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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
Fonte: 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: 07 out. 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 out. 07 ] 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 out. 07 ] 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
Fonte: 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: 07 out. 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 out. 07 ] 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 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119427
Artigo de periodico
A smoothed Zig-Zag plate finite element for the analysis of laminated composite plates (2025)
Souza, Vinicius de Barros ; Fantuzzi, Nicholas ; Coda, Humberto Breves
Fonte: Composite Structures. Unidade: EESC
Assunto: ESTRUTURAS
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ABNT
SOUZA, Vinicius de Barros e FANTUZZI, Nicholas e CODA, Humberto Breves. A smoothed Zig-Zag plate finite element for the analysis of laminated composite plates. Composite Structures, v. 371, p. 1-25, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2025.119412. Acesso em: 07 out. 2025.
APA
Souza, V. de B., Fantuzzi, N., & Coda, H. B. (2025). A smoothed Zig-Zag plate finite element for the analysis of laminated composite plates. Composite Structures, 371, 1-25. doi:10.1016/j.compstruct.2025.119412
NLM
Souza V de B, Fantuzzi N, Coda HB. A smoothed Zig-Zag plate finite element for the analysis of laminated composite plates [Internet]. Composite Structures. 2025 ; 371 1-25.[citado 2025 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119412
Vancouver
Souza V de B, Fantuzzi N, Coda HB. A smoothed Zig-Zag plate finite element for the analysis of laminated composite plates [Internet]. Composite Structures. 2025 ; 371 1-25.[citado 2025 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119412
Artigo de periodico
Statistical reconstruction through simulated annealing for the generation of composite microstructures (2025)
Urzedo Quirino, Matheus ; Ribeiro, Marcelo Leite
Fonte: Composite Structures. Unidade: EESC
Assunto: ESTRUTURAS
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ABNT
URZEDO QUIRINO, Matheus e RIBEIRO, Marcelo Leite. Statistical reconstruction through simulated annealing for the generation of composite microstructures. Composite Structures, v. 373, p. 1-14, 2025Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2025.119619. Acesso em: 07 out. 2025.
APA
Urzedo Quirino, M., & Ribeiro, M. L. (2025). Statistical reconstruction through simulated annealing for the generation of composite microstructures. Composite Structures, 373, 1-14. doi:10.1016/j.compstruct.2025.119619
NLM
Urzedo Quirino M, Ribeiro ML. Statistical reconstruction through simulated annealing for the generation of composite microstructures [Internet]. Composite Structures. 2025 ; 373 1-14.[citado 2025 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119619
Vancouver
Urzedo Quirino M, Ribeiro ML. Statistical reconstruction through simulated annealing for the generation of composite microstructures [Internet]. Composite Structures. 2025 ; 373 1-14.[citado 2025 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2025.119619
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
Fonte: 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: 07 out. 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 out. 07 ] 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 out. 07 ] 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
Fonte: Composite Structures. Unidade: EESC
Assuntos: 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: 07 out. 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 out. 07 ] 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 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
Artigo de periodico
A review on bistable composite laminates for aerospace applications (2024)
Lemos, Diego Magela; Marques, Flavio Donizeti ; Ferreira, Antonio Joaquim Mendes
Fonte: Composite Structures. Unidade: EESC
Assuntos: MATERIAIS COMPÓSITOS, LAMINADOS, ENGENHARIA MECÂNICA
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ABNT
LEMOS, Diego Magela e MARQUES, Flavio Donizeti e FERREIRA, Antonio Joaquim Mendes. A review on bistable composite laminates for aerospace applications. Composite Structures, v. 329, p. 1-21, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2023.117756. Acesso em: 07 out. 2025.
APA
Lemos, D. M., Marques, F. D., & Ferreira, A. J. M. (2024). A review on bistable composite laminates for aerospace applications. Composite Structures, 329, 1-21. doi:10.1016/j.compstruct.2023.117756
NLM
Lemos DM, Marques FD, Ferreira AJM. A review on bistable composite laminates for aerospace applications [Internet]. Composite Structures. 2024 ; 329 1-21.[citado 2025 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117756
Vancouver
Lemos DM, Marques FD, Ferreira AJM. A review on bistable composite laminates for aerospace applications [Internet]. Composite Structures. 2024 ; 329 1-21.[citado 2025 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117756
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
Fonte: Composite Structures. Unidade: EESC
Assuntos: MATERIAIS COMPÓSITOS, FUSELAGEM DE AERONAVES, DANO, ESTRUTURA DE AERONAVES, ENGENHARIA AERONÁUTICA
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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: 07 out. 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 out. 07 ] 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 out. 07 ] 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
Fonte: Composite Structures. Unidade: EESC
Assuntos: 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: 07 out. 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 out. 07 ] 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 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2024.118506
Artigo de periodico
Vibro-acoustic performance of graded piezoelectric metamaterial plates (2024)
Schimidt, Camila Sanches; Oliveira, Leopoldo Pisanelli Rodrigues de ; De Marqui Júnior, Carlos
Fonte: Composite Structures. Unidade: EESC
Assuntos: PIEZOELETRICIDADE, MATERIAIS, ACÚSTICA, ENGENHARIA MECÂNICA
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ABNT
SCHIMIDT, Camila Sanches e OLIVEIRA, Leopoldo Pisanelli Rodrigues de e DE MARQUI JÚNIOR, Carlos. Vibro-acoustic performance of graded piezoelectric metamaterial plates. Composite Structures, v. 327, p. 1-10, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2023.117656. Acesso em: 07 out. 2025.
APA
Schimidt, C. S., Oliveira, L. P. R. de, & De Marqui Júnior, C. (2024). Vibro-acoustic performance of graded piezoelectric metamaterial plates. Composite Structures, 327, 1-10. doi:10.1016/j.compstruct.2023.117656
NLM
Schimidt CS, Oliveira LPR de, De Marqui Júnior C. Vibro-acoustic performance of graded piezoelectric metamaterial plates [Internet]. Composite Structures. 2024 ; 327 1-10.[citado 2025 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117656
Vancouver
Schimidt CS, Oliveira LPR de, De Marqui Júnior C. Vibro-acoustic performance of graded piezoelectric metamaterial plates [Internet]. Composite Structures. 2024 ; 327 1-10.[citado 2025 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117656
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
Fonte: Composite Structures. Unidade: EESC
Assuntos: 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: 07 out. 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 out. 07 ] 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 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2022.116292
Artigo de periodico
Data reduction methods in the fatigue analysis of the Double Cantilever Beam, Part II: evaluation and case studies (2023)
Marques, Denys; Madureira, Fernando; Tita, Volnei
Fonte: Composite Structures. Unidade: EESC
Assuntos: FADIGA DOS MATERIAIS, JUNTAS ESTRUTURAIS, ENGENHARIA AERONÁUTICA
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ABNT
MARQUES, Denys e MADUREIRA, Fernando e TITA, Volnei. Data reduction methods in the fatigue analysis of the Double Cantilever Beam, Part II: evaluation and case studies. Composite Structures, v. 324, p. 1-11, 2023Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2023.117528. Acesso em: 07 out. 2025.
APA
Marques, D., Madureira, F., & Tita, V. (2023). Data reduction methods in the fatigue analysis of the Double Cantilever Beam, Part II: evaluation and case studies. Composite Structures, 324, 1-11. doi:10.1016/j.compstruct.2023.117528
NLM
Marques D, Madureira F, Tita V. Data reduction methods in the fatigue analysis of the Double Cantilever Beam, Part II: evaluation and case studies [Internet]. Composite Structures. 2023 ; 324 1-11.[citado 2025 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2023.117528
Vancouver
Marques D, Madureira F, Tita V. Data reduction methods in the fatigue analysis of the Double Cantilever Beam, Part II: evaluation and case studies [Internet]. Composite Structures. 2023 ; 324 1-11.[citado 2025 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2023.117528
Artigo de periodico
Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels (2022)
Cabral, Myrella Vieira; Marques, Flavio Donizeti ; Ferreira, Antonio J. M
Fonte: Composite Structures. Unidade: EESC
Assuntos: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA MECÂNICA
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ABNT
CABRAL, Myrella Vieira e MARQUES, Flavio Donizeti e FERREIRA, Antonio J. M. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels. Composite Structures, v. 286, p. 1-15, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2021.115128. Acesso em: 07 out. 2025.
APA
Cabral, M. V., Marques, F. D., & Ferreira, A. J. M. (2022). Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels. Composite Structures, 286, 1-15. doi:10.1016/j.compstruct.2021.115128
NLM
Cabral MV, Marques FD, Ferreira AJM. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels [Internet]. Composite Structures. 2022 ; 286 1-15.[citado 2025 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
Vancouver
Cabral MV, Marques FD, Ferreira AJM. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels [Internet]. Composite Structures. 2022 ; 286 1-15.[citado 2025 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
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
Fonte: Composite Structures. Unidade: EESC
Assuntos: 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: 07 out. 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 out. 07 ] 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 out. 07 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2021.114933
Artigo de periodico
A FEM formulation for the analysis of laminated and functionally graded hyperelastic beams with continuous transverse shear stresses (2022)
Coda, Humberto Breves ; Bernardo, Caio César La-Cava Gonçalves; Paccola, Rodrigo Ribeiro
Fonte: Composite Structures. Unidade: EESC
Assuntos: VIGAS, CISALHAMENTO, MÉTODO DOS ELEMENTOS FINITOS, TENSÃO ESTRUTURAL, ESTRUTURAS
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ABNT
CODA, Humberto Breves e BERNARDO, Caio César La-Cava Gonçalves e PACCOLA, Rodrigo Ribeiro. A FEM formulation for the analysis of laminated and functionally graded hyperelastic beams with continuous transverse shear stresses. Composite Structures, v. 292, p. 1-17, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2022.115606. Acesso em: 07 out. 2025.
APA
Coda, H. B., Bernardo, C. C. L. -C. G., & Paccola, R. R. (2022). A FEM formulation for the analysis of laminated and functionally graded hyperelastic beams with continuous transverse shear stresses. Composite Structures, 292, 1-17. doi:10.1016/j.compstruct.2022.115606
NLM
Coda HB, Bernardo CCL-CG, Paccola RR. A FEM formulation for the analysis of laminated and functionally graded hyperelastic beams with continuous transverse shear stresses [Internet]. Composite Structures. 2022 ; 292 1-17.[citado 2025 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2022.115606
Vancouver
Coda HB, Bernardo CCL-CG, Paccola RR. A FEM formulation for the analysis of laminated and functionally graded hyperelastic beams with continuous transverse shear stresses [Internet]. Composite Structures. 2022 ; 292 1-17.[citado 2025 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2022.115606
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
Fonte: Composite Structures. Unidade: EP
Assuntos: 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: 07 out. 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 out. 07 ] 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 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112916
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
Fonte: Composite Structures. Unidade: EESC
Assuntos: 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: 07 out. 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 out. 07 ] 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 out. 07 ] 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
Fonte: Composite Structures. Unidade: EESC
Assuntos: 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: 07 out. 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 out. 07 ] 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 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112974
Artigo de periodico
Topology optimization of fibers orientation in hyperelastic composite material (2020)
Silva, Andre Luis Ferreira da ; Salas Varela, Ruben Andres ; Silva, Emílio Carlos Nelli ; Reddy, J. N.
Fonte: Composite Structures. Unidade: EP
Assuntos: TOPOLOGIA, MATERIAIS COMPÓSITOS DE FIBRAS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SILVA, Andre Luis Ferreira da et al. Topology optimization of fibers orientation in hyperelastic composite material. Composite Structures, v. 232, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2019.111488. Acesso em: 07 out. 2025.
APA
Silva, A. L. F. da, Salas Varela, R. A., Silva, E. C. N., & Reddy, J. N. (2020). Topology optimization of fibers orientation in hyperelastic composite material. Composite Structures, 232. doi:10.1016/j.compstruct.2019.111488
NLM
Silva ALF da, Salas Varela RA, Silva ECN, Reddy JN. Topology optimization of fibers orientation in hyperelastic composite material [Internet]. Composite Structures. 2020 ; 232[citado 2025 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2019.111488
Vancouver
Silva ALF da, Salas Varela RA, Silva ECN, Reddy JN. Topology optimization of fibers orientation in hyperelastic composite material [Internet]. Composite Structures. 2020 ; 232[citado 2025 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2019.111488
Artigo de periodico
Vibration and stress analysis of orthotropic laminated panels by active face prismatic finite element (2020)
Carrazedo, Rogério ; Paccola, Rodrigo Ribeiro ; Coda, Humberto Breves ; Salomão, Rafael
Fonte: Composite Structures. Unidade: EESC
Assuntos: MÉTODO DOS ELEMENTOS FINITOS, PAINÉIS SANDWICH, ESTRUTURAS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CARRAZEDO, Rogério et al. Vibration and stress analysis of orthotropic laminated panels by active face prismatic finite element. Composite Structures, v. 244, p. 1-16, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2020.112254. Acesso em: 07 out. 2025.
APA
Carrazedo, R., Paccola, R. R., Coda, H. B., & Salomão, R. (2020). Vibration and stress analysis of orthotropic laminated panels by active face prismatic finite element. Composite Structures, 244, 1-16. doi:10.1016/j.compstruct.2020.112254
NLM
Carrazedo R, Paccola RR, Coda HB, Salomão R. Vibration and stress analysis of orthotropic laminated panels by active face prismatic finite element [Internet]. Composite Structures. 2020 ; 244 1-16.[citado 2025 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112254
Vancouver
Carrazedo R, Paccola RR, Coda HB, Salomão R. Vibration and stress analysis of orthotropic laminated panels by active face prismatic finite element [Internet]. Composite Structures. 2020 ; 244 1-16.[citado 2025 out. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112254

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