| Title: | FE analysis of the T-profile for airplane door |
| Authors: | Zámečníková, T. Padovec, Z. Sedláček, R. Křena, J. |
| Citation: | Computational mechanics 2018: book of extended abstracts: 34th conference with international participation, p. 135-136. |
| Issue Date: | 2018 |
| Publisher: | Západočeská univerzita v Plzni |
| Document type: | konferenční příspěvek conferenceObject |
| URI: | http://hdl.handle.net/11025/30844 https://www.zcu.cz/export/sites/zcu/pracoviste/vyd/online/FAV_Computational_Mechanics_2018.pdf |
| ISBN: | 978-80-261-0819-1 |
| Keywords: | analýza pomocí metody konečných prvků;dveře letadla |
| Keywords in different language: | finite element method analysis;airplane door |
| Abstract in different language: | 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. |
| Rights: | Copyright © 2018 University of West Bohemia, Plzeň, Czech Republic |
| Appears in Collections: | Computational mechanics 2018 Computational mechanics 2018 |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| Zamecnikova.pdf | Plný text | 496,31 kB | Adobe PDF | View/Open |
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