Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses (2018)
- Authors:
- USP affiliated authors: RIBEIRO, MARCELO LEITE - EESC ; TITA, VOLNEI - EESC
- Unidade: EESC
- DOI: 10.1016/j.compositesb.2018.05.004
- Subjects: FLAMBAGEM; MÉTODO DOS ELEMENTOS FINITOS; ENGENHARIA AERONÁUTICA
- Agências de fomento:
- Language: Inglês
- Imprenta:
- Publisher: Elsevier
- Publisher place: Oxford, United Kingdom
- Date published: 2018
- Source:
- Título: Composites Part B
- ISSN: 1359-8368
- Volume/Número/Paginação/Ano: v. 149, p. 227-239, 2018
- Status:
- Artigo possui versão em acesso aberto em repositório (Green Open Access)
- Versão do Documento:
- Versão publicada (Published version)
- Acessar versão aberta:
-
ABNT
ALMEIDA JÚNIOR, José Humberto Santos et al. Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses. Composites Part B, v. 149, p. 227-239, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.compositesb.2018.05.004. Acesso em: 07 abr. 2026. -
APA
Almeida Júnior, J. H. S., Tonatto, M. L. P., Ribeiro, M. L., Tita, V., & Amico, S. C. (2018). Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses. Composites Part B, 149, 227-239. doi:10.1016/j.compositesb.2018.05.004 -
NLM
Almeida Júnior JHS, Tonatto MLP, Ribeiro ML, Tita V, Amico SC. Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses [Internet]. Composites Part B. 2018 ; 149 227-239.[citado 2026 abr. 07 ] Available from: https://doi.org/10.1016/j.compositesb.2018.05.004 -
Vancouver
Almeida Júnior JHS, Tonatto MLP, Ribeiro ML, Tita V, Amico SC. Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses [Internet]. Composites Part B. 2018 ; 149 227-239.[citado 2026 abr. 07 ] Available from: https://doi.org/10.1016/j.compositesb.2018.05.004 - Experimental dynamic investigations of bio and synthetic composites for use in aircraft interior structures
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- Damage and failure in carbon/epoxy filament wound composite tubes under external pressure: experimental and numerical approaches
- Influence of stacking sequence on the radial compression of filament wound composite tubes
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- A finite element damage model to predict failure behavior of composite sandwich structures
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