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Artigo de periodico
On the influence of material property uncertainties for a phenomenological progressive damage in composite laminated coupons: a sensitivity analysis approach (2025)
Santana, Pedro Bührer ; Gomes, Hebert Martins; Ferreira, Antonio J. M; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Assunto: ENGENHARIA AERONÁUTICA
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ABNT
SANTANA, Pedro Bührer et al. On the influence of material property uncertainties for a phenomenological progressive damage in composite laminated coupons: a sensitivity analysis approach. Composite Structures, v. 366, p. 1-15, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2025.119209. Acesso em: 17 nov. 2025.
APA
Santana, P. B., Gomes, H. M., Ferreira, A. J. M., & Tita, V. (2025). On the influence of material property uncertainties for a phenomenological progressive damage in composite laminated coupons: a sensitivity analysis approach. Composite Structures, 366, 1-15. doi:10.1016/j.compstruct.2025.119209
NLM
Santana PB, Gomes HM, Ferreira AJM, Tita V. On the influence of material property uncertainties for a phenomenological progressive damage in composite laminated coupons: a sensitivity analysis approach [Internet]. Composite Structures. 2025 ; 366 1-15.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119209
Vancouver
Santana PB, Gomes HM, Ferreira AJM, Tita V. On the influence of material property uncertainties for a phenomenological progressive damage in composite laminated coupons: a sensitivity analysis approach [Internet]. Composite Structures. 2025 ; 366 1-15.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119209
Artigo de periodico
Analysing the influence of delamination on composite structures using modal analysis and statistical indices (2025)
Zanetti, Matteo ; Negri, Doglas ; Vandepitte, Dirk ; Tita, Volnei ; Medeiros, Ricardo de
Source: Composite Structures. Unidade: EESC
Assunto: ENGENHARIA AERONÁUTICA
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ABNT
ZANETTI, Matteo et al. Analysing the influence of delamination on composite structures using modal analysis and statistical indices. Composite Structures, v. 371, p. 1-17, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2025.119427. Acesso em: 17 nov. 2025.
APA
Zanetti, M., Negri, D., Vandepitte, D., Tita, V., & Medeiros, R. de. (2025). Analysing the influence of delamination on composite structures using modal analysis and statistical indices. Composite Structures, 371, 1-17. doi:10.1016/j.compstruct.2025.119427
NLM
Zanetti M, Negri D, Vandepitte D, Tita V, Medeiros R de. Analysing the influence of delamination on composite structures using modal analysis and statistical indices [Internet]. Composite Structures. 2025 ; 371 1-17.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119427
Vancouver
Zanetti M, Negri D, Vandepitte D, Tita V, Medeiros R de. Analysing the influence of delamination on composite structures using modal analysis and statistical indices [Internet]. Composite Structures. 2025 ; 371 1-17.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119427
Artigo de periodico
Radial compression of thin-walled variable-angle tow filament-wound composite cylinders, Part I: Manufacture, experimental, and computational analyses in the linear-elastic regime (2025)
Souza, Gabriel Sales Candido ; Santos, Anderson Lima dos ; Maciel, Maísa Milanez Ávila Dias ; Guedes, Rui Miranda ; Viriato, Nuno ; Amico, Sandro Campos ; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Assunto: ENGENHARIA AERONÁUTICA
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ABNT
SOUZA, Gabriel Sales Candido et al. Radial compression of thin-walled variable-angle tow filament-wound composite cylinders, Part I: Manufacture, experimental, and computational analyses in the linear-elastic regime. Composite Structures, v. 366, p. 1-12, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2025.119178. Acesso em: 17 nov. 2025.
APA
Souza, G. S. C., Santos, A. L. dos, Maciel, M. M. Á. D., Guedes, R. M., Viriato, N., Amico, S. C., & Tita, V. (2025). Radial compression of thin-walled variable-angle tow filament-wound composite cylinders, Part I: Manufacture, experimental, and computational analyses in the linear-elastic regime. Composite Structures, 366, 1-12. doi:10.1016/j.compstruct.2025.119178
NLM
Souza GSC, Santos AL dos, Maciel MMÁD, Guedes RM, Viriato N, Amico SC, Tita V. Radial compression of thin-walled variable-angle tow filament-wound composite cylinders, Part I: Manufacture, experimental, and computational analyses in the linear-elastic regime [Internet]. Composite Structures. 2025 ; 366 1-12.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119178
Vancouver
Souza GSC, Santos AL dos, Maciel MMÁD, Guedes RM, Viriato N, Amico SC, Tita V. Radial compression of thin-walled variable-angle tow filament-wound composite cylinders, Part I: Manufacture, experimental, and computational analyses in the linear-elastic regime [Internet]. Composite Structures. 2025 ; 366 1-12.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119178
Artigo de periodico
Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers (2024)
Longo, Janice; Silva, Matheus Rodrigues; Santana, Humberto Brito; Ferreira, Antonio Joaquim Mendes; Tita, Volnei ; Medeiros, Ricardo de
Source: Composite Structures. Unidade: EESC
Subjects: PIEZOELETRICIDADE, MÉTODO DOS ELEMENTOS FINITOS, ATUADORES PIEZELÉTRICOS, ENGENHARIA AERONÁUTICA
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ABNT
LONGO, Janice et al. Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers. Composite Structures, v. 349-350, p. 1-9, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2024.118506. Acesso em: 17 nov. 2025.
APA
Longo, J., Silva, M. R., Santana, H. B., Ferreira, A. J. M., Tita, V., & Medeiros, R. de. (2024). Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers. Composite Structures, 349-350, 1-9. doi:10.1016/j.compstruct.2024.118506
NLM
Longo J, Silva MR, Santana HB, Ferreira AJM, Tita V, Medeiros R de. Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers [Internet]. Composite Structures. 2024 ; 349-350 1-9.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
Vancouver
Longo J, Silva MR, Santana HB, Ferreira AJM, Tita V, Medeiros R de. Development of a numerical and analytical methodology for analyzing hybrid laminates with multi-oriented piezoelectric and structural layers [Internet]. Composite Structures. 2024 ; 349-350 1-9.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
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
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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
Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE (2023)
Silva, Matheus Rodrigues; Tita, Volnei ; Medeiros, Ricardo de
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, PIEZOELETRICIDADE, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA
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ABNT
SILVA, Matheus Rodrigues e TITA, Volnei e MEDEIROS, Ricardo de. Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE. Composite Structures, v. 303, p. 1-12, 2023Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2022.116292. Acesso em: 17 nov. 2025.
APA
Silva, M. R., Tita, V., & Medeiros, R. de. (2023). Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE. Composite Structures, 303, 1-12. doi:10.1016/j.compstruct.2022.116292
NLM
Silva MR, Tita V, Medeiros R de. Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE [Internet]. Composite Structures. 2023 ; 303 1-12.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2022.116292
Vancouver
Silva MR, Tita V, Medeiros R de. Influence of the geometric parameters on the effective properties of piezoelectric composite sensors using real measurements and a new RVE [Internet]. Composite Structures. 2023 ; 303 1-12.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2022.116292
Artigo de periodico
Calibration of group effect parameters through genetic algorithms for micromechanical modeling of UHPFRC (2022)
Ribeiro, Paula de Oliveira; Krahl, Pablo Augusto; Carrazedo, Ricardo
Source: Composite Structures. Unidade: EESC
Subjects: CONCRETO DE ALTA RESISTÊNCIA, CONCRETO REFORÇADO COM FIBRAS, CONCRETO REFORÇADO COM FIBRAS, ESTRUTURAS
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ABNT
RIBEIRO, Paula de Oliveira e KRAHL, Pablo Augusto e CARRAZEDO, Ricardo. Calibration of group effect parameters through genetic algorithms for micromechanical modeling of UHPFRC. Composite Structures, v. 280, p. 1-14, 2022Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2021.114933. Acesso em: 17 nov. 2025.
APA
Ribeiro, P. de O., Krahl, P. A., & Carrazedo, R. (2022). Calibration of group effect parameters through genetic algorithms for micromechanical modeling of UHPFRC. Composite Structures, 280, 1-14. doi:10.1016/j.compstruct.2021.114933
NLM
Ribeiro P de O, Krahl PA, Carrazedo R. Calibration of group effect parameters through genetic algorithms for micromechanical modeling of UHPFRC [Internet]. Composite Structures. 2022 ; 280 1-14.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2021.114933
Vancouver
Ribeiro P de O, Krahl PA, Carrazedo R. Calibration of group effect parameters through genetic algorithms for micromechanical modeling of UHPFRC [Internet]. Composite Structures. 2022 ; 280 1-14.[citado 2025 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2021.114933
Artigo de periodico
Bond-slip response of steel fibers after exposure to elevated temperatures: experimental program and design-oriented constitutive equation (2021)
Serafini, Ramoel ; Agra, Ronney Rodrigues ; Bitencourt Júnior, Luís Antônio Guimarães ; Fuente Antequera, Albert de La ; Figueiredo, Antonio Domingues de
Source: Composite Structures. Unidade: EP
Subjects: CONCRETO REFORÇADO COM FIBRAS, CIMENTO REFORÇADO COM FIBRAS
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ABNT
SERAFINI, Ramoel et al. Bond-slip response of steel fibers after exposure to elevated temperatures: experimental program and design-oriented constitutive equation. Composite Structures, v. 255, n. 1 Ja 2021, p. 17 on-line, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2020.112916. Acesso em: 17 nov. 2025.
APA
Serafini, R., Agra, R. R., Bitencourt Júnior, L. A. G., Fuente Antequera, A. de L., & Figueiredo, A. D. de. (2021). Bond-slip response of steel fibers after exposure to elevated temperatures: experimental program and design-oriented constitutive equation. Composite Structures, 255( 1 Ja 2021), 17 on-line. doi:10.1016/j.compstruct.2020.112916
NLM
Serafini R, Agra RR, Bitencourt Júnior LAG, Fuente Antequera A de L, Figueiredo AD de. Bond-slip response of steel fibers after exposure to elevated temperatures: experimental program and design-oriented constitutive equation [Internet]. Composite Structures. 2021 ; 255( 1 Ja 2021): 17 on-line.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112916
Vancouver
Serafini R, Agra RR, Bitencourt Júnior LAG, Fuente Antequera A de L, Figueiredo AD de. Bond-slip response of steel fibers after exposure to elevated temperatures: experimental program and design-oriented constitutive equation [Internet]. Composite Structures. 2021 ; 255( 1 Ja 2021): 17 on-line.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112916
Artigo de periodico
Design of SFRC members aided by a multiscale model: part I – predicting the post-cracking parameters (2020)
Trindade, Yasmin Teixeira ; Bitencourt Júnior, Luís Antônio Guimarães ; Monte, Renata ; Figueiredo, Antonio Domingues de ; Manzoli, Osvaldo Luis
Source: Composite Structures. Unidade: EP
Subjects: CONCRETO REFORÇADO COM FIBRAS, VIGAS
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ABNT
TRINDADE, Yasmin Teixeira et al. Design of SFRC members aided by a multiscale model: part I – predicting the post-cracking parameters. Composite Structures, v. 241, p. com 14 , 2020Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2020.112078. Acesso em: 17 nov. 2025.
APA
Trindade, Y. T., Bitencourt Júnior, L. A. G., Monte, R., Figueiredo, A. D. de, & Manzoli, O. L. (2020). Design of SFRC members aided by a multiscale model: part I – predicting the post-cracking parameters. Composite Structures, 241, com 14 . doi:10.1016/j.compstruct.2020.112078
NLM
Trindade YT, Bitencourt Júnior LAG, Monte R, Figueiredo AD de, Manzoli OL. Design of SFRC members aided by a multiscale model: part I – predicting the post-cracking parameters [Internet]. Composite Structures. 2020 ; 241 com 14 .[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112078
Vancouver
Trindade YT, Bitencourt Júnior LAG, Monte R, Figueiredo AD de, Manzoli OL. Design of SFRC members aided by a multiscale model: part I – predicting the post-cracking parameters [Internet]. Composite Structures. 2020 ; 241 com 14 .[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112078
Artigo de periodico
On the modeling of nonlinear supersonic flutter of multibay composite panels (2020)
Guimarães, Thiago A. M.; Marques, Flavio Donizeti ; Ferreira, Antonio J. M
Source: Composite Structures. Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, MATERIAIS COMPÓSITOS, PAINÉIS, ESTRUTURAS
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ABNT
GUIMARÃES, Thiago A. M. e MARQUES, Flavio Donizeti e FERREIRA, Antonio J. M. On the modeling of nonlinear supersonic flutter of multibay composite panels. Composite Structures, v. 232, n. Ja 2020, p. 1-6, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2019.111522. Acesso em: 17 nov. 2025.
APA
Guimarães, T. A. M., Marques, F. D., & Ferreira, A. J. M. (2020). On the modeling of nonlinear supersonic flutter of multibay composite panels. Composite Structures, 232( Ja 2020), 1-6. doi:10.1016/j.compstruct.2019.111522
NLM
Guimarães TAM, Marques FD, Ferreira AJM. On the modeling of nonlinear supersonic flutter of multibay composite panels [Internet]. Composite Structures. 2020 ; 232( Ja 2020): 1-6.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2019.111522
Vancouver
Guimarães TAM, Marques FD, Ferreira AJM. On the modeling of nonlinear supersonic flutter of multibay composite panels [Internet]. Composite Structures. 2020 ; 232( Ja 2020): 1-6.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2019.111522
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
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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 and numerical dynamic analysis of laminate plates via Carrera Unified Formulation (2018)
Ribeiro, Marcelo Leite ; Ferreira, Gregório Felipe Oliveira; Medeiros, Ricardo de; Ferreira, Antonio Joaquim Mendes; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, VIBRAÇÕES, ENGENHARIA AERONÁUTICA
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ABNT
RIBEIRO, Marcelo Leite et al. Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation. Composite Structures, v. 202, p. 1176-1185, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2018.05.085. Acesso em: 17 nov. 2025.
APA
Ribeiro, M. L., Ferreira, G. F. O., Medeiros, R. de, Ferreira, A. J. M., & Tita, V. (2018). Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation. Composite Structures, 202, 1176-1185. doi:10.1016/j.compstruct.2018.05.085
NLM
Ribeiro ML, Ferreira GFO, Medeiros R de, Ferreira AJM, Tita V. Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation [Internet]. Composite Structures. 2018 ; 202 1176-1185.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
Vancouver
Ribeiro ML, Ferreira GFO, Medeiros R de, Ferreira AJM, Tita V. Experimental and numerical dynamic analysis of laminate plates via Carrera Unified Formulation [Internet]. Composite Structures. 2018 ; 202 1176-1185.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
Artigo de periodico
Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage (2017)
Almeida Júnior, José Humberto Santos; Ribeiro, Marcelo Leite ; Tita, Volnei ; Amico, Sandro Campos
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, ALGORITMOS GENÉTICOS, MATERIAIS COMPÓSITOS, FALHA, ENGENHARIA AERONÁUTICA
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ABNT
ALMEIDA JÚNIOR, José Humberto Santos et al. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage. Composite Structures, v. 178, p. 20-26, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.07.054. Acesso em: 17 nov. 2025.
APA
Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2017). Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage. Composite Structures, 178, 20-26. doi:10.1016/j.compstruct.2017.07.054
NLM
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage [Internet]. Composite Structures. 2017 ; 178 20-26.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
Vancouver
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Stacking sequence optimization in composite tubes under internal pressure based on genetic algorithm accounting for progressive damage [Internet]. Composite Structures. 2017 ; 178 20-26.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.07.054
Artigo de periodico
Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression (2017)
Almeida Júnior, José Humberto Santos; Ribeiro, Marcelo Leite ; Tita, Volnei ; Amico, Sandro Campos
Source: Composite Structures. Unidade: EESC
Subjects: ANÁLISE NUMÉRICA, FALHA, MÉTODO DOS ELEMENTOS FINITOS
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ABNT
ALMEIDA JÚNIOR, José Humberto Santos et al. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression. Composite Structures, v. 160, n. Ja 2017, p. 204-210, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.10.036. Acesso em: 17 nov. 2025.
APA
Almeida Júnior, J. H. S., Ribeiro, M. L., Tita, V., & Amico, S. C. (2017). Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression. Composite Structures, 160( Ja 2017), 204-210. doi:10.1016/j.compstruct.2016.10.036
NLM
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression [Internet]. Composite Structures. 2017 ; 160( Ja 2017): 204-210.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.036
Vancouver
Almeida Júnior JHS, Ribeiro ML, Tita V, Amico SC. Damage modeling for carbon fiber/epoxy filament wound composite tubes under radial compression [Internet]. Composite Structures. 2017 ; 160( Ja 2017): 204-210.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.036

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