Dynamic Pulse Buckling of Composite Stanchions in the Sub-Cargo Floor Area of a Civil Regional Aircraft

This work is focused on the investigation of the structural behavior of a composite floor beam, located in the cargo zone of a civil aircraft, subjected to cyclical low-frequency compressive loads with different amplitudes. In the first stage, the numerical models able to correctly simulate the inve...

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Detalles Bibliográficos
Autores principales: Sellitto, Andrea, Di Caprio, Francesco, Guida, Michele, Saputo, Salvatore, Riccio, Aniello
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2020
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7475968/
https://www.ncbi.nlm.nih.gov/pubmed/32823880
http://dx.doi.org/10.3390/ma13163594

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC7475968/
https://www.ncbi.nlm.nih.gov/pubmed/32823880
http://dx.doi.org/10.3390/ma13163594

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