A Probabilistic Approach in Fuselage Damage Analysis <em>via</em> Boundary Element Method

This chapter presents a new alternative approach to the analysis of the fatigue life of aircraft fuselage parts considering the compliance of internal elements to replace the classical model of critical crack size. In this case, from a global–local analysis using the boundary element method (BEM), i...

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Detalles Bibliográficos

Autores principales:	Gomes, Gilberto, Oliveira, Thiago, Jr, Francisco Evangelista
Formato:	Capítulo de libro
Lenguaje:	inglés
Publicado:	IntechOpen 2021
Materias:	Physical Sciences, Engineering and Technology
Acceso en línea:	https://www.intechopen.com/chapters/77541
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