Numerical Analysis of Interior Aircraft Structures made of Composite Materials

Pan, Lei

dc.contributor	Martínez García, Javier
dc.contributor.author	Pan, Lei
dc.contributor.other	Universitat Politècnica de Catalunya. Departament d'Enginyeria Civil i Ambiental
dc.date.accessioned	2019-11-09T09:33:17Z
dc.date.available	2019-11-09T09:33:17Z
dc.date.issued	2019-06-05
dc.identifier.uri	http://hdl.handle.net/2117/172018
dc.description.abstract	This master thesis focuses on the simulation of interior aircraft structures made of composite materials. These structures are made of a sandwich material consisting of two glass fiber skins around a honeycomb core. Different strategies developed to simulate composite materials will be used for their mechanical characterization. The composites that will be used in this project are bio-based. Developing this project the student will learn basic concepts of structural analysis using FEM and will familiarize with formulations to characterize composite materials.
dc.language.iso	eng
dc.publisher	Universitat Politècnica de Catalunya
dc.rights	Attribution-NonCommercial 3.0 Spain
dc.rights.uri	http://creativecommons.org/licenses/by-nc/3.0/es/
dc.subject	Àrees temàtiques de la UPC::Enginyeria civil
dc.subject.lcsh	Composite materials
dc.subject.lcsh	Numerical analysis
dc.title	Numerical Analysis of Interior Aircraft Structures made of Composite Materials
dc.type	Master thesis
dc.subject.lemac	Materials compostos
dc.subject.lemac	Anàlisi numèrica
dc.identifier.slug	PRISMA-145523
dc.rights.access	Open Access
dc.date.updated	2019-07-19T11:33:01Z
dc.audience.educationlevel	Màster
dc.audience.mediator	Escola Tècnica Superior d'Enginyers de Camins, Canals i Ports de Barcelona