A finite element unified formulation for composite laminates in bending considering progressive damage (2022)
- Authors:
- USP affiliated authors: RIBEIRO, MARCELO LEITE - EESC ; TITA, VOLNEI - EESC ; FERREIRA, GREGÓRIO FELIPE OLIVEIRA - EESC
- Unidade: EESC
- DOI: 10.1016/j.tws.2021.108864
- Subjects: MECÂNICA DO DANO; MÉTODO DOS ELEMENTOS FINITOS; ENGENHARIA MECÂNICA
- Agências de fomento:
- Language: Inglês
- Imprenta:
- Publisher: Elsevier
- Publisher place: Kidlington, UK
- Date published: 2022
- Source:
- Título: Thin-Walled Structures
- ISSN: 0263-8231
- Volume/Número/Paginação/Ano: v. 172, article 108864, p. 1-13, 2022
- Status:
- Artigo aberto em periódico híbrido (Hybrid Open Access)
- Versão do Documento:
- Versão publicada (Published version)
- Acessar versão aberta:
-
ABNT
FERREIRA, Gregório Felipe Oliveira et al. A finite element unified formulation for composite laminates in bending considering progressive damage. Thin-Walled Structures, v. 172, p. 1-13, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.tws.2021.108864. Acesso em: 07 maio 2026. -
APA
Ferreira, G. F. O., Almeida Júnior, J. H. S., Ribeiro, M. L., Ferreira, A. J. M., & Tita, V. (2022). A finite element unified formulation for composite laminates in bending considering progressive damage. Thin-Walled Structures, 172, 1-13. doi:10.1016/j.tws.2021.108864 -
NLM
Ferreira GFO, Almeida Júnior JHS, Ribeiro ML, Ferreira AJM, Tita V. A finite element unified formulation for composite laminates in bending considering progressive damage [Internet]. Thin-Walled Structures. 2022 ; 172 1-13.[citado 2026 maio 07 ] Available from: https://doi.org/10.1016/j.tws.2021.108864 -
Vancouver
Ferreira GFO, Almeida Júnior JHS, Ribeiro ML, Ferreira AJM, Tita V. A finite element unified formulation for composite laminates in bending considering progressive damage [Internet]. Thin-Walled Structures. 2022 ; 172 1-13.[citado 2026 maio 07 ] Available from: https://doi.org/10.1016/j.tws.2021.108864 - Development of a finite element via unified formulation: implementation as a user element subroutine to predict stress profiles in composite plates
- Computational analysis for carbon-epoxy plates damaged by low-velocity impact
- Computational analyses of composite plates under low-velocity impact loading
- Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation
- Evaluation of progressive failure of filament winding composite structures under multiple stress state
- Experimental dynamic investigations of bio and synthetic composites for use in aircraft interior structures
- Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage
- Comparison between mechanical properties of bio and synthetic composites for use in aircraft interior structures
- Transversal shear caracterisation of thick laminated composite using a representative volume element (RVE)
- Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression
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