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Artigo de periodico
Crashworthiness assessment of a composite fuselage stanchion employing a strain rate dependent damage model (2024)
Miranda, Mario; Cini, Andrea; Raimondo, Antonio; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, FUSELAGEM DE AERONAVES, DANO, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 17 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.2024.118674
NLM
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. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118674
Vancouver
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. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118674
Artigo de periodico
Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation (2024)
Santana, Pedro Bührer; Ferreira, Antonio Joaquim Mendes; Gomes, Herbert Martins; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, ANÁLISE NÃO LINEAR DE ESTRUTURAS, DANO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SANTANA, Pedro Bührer et al. Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation. Composite Structures, v. 348, p. 1-16, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2024.118506. Acesso em: 17 nov. 2025.
APA
Santana, P. B., Ferreira, A. J. M., Gomes, H. M., & Tita, V. (2024). Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation. Composite Structures, 348, 1-16. doi:10.1016/j.compstruct.2024.118494
NLM
Santana PB, Ferreira AJM, Gomes HM, Tita V. Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation [Internet]. Composite Structures. 2024 ; 348 1-16.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
Vancouver
Santana PB, Ferreira AJM, Gomes HM, Tita V. Nonlinear finite element damage analysis of laminated shells by Carrera Unified Formulation [Internet]. Composite Structures. 2024 ; 348 1-16.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
Artigo de periodico
Novel progressive failure model for quasi-orthotropic pultruded FRP structures: application to compact tension and web-crippling case studies (Part II) (2021)
Gonilha, Jose A.; Silvestre, Nuno; Correia, João R.; Tita, Volnei ; Fernandes, Lourenço Almeida
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS DE FIBRAS, DANO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GONILHA, Jose A. et al. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: application to compact tension and web-crippling case studies (Part II). Composite Structures, v. 255, p. 1-16, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2020.112973. Acesso em: 17 nov. 2025.
APA
Gonilha, J. A., Silvestre, N., Correia, J. R., Tita, V., & Fernandes, L. A. (2021). Novel progressive failure model for quasi-orthotropic pultruded FRP structures: application to compact tension and web-crippling case studies (Part II). Composite Structures, 255, 1-16. doi:10.1016/j.compstruct.2020.112973
NLM
Gonilha JA, Silvestre N, Correia JR, Tita V, Fernandes LA. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: application to compact tension and web-crippling case studies (Part II) [Internet]. Composite Structures. 2021 ; 255 1-16.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112973
Vancouver
Gonilha JA, Silvestre N, Correia JR, Tita V, Fernandes LA. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: application to compact tension and web-crippling case studies (Part II) [Internet]. Composite Structures. 2021 ; 255 1-16.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112973
Artigo de periodico
Novel progressive failure model for quasi-orthotropic pultruded FRP structures: formulation and calibration of parameters (Part I) (2021)
Gonilha, Jose A.; Silvestre, Nuno; Correia, João R.; Tita, Volnei ; Martins, David
Source: Composite Structures. Unidade: EESC
Subjects: DANO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GONILHA, Jose A. et al. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: formulation and calibration of parameters (Part I). Composite Structures, v. 255, p. 1-22, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2020.112974. Acesso em: 17 nov. 2025.
APA
Gonilha, J. A., Silvestre, N., Correia, J. R., Tita, V., & Martins, D. (2021). Novel progressive failure model for quasi-orthotropic pultruded FRP structures: formulation and calibration of parameters (Part I). Composite Structures, 255, 1-22. doi:10.1016/j.compstruct.2020.112974
NLM
Gonilha JA, Silvestre N, Correia JR, Tita V, Martins D. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: formulation and calibration of parameters (Part I) [Internet]. Composite Structures. 2021 ; 255 1-22.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112974
Vancouver
Gonilha JA, Silvestre N, Correia JR, Tita V, Martins D. Novel progressive failure model for quasi-orthotropic pultruded FRP structures: formulation and calibration of parameters (Part I) [Internet]. Composite Structures. 2021 ; 255 1-22.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112974
Artigo de periodico
Micro drilling of carbon fiber reinforced polymer (2019)
Basso, Igor; Batista, Marcelo Ferreira; Jasinevicius, Renato Goulart ; Rodrigues, Alessandro Roger ; Rubio, Juan Carlos Campos
Source: Composite Structures. Unidade: EESC
Subjects: PERFURAÇÃO, POLÍMEROS (MATERIAIS), DANO
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BASSO, Igor et al. Micro drilling of carbon fiber reinforced polymer. Composite Structures, v. No 2019, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2019.111312. Acesso em: 17 nov. 2025.
APA
Basso, I., Batista, M. F., Jasinevicius, R. G., Rodrigues, A. R., & Rubio, J. C. C. (2019). Micro drilling of carbon fiber reinforced polymer. Composite Structures, No 2019. doi:10.1016/j.compstruct.2019.111312
NLM
Basso I, Batista MF, Jasinevicius RG, Rodrigues AR, Rubio JCC. Micro drilling of carbon fiber reinforced polymer [Internet]. Composite Structures. 2019 ; No 2019[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2019.111312
Vancouver
Basso I, Batista MF, Jasinevicius RG, Rodrigues AR, Rubio JCC. Micro drilling of carbon fiber reinforced polymer [Internet]. Composite Structures. 2019 ; No 2019[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2019.111312
Artigo de periodico
Experimental analysis of transverse impact loading on composite cylinders (2015)
Ribeiro, Marcelo Leite ; Vandepitte, Dirk; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: ANÁLISE EXPERIMENTAL DE ESTRUTURAS, DANO, ESTRUTURAS (IMPACTO)
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 17 nov. 2025.
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 2025 nov. 17 ] 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 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2015.07.088

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