Experimental analysis of transverse impact loading on composite cylinders (2015)
- Authors:
- USP affiliated authors: RIBEIRO, MARCELO LEITE - EESC ; TITA, VOLNEI - EESC
- Unidade: EESC
- DOI: 10.1016/j.compstruct.2015.07.088
- Subjects: ANÁLISE EXPERIMENTAL DE ESTRUTURAS; DANO; ESTRUTURAS (IMPACTO)
- Language: Inglês
- Imprenta:
- Source:
- Título do periódico: Composite Structures
- ISSN: 0263-8223
- Volume/Número/Paginação/Ano: v. 133, p. 547-563, Dec. 2015
- Este periódico é de assinatura
- Este artigo NÃO é de acesso aberto
- Cor do Acesso Aberto: closed
-
ABNT
RIBEIRO, Marcelo Leite e VANDEPITTE, Dirk e TITA, Volnei. Experimental analysis of transverse impact loading on composite cylinders. Composite Structures, v. 133, p. 547-563, 2015Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2015.07.088. Acesso em: 19 abr. 2024. -
APA
Ribeiro, M. L., Vandepitte, D., & Tita, V. (2015). Experimental analysis of transverse impact loading on composite cylinders. Composite Structures, 133, 547-563. doi:10.1016/j.compstruct.2015.07.088 -
NLM
Ribeiro ML, Vandepitte D, Tita V. Experimental analysis of transverse impact loading on composite cylinders [Internet]. Composite Structures. 2015 ; 133 547-563.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1016/j.compstruct.2015.07.088 -
Vancouver
Ribeiro ML, Vandepitte D, Tita V. Experimental analysis of transverse impact loading on composite cylinders [Internet]. Composite Structures. 2015 ; 133 547-563.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1016/j.compstruct.2015.07.088 - 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
- Buckling and post-buckling of filament wound composite tubes under axial compression: linear, nonlinear, damage and experimental analyses
Informações sobre o DOI: 10.1016/j.compstruct.2015.07.088 (Fonte: oaDOI API)
How to cite
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas