Application of failure criteria in aeronautical sandwich structure composites with a central hole subjected to bending testing
This study aimeds at investigating the mechanical behavior of an E-glass fiber-reinforced epoxy resin of a laminated composite sandwich with honeycomb core and a central hole, used in the aeronautics industry submitted to bending loading. Three analytical failure models applied to laminated composit...
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| Principais autores: | , , , |
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| Formato: | article |
| Idioma: | English |
| Publicado em: |
ABM, ABC, ABPol
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| Assuntos: | |
| Endereço do item: | https://repositorio.ufrn.br/handle/123456789/31650 |
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