Numerical study on the impact response of aircraft fuselage structures subjected to large-size tire fragment

By applying finite element software ANSYS/LS-DYNA, finite element models of front bulkhead and main cabin are established, which aims to assess the dynamic response of fuselage structures impacted by tire fragment under bursting mode. Besides, dynamic characteristics of the two fuselage structures i...

Descripción completa

Detalles Bibliográficos
Autores principales: Jia, Senqing, Wang, Fusheng, Yu, Lingjun, Wei, Zheng, Xu, Bin
Formato: Online Artículo Texto
Lenguaje:English
Publicado: SAGE Publications 2019
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10453686/
https://www.ncbi.nlm.nih.gov/pubmed/31829868
http://dx.doi.org/10.1177/0036850419877744

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10453686/
https://www.ncbi.nlm.nih.gov/pubmed/31829868
http://dx.doi.org/10.1177/0036850419877744

Ejemplares similares