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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: 20 out. 2024.
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 2024 out. 20 ] 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 2024 out. 20 ] 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
Source: Composite Structures. Unidade: EESC
Subjects: 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: 20 out. 2024.
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 2024 out. 20 ] 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 2024 out. 20 ] 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
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: 20 out. 2024.
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 2024 out. 20 ] 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 2024 out. 20 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
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: 20 out. 2024.
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 2024 out. 20 ] 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 2024 out. 20 ] Available from: https://doi.org/10.1016/j.compstruct.2022.115606
Artigo de periodico
Prediction of effective properties for multilayered laminated composite with delamination: a multiscale methodology proposal (2022)
Guinovart Sanjuan, David; Rodríguez Ramos, R.; Vajravelu, K.; Mohapatra, R.; Guinovart Díaz, R; Brito Santana, H.; Tita, Volnei ; Sabina, F. J.
Source: Composite Structures. Unidade: EESC
Subjects: PIEZOELETRICIDADE, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA
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ABNT
GUINOVART SANJUAN, David et al. Prediction of effective properties for multilayered laminated composite with delamination: a multiscale methodology proposal. Composite Structures, v. 297, p. 1-12, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2022.115910. Acesso em: 20 out. 2024.
APA
Guinovart Sanjuan, D., Rodríguez Ramos, R., Vajravelu, K., Mohapatra, R., Guinovart Díaz, R., Brito Santana, H., et al. (2022). Prediction of effective properties for multilayered laminated composite with delamination: a multiscale methodology proposal. Composite Structures, 297, 1-12. doi:10.1016/j.compstruct.2022.115910
NLM
Guinovart Sanjuan D, Rodríguez Ramos R, Vajravelu K, Mohapatra R, Guinovart Díaz R, Brito Santana H, Tita V, Sabina FJ. Prediction of effective properties for multilayered laminated composite with delamination: a multiscale methodology proposal [Internet]. Composite Structures. 2022 ; 297 1-12.[citado 2024 out. 20 ] Available from: https://doi.org/10.1016/j.compstruct.2022.115910
Vancouver
Guinovart Sanjuan D, Rodríguez Ramos R, Vajravelu K, Mohapatra R, Guinovart Díaz R, Brito Santana H, Tita V, Sabina FJ. Prediction of effective properties for multilayered laminated composite with delamination: a multiscale methodology proposal [Internet]. Composite Structures. 2022 ; 297 1-12.[citado 2024 out. 20 ] Available from: https://doi.org/10.1016/j.compstruct.2022.115910
Artigo de periodico
Novel progressive failure model for quasi-orthotropic pultruded FRP structures: application to compact tension and web-crippling case studies (Part II) (2021)
Gonilha, Jose A.; Silvestre, Nuno; Correia, João R.; Tita, Volnei ; Fernandes, Lourenço Almeida
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS DE FIBRAS, DANO, ENGENHARIA AERONÁUTICA
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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: 20 out. 2024.
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 2024 out. 20 ] 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 2024 out. 20 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112973
Artigo de periodico
Novel progressive failure model for quasi-orthotropic pultruded FRP structures: formulation and calibration of parameters (Part I) (2021)
Gonilha, Jose A.; Silvestre, Nuno; Correia, João R.; Tita, Volnei ; Martins, David
Source: Composite Structures. Unidade: EESC
Subjects: DANO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA
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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: 20 out. 2024.
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 2024 out. 20 ] 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 2024 out. 20 ] 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: 20 out. 2024.
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 2024 out. 20 ] 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 2024 out. 20 ] 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: 20 out. 2024.
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 2024 out. 20 ] 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 2024 out. 20 ] 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: 20 out. 2024.
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 2024 out. 20 ] 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 2024 out. 20 ] Available from: https://doi.org/10.1016/j.compstruct.2018.05.085
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: 20 out. 2024.
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 2024 out. 20 ] 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 2024 out. 20 ] Available from: https://doi.org/10.1016/j.compstruct.2017.08.058

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