dc.contributor
Universitat de Girona. Escola Politècnica Superior
dc.contributor
Costa i Balanzat, Josep
dc.contributor.author
García García, Axel
dc.date.accessioned
2024-05-22T11:06:26Z
dc.date.available
2024-05-22T11:06:26Z
dc.identifier
http://hdl.handle.net/10256/11526
dc.identifier.uri
https://hdl.handle.net/10256/11526
dc.description.abstract
Nowadays the use of composite materials is really common in industries because of its low weight in comparison with its structural benefits. In aeronautic industries, there is a constant interest in lightening all of its components. Especially on civil aircraft fuselages which are done with skin and reinforcements. One of the design’s objectives of this skin is to avoid buckling.
Our objective is to create a laminate that can accomplish the fuselage’s skin’s requirements reducing its weight and preserving its mechanical integrity
dc.format
application/pdf
dc.format
application/vnd.ms-excel
dc.rights
Attribution-NonCommercial-NoDerivs 3.0 Spain
dc.rights
http://creativecommons.org/licenses/by-nc-nd/3.0/es/
dc.rights
info:eu-repo/semantics/openAccess
dc.source
Enginyeria en Tecnologies Industrials (TFG)
dc.subject
Indústria aeronàutica
dc.subject
Materials laminats
dc.subject
Aircraft industry
dc.subject
Laminated materials
dc.title
Improvement of the carbon composite skin of the fuselage of an aircraft by means of optimization algorithms to define laminate stacking sequences
dc.type
info:eu-repo/semantics/bachelorThesis
