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 do periódico: Composites Part B
- ISSN: 1359-8368
- Volume/Número/Paginação/Ano: v. 149, p. 227-239, 2018
- Este periódico é de assinatura
- Este artigo é de acesso aberto
- URL de acesso aberto
- Cor do Acesso Aberto: hybrid
- Licença: publisher-specific-oa
-
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: 16 abr. 2024. -
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 2024 abr. 16 ] 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 2024 abr. 16 ] Available from: https://doi.org/10.1016/j.compositesb.2018.05.004 - A finite element damage model to predict failure behavior of composite sandwich structures
- Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage
- Progressive failure analysis of filament wound composite tubes under internal pressure
- Transversal shear caracterisation of thick laminated composite using a representative volume element (RVE)
- Experimental dynamic investigations of bio and synthetic composites for use in aircraft interior structures
- Buckling optimization in variable stiffness composite laminated
- Failure models for composite structures under compression loading
- Influence of stacking sequence on the radial compression of filament wound composite tubes
- Experimental methodology for testing metal-composite bolted joints
- Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression
Informações sobre o DOI: 10.1016/j.compositesb.2018.05.004 (Fonte: oaDOI API)
Download do texto completo
| Tipo | Nome | Link | |
|---|---|---|---|
 | artigo 06 - Buckling and ... |
How to cite
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
