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Artigo de periodico
A review on bistable composite laminates for aerospace applications (2024)
Lemos, Diego Magela; Marques, Flavio Donizeti ; Ferreira, Antonio Joaquim Mendes
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 17 nov. 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 nov. 17 ] 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 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117756
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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
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
Vibro-acoustic performance of graded piezoelectric metamaterial plates (2024)
Schimidt, Camila Sanches; Oliveira, Leopoldo Pisanelli Rodrigues de ; De Marqui Júnior, Carlos
Source: Composite Structures. Unidade: EESC
Subjects: PIEZOELETRICIDADE, MATERIAIS, ACÚSTICA, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 17 nov. 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 nov. 17 ] 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 nov. 17 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117656

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