Full metadata record
| DC pole | Hodnota | Jazyk |
|---|---|---|
| dc.contributor.author | Zámečníková, T. | |
| dc.contributor.author | Padovec, Z. | |
| dc.contributor.author | Sedláček, R. | |
| dc.contributor.author | Křena, J. | |
| dc.contributor.editor | Adámek, Vítězslav | |
| dc.contributor.editor | Jonášová, Alena | |
| dc.contributor.editor | Plánička, Stanislav | |
| dc.contributor.editor | Zajíček, Martin | |
| dc.date.accessioned | 2019-01-18T11:12:09Z | - |
| dc.date.available | 2019-01-18T11:12:09Z | - |
| dc.date.issued | 2018 | |
| dc.identifier.citation | Computational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 135-136. | en |
| dc.identifier.isbn | 978-80-261-0819-1 | |
| dc.identifier.uri | http://hdl.handle.net/11025/30844 | |
| dc.identifier.uri | https://www.zcu.cz/export/sites/zcu/pracoviste/vyd/online/FAV_Computational_Mechanics_2018.pdf | |
| dc.description.sponsorship | The work has been supported by the grant project MPO FV30033 and by the research project SGS18/175/OHK2/3T/12. | 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 | analýza pomocí metody konečných prvků | cs |
| dc.subject | dveře letadla | cs |
| dc.title | FE analysis of the T-profile for airplane door | 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 the replacement of the titanium profile in the airplane door with the composite one. The aim of the project is the FEM analysis of the titanium T-profile integrated in airplane door and to design a composite part which will be lighter and stiffer. It is obvious that the design will change the shape of the cross-section of the T-profile. The connecting dimensions have to remain the same. So, several ways were chosen to examine the stiffness of the titanium and composite T-profile. | en |
| dc.subject.translated | finite element method analysis | en |
| dc.subject.translated | airplane door | 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 | |
|---|---|---|---|---|
| Zamecnikova.pdf | Plný text | 496,31 kB | Adobe PDF | Zobrazit/otevřít |
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