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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
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
Source: Composite Structures. Unidade: EESC
Subjects: 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: 17 nov. 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 nov. 17 ] 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 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2022.115606
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
Source: Composite Structures. Unidade: EESC
Subjects: 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: 17 nov. 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 nov. 17 ] 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 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
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
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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
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
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, PAINÉIS SANDWICH, ESTRUTURAS
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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: 17 nov. 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 nov. 17 ] 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 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112254
Artigo de periodico
Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout (2019)
Almeida Júnior, José Humberto Santos; Bittrich, Lars; Jansen, Eelco; Tita, Volnei ; Spickenheuer, Axel
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS
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ABNT
ALMEIDA JÚNIOR, José Humberto Santos et al. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout. Composite Structures, v. 222, p. 1-12, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2019.110928. Acesso em: 17 nov. 2025.
APA
Almeida Júnior, J. H. S., Bittrich, L., Jansen, E., Tita, V., & Spickenheuer, A. (2019). Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout. Composite Structures, 222, 1-12. doi:10.1016/j.compstruct.2019.110928
NLM
Almeida Júnior JHS, Bittrich L, Jansen E, Tita V, Spickenheuer A. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout [Internet]. Composite Structures. 2019 ; 222 1-12.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2019.110928
Vancouver
Almeida Júnior JHS, Bittrich L, Jansen E, Tita V, Spickenheuer A. Buckling optimization of composite cylinders for axial compression: A design methodology considering a variable-axial fiber layout [Internet]. Composite Structures. 2019 ; 222 1-12.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2019.110928
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
Active face prismatic positional finite element for linear and geometrically nonlinear analysis of honeycomb sandwich plates and shells (2018)
Carrazedo, Rogério ; Paccola, Rodrigo Ribeiro ; Coda, Humberto Breves
Source: Composite Structures. Unidade: EESC
Subjects: ANÁLISE NÃO LINEAR DE ESTRUTURAS, MÉTODO DOS ELEMENTOS FINITOS, ESTRUTURAS
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ABNT
CARRAZEDO, Rogério e PACCOLA, Rodrigo Ribeiro e CODA, Humberto Breves. Active face prismatic positional finite element for linear and geometrically nonlinear analysis of honeycomb sandwich plates and shells. Composite Structures, v. 200, p. 849-863, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2018.06.009. Acesso em: 17 nov. 2025.
APA
Carrazedo, R., Paccola, R. R., & Coda, H. B. (2018). Active face prismatic positional finite element for linear and geometrically nonlinear analysis of honeycomb sandwich plates and shells. Composite Structures, 200, 849-863. doi:10.1016/j.compstruct.2018.06.009
NLM
Carrazedo R, Paccola RR, Coda HB. Active face prismatic positional finite element for linear and geometrically nonlinear analysis of honeycomb sandwich plates and shells [Internet]. Composite Structures. 2018 ; 200 849-863.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2018.06.009
Vancouver
Carrazedo R, Paccola RR, Coda HB. Active face prismatic positional finite element for linear and geometrically nonlinear analysis of honeycomb sandwich plates and shells [Internet]. Composite Structures. 2018 ; 200 849-863.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2018.06.009
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
Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime (2017)
Pacheco, D. R. Q.; Marques, Flavio Donizeti ; Natarajan, S.; Ferreira, A. J. M.
Source: Composite Structures. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
PACHECO, D. R. Q. et al. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime. Composite Structures, v. 180, p. 883-891, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.08.058. Acesso em: 17 nov. 2025.
APA
Pacheco, D. R. Q., Marques, F. D., Natarajan, S., & Ferreira, A. J. M. (2017). Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime. Composite Structures, 180, 883-891. doi:10.1016/j.compstruct.2017.08.058
NLM
Pacheco DRQ, Marques FD, Natarajan S, Ferreira AJM. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime [Internet]. Composite Structures. 2017 ; 180 883-891.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.08.058
Vancouver
Pacheco DRQ, Marques FD, Natarajan S, Ferreira AJM. Nonlinear finite element post-flutter analysis of multibay composite panels in supersonic regime [Internet]. Composite Structures. 2017 ; 180 883-891.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.08.058
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
Artigo de periodico
Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells (2017)
Carrazedo, Rogério ; Coda, Humberto Breves
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, VIGAS, LAMINADOS, ESTRUTURAS
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ABNT
CARRAZEDO, Rogério e CODA, Humberto Breves. Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells. Composite Structures, v. 168, p. 234-246, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.02.027. Acesso em: 17 nov. 2025.
APA
Carrazedo, R., & Coda, H. B. (2017). Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells. Composite Structures, 168, 234-246. doi:10.1016/j.compstruct.2017.02.027
NLM
Carrazedo R, Coda HB. Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells [Internet]. Composite Structures. 2017 ; 168 234-246.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.02.027
Vancouver
Carrazedo R, Coda HB. Triangular based prismatic finite element for the analysis of orthotropic laminated beams, plates and shells [Internet]. Composite Structures. 2017 ; 168 234-246.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2017.02.027
Artigo de periodico
Finite element characterisation of multilayer d31 piezoelectric macro-fibre composites (2016)
Trindade, Marcelo Areias ; Benjeddou, Ayech
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS DE FIBRAS, PIEZOELETRICIDADE, MÉTODO DOS ELEMENTOS FINITOS
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ABNT
TRINDADE, Marcelo Areias e BENJEDDOU, Ayech. Finite element characterisation of multilayer d31 piezoelectric macro-fibre composites. Composite Structures, v. 151, p. 47-57, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2015.10.011. Acesso em: 17 nov. 2025.
APA
Trindade, M. A., & Benjeddou, A. (2016). Finite element characterisation of multilayer d31 piezoelectric macro-fibre composites. Composite Structures, 151, 47-57. doi:10.1016/j.compstruct.2015.10.011
NLM
Trindade MA, Benjeddou A. Finite element characterisation of multilayer d31 piezoelectric macro-fibre composites [Internet]. Composite Structures. 2016 ; 151 47-57.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2015.10.011
Vancouver
Trindade MA, Benjeddou A. Finite element characterisation of multilayer d31 piezoelectric macro-fibre composites [Internet]. Composite Structures. 2016 ; 151 47-57.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2015.10.011
Artigo de periodico
A direct FEM approach for particulate reinforced elastic solids (2016)
Paccola, Rodrigo Ribeiro ; Coda, Humberto Breves
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, ESTRUTURAS, ELASTICIDADE DAS ESTRUTURAS
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ABNT
PACCOLA, Rodrigo Ribeiro e CODA, Humberto Breves. A direct FEM approach for particulate reinforced elastic solids. Composite Structures, v. 141, p. 282-291, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.01.062. Acesso em: 17 nov. 2025.
APA
Paccola, R. R., & Coda, H. B. (2016). A direct FEM approach for particulate reinforced elastic solids. Composite Structures, 141, 282-291. doi:10.1016/j.compstruct.2016.01.062
NLM
Paccola RR, Coda HB. A direct FEM approach for particulate reinforced elastic solids [Internet]. Composite Structures. 2016 ; 141 282-291.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.01.062
Vancouver
Paccola RR, Coda HB. A direct FEM approach for particulate reinforced elastic solids [Internet]. Composite Structures. 2016 ; 141 282-291.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.01.062
Artigo de periodico
A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method (2016)
Caliri Junior, Mauricio Francisco; Ferreira, António Joaquim Mendes; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, MÉTODO DOS ELEMENTOS FINITOS
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ABNT
CALIRI JUNIOR, Mauricio Francisco e FERREIRA, António Joaquim Mendes e TITA, Volnei. A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method. Composite Structures, v. No 2016, p. 63-77, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.02.036. Acesso em: 17 nov. 2025.
APA
Caliri Junior, M. F., Ferreira, A. J. M., & Tita, V. (2016). A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method. Composite Structures, No 2016, 63-77. doi:10.1016/j.compstruct.2016.02.036
NLM
Caliri Junior MF, Ferreira AJM, Tita V. A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method [Internet]. Composite Structures. 2016 ; No 2016 63-77.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.036
Vancouver
Caliri Junior MF, Ferreira AJM, Tita V. A review on plate and shell theories for laminated and sandwich structures highlighting the finite element method [Internet]. Composite Structures. 2016 ; No 2016 63-77.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.036
Artigo de periodico
Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion (2016)
Santana, Humberto Brito; Medeiros, Ricardo de; Rodríguez Ramos, Reinaldo; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: PIEZOELETRICIDADE, MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SANTANA, Humberto Brito et al. Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion. Composite Structures, v. 151, p. 70-80, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.02.003. Acesso em: 17 nov. 2025.
APA
Santana, H. B., Medeiros, R. de, Rodríguez Ramos, R., & Tita, V. (2016). Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion. Composite Structures, 151, 70-80. doi:10.1016/j.compstruct.2016.02.003
NLM
Santana HB, Medeiros R de, Rodríguez Ramos R, Tita V. Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion [Internet]. Composite Structures. 2016 ; 151 70-80.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.003
Vancouver
Santana HB, Medeiros R de, Rodríguez Ramos R, Tita V. Different interface models for calculating the effective properties in piezoelectric composite materials with imperfect fiber-matrix adhesion [Internet]. Composite Structures. 2016 ; 151 70-80.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.02.003
Artigo de periodico
A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation (2015)
Sartorato, Murilo; Medeiros, Ricardo de; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, ATUADORES PIEZELÉTRICOS, MATERIAIS COMPÓSITOS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SARTORATO, Murilo e MEDEIROS, Ricardo de e TITA, Volnei. A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation. Composite Structures, v. 127, p. 185-198, 2015Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2015.03.009. Acesso em: 17 nov. 2025.
APA
Sartorato, M., Medeiros, R. de, & Tita, V. (2015). A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation. Composite Structures, 127, 185-198. doi:10.1016/j.compstruct.2015.03.009
NLM
Sartorato M, Medeiros R de, Tita V. A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation [Internet]. Composite Structures. 2015 ; 127 185-198.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2015.03.009
Vancouver
Sartorato M, Medeiros R de, Tita V. A finite element formulation for smart piezoelectric composite shells: mathematical formulation, computational analysis and experimental evaluation [Internet]. Composite Structures. 2015 ; 127 185-198.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2015.03.009
Artigo de periodico
A geometrically nonlinear FEM formulation for the analysis of fiber reinforced laminated plates and shells (2015)
Sampaio, Maria do Socorro Martins; Paccola, Rodrigo Ribeiro ; Coda, Humberto Breves
Source: Composite Structures. Unidade: EESC
Subjects: ANÁLISE NÃO LINEAR DE ESTRUTURAS, MÉTODO DOS ELEMENTOS FINITOS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SAMPAIO, Maria do Socorro Martins e PACCOLA, Rodrigo Ribeiro e CODA, Humberto Breves. A geometrically nonlinear FEM formulation for the analysis of fiber reinforced laminated plates and shells. Composite Structures, v. 119, n. Ja 2015, p. 799-814, 2015Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2014.09.009. Acesso em: 17 nov. 2025.
APA
Sampaio, M. do S. M., Paccola, R. R., & Coda, H. B. (2015). A geometrically nonlinear FEM formulation for the analysis of fiber reinforced laminated plates and shells. Composite Structures, 119( Ja 2015), 799-814. doi:10.1016/j.compstruct.2014.09.009
NLM
Sampaio M do SM, Paccola RR, Coda HB. A geometrically nonlinear FEM formulation for the analysis of fiber reinforced laminated plates and shells [Internet]. Composite Structures. 2015 ; 119( Ja 2015): 799-814.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2014.09.009
Vancouver
Sampaio M do SM, Paccola RR, Coda HB. A geometrically nonlinear FEM formulation for the analysis of fiber reinforced laminated plates and shells [Internet]. Composite Structures. 2015 ; 119( Ja 2015): 799-814.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2014.09.009
Artigo de periodico
Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence (2013)
Rodríguez-Ramos, Reinaldo; Medeiros, Ricardo de; Guinovart-Díaz, Raúl; Bravo-Castillero, Julián; Otero, José Antonio; Tita, Volnei
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, HOMOGENEIZAÇÃO, MÉTODO DOS ELEMENTOS FINITOS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
RODRÍGUEZ-RAMOS, Reinaldo et al. Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence. Composite Structures, v. 99, p. 264-275, 2013Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2012.11.040. Acesso em: 17 nov. 2025.
APA
Rodríguez-Ramos, R., Medeiros, R. de, Guinovart-Díaz, R., Bravo-Castillero, J., Otero, J. A., & Tita, V. (2013). Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence. Composite Structures, 99, 264-275. doi:10.1016/j.compstruct.2012.11.040
NLM
Rodríguez-Ramos R, Medeiros R de, Guinovart-Díaz R, Bravo-Castillero J, Otero JA, Tita V. Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence [Internet]. Composite Structures. 2013 ; 99 264-275.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2012.11.040
Vancouver
Rodríguez-Ramos R, Medeiros R de, Guinovart-Díaz R, Bravo-Castillero J, Otero JA, Tita V. Different approaches for calculating the effective elastic properties in composite materials under imperfect contact adherence [Internet]. Composite Structures. 2013 ; 99 264-275.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2012.11.040

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