Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, FUSELAGEM DE AERONAVES, DANO, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA
ABNT
MIRANDA, Mario et al. Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model. Composite Structures, v. 352, p. 1-16, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2024.118674. Acesso em: 10 nov. 2025.APA
Miranda, M., Cini, A., Raimondo, A., & Tita, V. (2024). Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model. Composite Structures, 352, 1-16. doi:10.1016/j.compstruct.2024.118674NLM
Miranda M, Cini A, Raimondo A, Tita V. Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model [Internet]. Composite Structures. 2024 ; 352 1-16.[citado 2025 nov. 10 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118674Vancouver
Miranda M, Cini A, Raimondo A, Tita V. Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model [Internet]. Composite Structures. 2024 ; 352 1-16.[citado 2025 nov. 10 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118674
