Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Dupal, J. | |
| dc.contributor.author | Zajíček, M. | |
| dc.contributor.author | Lukeš, V. | |
| dc.contributor.editor | Adámek, Vítězslav | |
| dc.contributor.editor | Jonášová, Alena | |
| dc.contributor.editor | Plánička, Stanislav | |
| dc.contributor.editor | Zajíček, Martin | |
| dc.date.accessioned | 2019-01-16T06:56:08Z | - |
| dc.date.available | 2019-01-16T06:56:08Z | - |
| dc.date.issued | 2018 | |
| dc.identifier.citation | Computational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 15-16. | en |
| dc.identifier.isbn | 978-80-261-0819-1 | |
| dc.identifier.uri | http://hdl.handle.net/11025/30784 | |
| dc.identifier.uri | https://www.zcu.cz/export/sites/zcu/pracoviste/vyd/online/FAV_Computational_Mechanics_2018.pdf | |
| dc.description.sponsorship | This publication was supported by the project TE 01020068 of the Technology Agency of the Czech Republic and by the project GA16-04546S. | 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 | modelovaní konečných prvků | cs |
| dc.subject | lopatka turbíny | cs |
| dc.subject | vibrace | cs |
| dc.title | Modelling of the turbine blade by new finite element | en |
| dc.type | konferenční příspěvek | cs |
| dc.type | conferenceObject | en |
| dc.rights.access | openAccess | en |
| dc.type.version | publishedVersion | en |
| dc.description.abstract-translated | The paper deals with 1D finite element modelling of a turbine blade. The proposed finite element has only 16 degrees of freedom (DOF) and enables to achieve a complex model of turbo-machine with a relatively small DOF number, more details will be described in the article. It is a great advantage but the pre-processing for the blade cross section parameters of the individual blades is a little bit more complicated. This approach means to solve a warping function in chosen cross sections of the blade and simultaneously calculate the geometrical parameters of those cross sections. The second step represents an approximation of the obtained parameters along the axis coordinate ? by means of spline functions. The next step is gradual computation of local finite element matrices and assemblage of the global blade matrices. | en |
| dc.subject.translated | finite element modelling | en |
| dc.subject.translated | turbine blade | en |
| dc.subject.translated | vibration | en |
| dc.type.status | Peer-reviewed | en |
| Appears in Collections: | Konferenční příspěvky / Conference Papers (KME) Computational mechanics 2018 Computational mechanics 2018 | |
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