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Improvement of the carbon composite skin of the fuselage of an aircraft by means of optimization algorithms to define laminate stacking sequences

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

Manager: Costa i Balanzat, Josep
Other contributions: Universitat de Girona. Escola Politècnica Superior
Author: García García, Axel
Date: 2015 June
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
Format: application/pdf
application/vnd.ms-excel
Document access: http://hdl.handle.net/10256/11526
Language: eng
Collection: Enginyeria en Tecnologies Industrials (TFG)
Rights: Attribution-NonCommercial-NoDerivs 3.0 Spain
Rights URI: http://creativecommons.org/licenses/by-nc-nd/3.0/es/
Subject: Algorismes
Indústria aeronàutica
Materials laminats
Algorithms
Aircraft industry
Laminated materials
Title: Improvement of the carbon composite skin of the fuselage of an aircraft by means of optimization algorithms to define laminate stacking sequences
Type: info:eu-repo/semantics/bachelorThesis
Repository: DUGiDocs

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