |
| dc.type | konferenční příspěvek | cs |
| dc.type | conferenceObject | en |
| dc.rights.access | openAccess | en |
| dc.type.version | publishedVersion | en |
| dc.description.abstract-translated | 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. | en |
| dc.subject.translated | flutter boundary | en |
| dc.subject.translated | fluid-structure interaction | en |
| dc.subject.translated | aeroelastic analysis | en |
| dc.subject.translated | FlowPro | en |
| dc.subject.translated | Galerkin code | en |
| dc.type.status | Peer-reviewed | en |
| Vyskytuje se v kolekcích: | Konferenční příspěvky / Conference papers (NTIS) Konferenční příspěvky / Conference Papers (KME) Computational mechanics 2018 Computational mechanics 2018 | |
Soubory připojené k záznamu:
| Soubor | Popis | Velikost | Formát | |
|---|---|---|---|---|
| Pecka.pdf | Plný text | 1,24 MB | Adobe PDF | Zobrazit/otevřít |
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