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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: 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
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: 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
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: 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
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: 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
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: 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
Fonte: Composite Structures. Unidade: EESC
Assuntos: 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
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: 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
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: 17 nov. 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 nov. 17 ] 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 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2023.117528
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.
Fonte: Composite Structures. Unidade: EESC
Assuntos: PIEZOELETRICIDADE, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 17 nov. 2025.
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 2025 nov. 17 ] 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 2025 nov. 17 ] 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
Fonte: Composite Structures. Unidade: EESC
Assuntos: 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: 17 nov. 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 nov. 17 ] 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 nov. 17 ] 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: 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
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
Fonte: Composite Structures. Unidade: EESC
Assuntos: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, VIBRAÇÕES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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
Fonte: Composite Structures. Unidade: EESC
Assuntos: 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

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