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
Issue Date: 2018
Publisher: Západočeská univerzita v Plzni
Document type: konferenční příspěvek
conferenceObject
URI: http://hdl.handle.net/11025/30844
ISBN: 978-80-261-0819-1
Keywords: anal�za pomoc� metody kone�n�ch prvk�;dve�e 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 SizeFormat 
Zamecnikova.pdfPlný text496,31 kBAdobe PDFView/Open


Please use this identifier to cite or link to this item: http://hdl.handle.net/11025/30844

Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.