Full metadata record
| DC pole | Hodnota | Jazyk |
|---|---|---|
| dc.contributor.author | Čečrdle, J. | |
| dc.contributor.author | Vích, O. | |
| dc.contributor.editor | Adámek, Vítězslav | |
| dc.contributor.editor | Jonášová, Alena | |
| dc.contributor.editor | Plánička, Stanislav | |
| dc.contributor.editor | Zajíček, Martin | |
| dc.date.accessioned | 2019-01-16T06:20:41Z | - |
| dc.date.available | 2019-01-16T06:20:41Z | - |
| dc.date.issued | 2018 | |
| dc.identifier.citation | Computational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 7-8. | en |
| dc.identifier.isbn | 978-80-261-0819-1 | |
| dc.identifier.uri | http://hdl.handle.net/11025/30781 | |
| dc.identifier.uri | https://www.zcu.cz/export/sites/zcu/pracoviste/vyd/online/FAV_Computational_Mechanics_2018.pdf | |
| 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 | aeroelastická analýza | cs |
| dc.subject | turbovrtulové dopravní letadlo | cs |
| dc.subject | křídlové nádrže | cs |
| dc.title | Aeroelastic analysis of turboprop commuter aircraft with tip-tanks | 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 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.subject.translated | aeroelastic analysis | en |
| dc.subject.translated | turboprop commuter aircraft | en |
| dc.subject.translated | wing-tip tanks | en |
| dc.type.status | Peer-reviewed | en |
| Vyskytuje se v kolekcích: | Computational mechanics 2018 Computational mechanics 2018 | |
Soubory připojené k záznamu:
| Soubor | Popis | Velikost | Formát | |
|---|---|---|---|---|
| Cecrdle.pdf | Plný text | 217,03 kB | Adobe PDF | Zobrazit/otevřít |
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