STRUCTURAL EFFECT OF STAGGERED COMPOSITE REINFORCEMENTS WITHIN THE FIREWALL OF AN AIRCRAFT

VICTOR ALFONSO RAMIREZ ELÍASRodríguez-Sánchez, Alejandro E.Alejandro E.Rodríguez-SánchezELIAS RIGOBERTO LEDESMA OROZCOHILARIO HERNANDEZ MORENOERIK VARGAS ROJASLUIS FERNANDO PUENTE MEDELLINLUIS DAVID CELAYA GARCIA2024-04-052024-04-052019https://scripta.up.edu.mx/handle/20.500.12552/1025410.6036/9334The 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.CortafuegoCompuestosavión utilitarioAnálisis EstructuralMétodo de elemento FinitoAnálisis de Tsa-Wufirewallcompositesutilitarian aircraftstructural analysisfinite element methodTsai-Wu analysis.STRUCTURAL EFFECT OF STAGGERED COMPOSITE REINFORCEMENTS WITHIN THE FIREWALL OF AN AIRCRAFTResource Types::text::journal::journal article