Computational analyses of composite plates under low-velocity impact loading (2019)
- Authors:
- USP affiliated authors: RIBEIRO, MARCELO LEITE - EESC ; TITA, VOLNEI - EESC ; FERREIRA, GREGÓRIO FELIPE OLIVEIRA - EESC
- Unidade: EESC
- DOI: 10.1016/j.matpr.2019.02.020
- Subjects: MATERIAIS COMPÓSITOS; MÉTODO DOS ELEMENTOS FINITOS; FALHA; ENGENHARIA AERONÁUTICA
- Agências de fomento:
- Language: Inglês
- Imprenta:
- Publisher: Elsevier BV
- Publisher place: Amsterdam, Netherlands
- Date published: 2019
- Source:
- Título: Materials Today: Proceedings
- ISSN: 2214-7853
- Volume/Número/Paginação/Ano: v. 8, part 3, p. 778-788, 2019
- Conference titles: Brazilian Conference on Composite Materials - BCCM
- Este periódico é de assinatura
- Este artigo é de acesso aberto
- URL de acesso aberto
- Cor do Acesso Aberto: bronze
- Licença: publisher-specific-oa
-
ABNT
FERREIRA, Gregório Felipe Oliveira et al. Computational analyses of composite plates under low-velocity impact loading. Materials Today: Proceedings. Amsterdam, Netherlands: Elsevier BV. Disponível em: https://doi.org/10.1016/j.matpr.2019.02.020. Acesso em: 04 out. 2024. , 2019 -
APA
Ferreira, G. F. O., Ribeiro, M. L., Ferreira, A. J. M., & Tita, V. (2019). Computational analyses of composite plates under low-velocity impact loading. Materials Today: Proceedings. Amsterdam, Netherlands: Elsevier BV. doi:10.1016/j.matpr.2019.02.020 -
NLM
Ferreira GFO, Ribeiro ML, Ferreira AJM, Tita V. Computational analyses of composite plates under low-velocity impact loading [Internet]. Materials Today: Proceedings. 2019 ; 8 778-788.[citado 2024 out. 04 ] Available from: https://doi.org/10.1016/j.matpr.2019.02.020 -
Vancouver
Ferreira GFO, Ribeiro ML, Ferreira AJM, Tita V. Computational analyses of composite plates under low-velocity impact loading [Internet]. Materials Today: Proceedings. 2019 ; 8 778-788.[citado 2024 out. 04 ] Available from: https://doi.org/10.1016/j.matpr.2019.02.020 - Computational analysis for carbon-epoxy plates damaged by low-velocity impact
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- Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage
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- 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
Informações sobre o DOI: 10.1016/j.matpr.2019.02.020 (Fonte: oaDOI API)
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