Damage and failure in carbon/epoxy filament wound composite tubes under external pressure: experimental and numerical approaches (2016)
- Authors:
- USP affiliated authors: RIBEIRO, MARCELO LEITE - EESC ; TITA, VOLNEI - EESC
- Unidade: EESC
- DOI: 10.1016/j.matdes.2016.02.054
- Subjects: MÉTODO DOS ELEMENTOS FINITOS; TUBOS; FALHA
- Keywords: BUCKING; FILAMENT WINDING
- Language: Inglês
- Imprenta:
- Source:
- Título do periódico: Materials and Design
- ISSN: 0264-1275
- Volume/Número/Paginação/Ano: v. 96, p. 431-438, Apr. 2016
- Este periódico é de assinatura
- Este artigo NÃO é de acesso aberto
- Cor do Acesso Aberto: closed
-
ABNT
ALMEIDA JÚNIOR, José Humberto Santos et al. Damage and failure in carbon/epoxy filament wound composite tubes under external pressure: experimental and numerical approaches. Materials and Design, v. 96, p. 431-438, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.matdes.2016.02.054. Acesso em: 29 mar. 2024. -
APA
Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2016). Damage and failure in carbon/epoxy filament wound composite tubes under external pressure: experimental and numerical approaches. Materials and Design, 96, 431-438. doi:10.1016/j.matdes.2016.02.054 -
NLM
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage and failure in carbon/epoxy filament wound composite tubes under external pressure: experimental and numerical approaches [Internet]. Materials and Design. 2016 ; 96 431-438.[citado 2024 mar. 29 ] Available from: https://doi.org/10.1016/j.matdes.2016.02.054 -
Vancouver
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage and failure in carbon/epoxy filament wound composite tubes under external pressure: experimental and numerical approaches [Internet]. Materials and Design. 2016 ; 96 431-438.[citado 2024 mar. 29 ] Available from: https://doi.org/10.1016/j.matdes.2016.02.054 - A finite element damage model to predict failure behavior of composite sandwich structures
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Informações sobre o DOI: 10.1016/j.matdes.2016.02.054 (Fonte: oaDOI API)
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