STRUCTURAL EFFECT OF STAGGERED COMPOSITE REINFORCEMENTS WITHIN THE FIREWALL OF AN AIRCRAFT
Journal
DYNA
ISSN
1989-1490
Publisher
DYNA Publishing
Date Issued
2019
Author(s)
VICTOR ALFONSO RAMIREZ ELÍAS
ELIAS RIGOBERTO LEDESMA OROZCO
HILARIO HERNANDEZ MORENO
ERIK VARGAS ROJAS
LUIS FERNANDO PUENTE MEDELLIN
LUIS DAVID CELAYA GARCIA
Type
text::journal::journal article
DOI
Abstract
The performance of composite materials, such as high strength and low density, is ideal for aerospace applications. This paper presents the structural analysis of a component of a utility aircraft, the STELA M1. As this is still a prototype, the aim is to validate the resistance of its fuselage subjected first to static loads.