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...
Gardado en:
| Principais autores: | , , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado: |
SAGE Publishing
2020-03-01
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| Series: | Science Progress |
| Acceso en liña: | https://doi.org/10.1177/0036850419877744 |
| Tags: |
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