Numerical Analysis of Interior Aircraft Structures made of Composite Materials
Correo electrónico del autorupcpanleigmail.com
Tutor / director / evaluadorMartínez García, Javier
Tipo de documentoProjecte Final de Màster Oficial
Condiciones de accesoAcceso abierto
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.