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dc.contributorMartínez García, Javier
dc.contributor.authorPan, Lei
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament d'Enginyeria Civil i Ambiental
dc.date.accessioned2019-11-09T09:33:17Z
dc.date.available2019-11-09T09:33:17Z
dc.date.issued2019-06-05
dc.identifier.urihttp://hdl.handle.net/2117/172018
dc.description.abstractThis 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.isoeng
dc.publisherUniversitat Politècnica de Catalunya
dc.rightsAttribution-NonCommercial 3.0 Spain
dc.rights.urihttp://creativecommons.org/licenses/by-nc/3.0/es/
dc.subjectÀrees temàtiques de la UPC::Enginyeria civil
dc.subject.lcshComposite materials
dc.subject.lcshNumerical analysis
dc.titleNumerical Analysis of Interior Aircraft Structures made of Composite Materials
dc.typeMaster thesis
dc.subject.lemacMaterials compostos
dc.subject.lemacAnàlisi numèrica
dc.identifier.slugPRISMA-145523
dc.rights.accessOpen Access
dc.date.updated2019-07-19T11:33:01Z
dc.audience.educationlevelMàster
dc.audience.mediatorEscola Tècnica Superior d'Enginyers de Camins, Canals i Ports de Barcelona


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Except where otherwise noted, content on this work is licensed under a Creative Commons license: Attribution-NonCommercial 3.0 Spain