Filtros : "Financiado pela CAPES" "ENGENHARIA AERONÁUTICA" Removido: "Mastelaro, Valmor Roberto" Limpar

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  • Source: Composites Science and Technology. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, IMPRESSÃO 3-D, TOPOLOGIA, MANUFATURA ADITIVA, ENGENHARIA AERONÁUTICA

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      ALMEIDA JÚNIOR, José Humberto Santos et al. A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites. Composites Science and Technology, v. 232, p. 1-15, 2023Tradução . . Disponível em: https://doi.org/10.1016/j.compscitech.2022.109872. Acesso em: 03 nov. 2025.
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      Almeida Júnior, J. H. S., Christoff, B. G., Tita, V., & St-Pierre, L. (2023). A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites. Composites Science and Technology, 232, 1-15. doi:10.1016/j.compscitech.2022.109872
    • NLM

      Almeida Júnior JHS, Christoff BG, Tita V, St-Pierre L. A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites [Internet]. Composites Science and Technology. 2023 ; 232 1-15.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1016/j.compscitech.2022.109872
    • Vancouver

      Almeida Júnior JHS, Christoff BG, Tita V, St-Pierre L. A concurrent fibre orientation and topology optimisation framework for 3D-printed fibre-reinforced composites [Internet]. Composites Science and Technology. 2023 ; 232 1-15.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1016/j.compscitech.2022.109872
  • Source: Polymers. Unidade: EESC

    Subjects: SUSTENTABILIDADE, POLÍMEROS (MATERIAIS), ENGENHARIA AERONÁUTICA

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      SILVA, Ênio Henrique Pires da et al. Accelerated aging on the compression properties of a green polyurethane foam: experimental and numerical analysis. Polymers, v. 15, n. 7, p. 1-18, 2023Tradução . . Disponível em: https://doi.org/10.3390/polym15071784. Acesso em: 03 nov. 2025.
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      Silva, Ê. H. P. da, Barros, S. de, Vieira, A. F. C., Costa, R. R. C. da, & Ribeiro, M. L. (2023). Accelerated aging on the compression properties of a green polyurethane foam: experimental and numerical analysis. Polymers, 15( 7), 1-18. doi:10.3390/polym15071784
    • NLM

      Silva ÊHP da, Barros S de, Vieira AFC, Costa RRC da, Ribeiro ML. Accelerated aging on the compression properties of a green polyurethane foam: experimental and numerical analysis [Internet]. Polymers. 2023 ; 15( 7): 1-18.[citado 2025 nov. 03 ] Available from: https://doi.org/10.3390/polym15071784
    • Vancouver

      Silva ÊHP da, Barros S de, Vieira AFC, Costa RRC da, Ribeiro ML. Accelerated aging on the compression properties of a green polyurethane foam: experimental and numerical analysis [Internet]. Polymers. 2023 ; 15( 7): 1-18.[citado 2025 nov. 03 ] Available from: https://doi.org/10.3390/polym15071784
  • Source: Journal of the Brazilian Society of Mechanical Sciences and Engineering. Unidade: EESC

    Subjects: MOBILIDADE URBANA, PANDEMIAS, COVID-19, SISTEMAS DINÂMICOS, AEROELASTICIDADE DE AERONAVES, PIEZOELETRICIDADE, ENERGIA, ENGENHARIA AERONÁUTICA

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      AMARAL, Ana Carolina Godoy e DE MARQUI JÚNIOR, Carlos e SILVEIRA, Marcos. Aeroelastic energy harvesting in futter condition increases with combined nonlinear stifness and nonlinear piezoelectrical coupling. Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 45, p. 1-14, 2023Tradução . . Disponível em: https://doi.org/10.1007/s40430-022-03783-6. Acesso em: 03 nov. 2025.
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      Amaral, A. C. G., De Marqui Júnior, C., & Silveira, M. (2023). Aeroelastic energy harvesting in futter condition increases with combined nonlinear stifness and nonlinear piezoelectrical coupling. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 45, 1-14. doi:10.1007/s40430-022-03783-6
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      Amaral ACG, De Marqui Júnior C, Silveira M. Aeroelastic energy harvesting in futter condition increases with combined nonlinear stifness and nonlinear piezoelectrical coupling [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2023 ; 45 1-14.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1007/s40430-022-03783-6
    • Vancouver

      Amaral ACG, De Marqui Júnior C, Silveira M. Aeroelastic energy harvesting in futter condition increases with combined nonlinear stifness and nonlinear piezoelectrical coupling [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2023 ; 45 1-14.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1007/s40430-022-03783-6
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, PIEZOELETRICIDADE, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

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      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: 03 nov. 2025.
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      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. 03 ] 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. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2022.116292
  • Source: Composite Structures. Unidade: EESC

    Subjects: FADIGA DOS MATERIAIS, JUNTAS ESTRUTURAIS, ENGENHARIA AERONÁUTICA

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      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: 03 nov. 2025.
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      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. 03 ] 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. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2023.117528
  • Source: Composites Part C: Open Access. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, MATERIAIS COMPÓSITOS, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

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      CHRISTOFF, Bruno Guilherme et al. Multiscale embedded models to determine effective mechanical properties of composite materials: asymptotic Homogenization Method combined to Finite Element Method. Composites Part C: Open Access, p. 1-14, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.jcomc.2022.100303. Acesso em: 03 nov. 2025.
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      Christoff, B. G., Brito Santana, H., Talreja, R., & Tita, V. (2022). Multiscale embedded models to determine effective mechanical properties of composite materials: asymptotic Homogenization Method combined to Finite Element Method. Composites Part C: Open Access, 1-14. doi:10.1016/j.jcomc.2022.100303
    • NLM

      Christoff BG, Brito Santana H, Talreja R, Tita V. Multiscale embedded models to determine effective mechanical properties of composite materials: asymptotic Homogenization Method combined to Finite Element Method [Internet]. Composites Part C: Open Access. 2022 ; 1-14.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1016/j.jcomc.2022.100303
    • Vancouver

      Christoff BG, Brito Santana H, Talreja R, Tita V. Multiscale embedded models to determine effective mechanical properties of composite materials: asymptotic Homogenization Method combined to Finite Element Method [Internet]. Composites Part C: Open Access. 2022 ; 1-14.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1016/j.jcomc.2022.100303
  • Source: Materials. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, LIGAS METÁLICAS, CORROSÃO, ENGENHARIA AERONÁUTICA

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      SACONI, Felipe et al. Experimental characterization and numerical modeling of the corrosion effect on the mechanical properties of the biodegradable magnesium alloy WE43 for orthopedic applications. Materials, v. 15, n. 20, p. 1-20, 2022Tradução . . Disponível em: https://doi.org/10.3390/ma15207164. Acesso em: 03 nov. 2025.
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      Saconi, F., Hincapie Diaz, G., Vieira, A. C., & Ribeiro, M. L. (2022). Experimental characterization and numerical modeling of the corrosion effect on the mechanical properties of the biodegradable magnesium alloy WE43 for orthopedic applications. Materials, 15( 20), 1-20. doi:10.3390/ma15207164
    • NLM

      Saconi F, Hincapie Diaz G, Vieira AC, Ribeiro ML. Experimental characterization and numerical modeling of the corrosion effect on the mechanical properties of the biodegradable magnesium alloy WE43 for orthopedic applications [Internet]. Materials. 2022 ; 15( 20): 1-20.[citado 2025 nov. 03 ] Available from: https://doi.org/10.3390/ma15207164
    • Vancouver

      Saconi F, Hincapie Diaz G, Vieira AC, Ribeiro ML. Experimental characterization and numerical modeling of the corrosion effect on the mechanical properties of the biodegradable magnesium alloy WE43 for orthopedic applications [Internet]. Materials. 2022 ; 15( 20): 1-20.[citado 2025 nov. 03 ] Available from: https://doi.org/10.3390/ma15207164
  • Source: Fatigue & Fracture of Engineering Materials and Structures. Unidade: EESC

    Subjects: FADIGA DAS ESTRUTURAS, ESTRUTURAS, ENGENHARIA AERONÁUTICA

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      MARQUES, Denys Eduardo Teixeira e VANDEPITTE, Dirk e TITA, Volnei. Sensitivity and uncertainty analysis for structural healthmonitoring with crack propagation under random loads: anumerical framework in the frequency domain. Fatigue & Fracture of Engineering Materials and Structures, p. 1-16, 2022Tradução . . Disponível em: https://doi.org/10.1111/ffe.13853. Acesso em: 03 nov. 2025.
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      Marques, D. E. T., Vandepitte, D., & Tita, V. (2022). Sensitivity and uncertainty analysis for structural healthmonitoring with crack propagation under random loads: anumerical framework in the frequency domain. Fatigue & Fracture of Engineering Materials and Structures, 1-16. doi:10.1111/ffe.13853
    • NLM

      Marques DET, Vandepitte D, Tita V. Sensitivity and uncertainty analysis for structural healthmonitoring with crack propagation under random loads: anumerical framework in the frequency domain [Internet]. Fatigue & Fracture of Engineering Materials and Structures. 2022 ; 1-16.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1111/ffe.13853
    • Vancouver

      Marques DET, Vandepitte D, Tita V. Sensitivity and uncertainty analysis for structural healthmonitoring with crack propagation under random loads: anumerical framework in the frequency domain [Internet]. Fatigue & Fracture of Engineering Materials and Structures. 2022 ; 1-16.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1111/ffe.13853
  • Source: Proceedings. Conference titles: Latin American Robotics Symposium - LARS. Unidade: EESC

    Subjects: SISTEMAS EMBUTIDOS, SISTEMAS DE CONTROLE, INTERNET DAS COISAS, ENGENHARIA AERONÁUTICA

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      TAMANAKA, Gustavo Teruo Bernardino e AROCA, Rafael Vidal e CAURIN, Glauco Augusto de Paula. Fault-tolerant architecture and implementation of a distributed control system using containers. 2022, Anais.. Piscataway, NJ, USA: IEEE, 2022. Disponível em: https://doi.org/10.1109/LARS/SBR/WRE56824.2022.9995745. Acesso em: 03 nov. 2025.
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      Tamanaka, G. T. B., Aroca, R. V., & Caurin, G. A. de P. (2022). Fault-tolerant architecture and implementation of a distributed control system using containers. In Proceedings. Piscataway, NJ, USA: IEEE. doi:10.1109/LARS/SBR/WRE56824.2022.9995745
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      Tamanaka GTB, Aroca RV, Caurin GA de P. Fault-tolerant architecture and implementation of a distributed control system using containers [Internet]. Proceedings. 2022 ;[citado 2025 nov. 03 ] Available from: https://doi.org/10.1109/LARS/SBR/WRE56824.2022.9995745
    • Vancouver

      Tamanaka GTB, Aroca RV, Caurin GA de P. Fault-tolerant architecture and implementation of a distributed control system using containers [Internet]. Proceedings. 2022 ;[citado 2025 nov. 03 ] Available from: https://doi.org/10.1109/LARS/SBR/WRE56824.2022.9995745
  • Source: Livro de Resumos Expandidos. Conference titles: Simpósio Internacional de Iniciação Científica e Tecnológica da Universidade de São Paulo - SIICUSP. Unidade: EESC

    Subjects: EPILEPSIA, ENGENHARIA AERONÁUTICA

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      KAWAKAMI, Rodrigo Kazuo Morishigue e CAURIN, Glauco Augusto de Paula e POLEGATO, Paulo Henrique. Sistema de pulseiras inteligentes para detecção de crise epiléptica. 2021, Anais.. São Carlos, SP: EESC/USP, 2021. Disponível em: http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3391/2149. Acesso em: 03 nov. 2025.
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      Kawakami, R. K. M., Caurin, G. A. de P., & Polegato, P. H. (2021). Sistema de pulseiras inteligentes para detecção de crise epiléptica. In Livro de Resumos Expandidos. São Carlos, SP: EESC/USP. Recuperado de http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3391/2149
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      Kawakami RKM, Caurin GA de P, Polegato PH. Sistema de pulseiras inteligentes para detecção de crise epiléptica [Internet]. Livro de Resumos Expandidos. 2021 ;[citado 2025 nov. 03 ] Available from: http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3391/2149
    • Vancouver

      Kawakami RKM, Caurin GA de P, Polegato PH. Sistema de pulseiras inteligentes para detecção de crise epiléptica [Internet]. Livro de Resumos Expandidos. 2021 ;[citado 2025 nov. 03 ] Available from: http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3391/2149
  • Source: Evolutionary Intelligence. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AERONAVES NÃO TRIPULADAS, TRAJETÓRIA, ALGORITMOS GENÉTICOS

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      LIMA, Juliana Veiga Cardoso Fernandes de e BELO, Eduardo Morgado e MARQUES, Vinicius Abrão da Silva. Multi-agent path planning with nonlinear restrictions. Evolutionary Intelligence, p. [1-9], 2021Tradução . . Disponível em: https://doi.org/10.1007/s12065-020-00534-1. Acesso em: 03 nov. 2025.
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      Lima, J. V. C. F. de, Belo, E. M., & Marques, V. A. da S. (2021). Multi-agent path planning with nonlinear restrictions. Evolutionary Intelligence, [1-9]. doi:10.1007/s12065-020-00534-1
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      Lima JVCF de, Belo EM, Marques VA da S. Multi-agent path planning with nonlinear restrictions [Internet]. Evolutionary Intelligence. 2021 ; [1-9].[citado 2025 nov. 03 ] Available from: https://doi.org/10.1007/s12065-020-00534-1
    • Vancouver

      Lima JVCF de, Belo EM, Marques VA da S. Multi-agent path planning with nonlinear restrictions [Internet]. Evolutionary Intelligence. 2021 ; [1-9].[citado 2025 nov. 03 ] Available from: https://doi.org/10.1007/s12065-020-00534-1
  • Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS DE FIBRAS, DANO, ENGENHARIA AERONÁUTICA

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      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: 03 nov. 2025.
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      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. 03 ] 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. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112973
  • Source: Composite Structures. Unidade: EESC

    Subjects: DANO, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA AERONÁUTICA

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      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: 03 nov. 2025.
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      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. 03 ] 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. 03 ] Available from: https://doi.org/10.1016/j.compstruct.2020.112974
  • Source: IEEE Access. Unidade: EESC

    Subjects: SISTEMAS EMBUTIDOS, INTERNET DAS COISAS, ENGENHARIA AERONÁUTICA

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      SILVA JUNIOR, Andouglas Gonçalves da et al. BIPES: block based integrated platform for embedded systems. IEEE Access, v. 8, p. 197955-1917968, 2020Tradução . . Disponível em: https://doi.org/10.1109/ACCESS.2020.3035083. Acesso em: 03 nov. 2025.
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      Silva Junior, A. G. da, Gonçalves, L. M. G., Caurin, G. A. de P., Tamanaka, G. T. B., Hernandes, A. C., & Aroca, R. V. (2020). BIPES: block based integrated platform for embedded systems. IEEE Access, 8, 197955-1917968. doi:10.1109/ACCESS.2020.3035083
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      Silva Junior AG da, Gonçalves LMG, Caurin GA de P, Tamanaka GTB, Hernandes AC, Aroca RV. BIPES: block based integrated platform for embedded systems [Internet]. IEEE Access. 2020 ; 8 197955-1917968.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1109/ACCESS.2020.3035083
    • Vancouver

      Silva Junior AG da, Gonçalves LMG, Caurin GA de P, Tamanaka GTB, Hernandes AC, Aroca RV. BIPES: block based integrated platform for embedded systems [Internet]. IEEE Access. 2020 ; 8 197955-1917968.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1109/ACCESS.2020.3035083
  • Source: Aerospace Science and Technology. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, COMBUSTÍVEIS, ENGENHARIA AERONÁUTICA

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      EGUEA, João Paulo e SILVA, Gabriel Pereira Gouveia da e CATALANO, Fernando Martini. Fuel efficiency improvement on a business jet using a camber morphing winglet concept. Aerospace Science and Technology, v. 96, p. 1-9, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.105542. Acesso em: 03 nov. 2025.
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      Eguea, J. P., Silva, G. P. G. da, & Catalano, F. M. (2020). Fuel efficiency improvement on a business jet using a camber morphing winglet concept. Aerospace Science and Technology, 96, 1-9. doi:10.1016/j.ast.2019.105542
    • NLM

      Eguea JP, Silva GPG da, Catalano FM. Fuel efficiency improvement on a business jet using a camber morphing winglet concept [Internet]. Aerospace Science and Technology. 2020 ; 96 1-9.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
    • Vancouver

      Eguea JP, Silva GPG da, Catalano FM. Fuel efficiency improvement on a business jet using a camber morphing winglet concept [Internet]. Aerospace Science and Technology. 2020 ; 96 1-9.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
  • Source: Journal of Composite Materials. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, DANO, ENGENHARIA AERONÁUTICA

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      TONATTO, Maikson Luiz Passaia e TITA, Volnei e AMICO, Sandro Campos. Composite spirals and rings under flexural loading: experimental and numerical analysis. Journal of Composite Materials, v. 54, n. 20, p. 2697-2705, 2020Tradução . . Disponível em: https://doi.org/10.1177/0021998320902504. Acesso em: 03 nov. 2025.
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      Tonatto, M. L. P., Tita, V., & Amico, S. C. (2020). Composite spirals and rings under flexural loading: experimental and numerical analysis. Journal of Composite Materials, 54( 20), 2697-2705. doi:10.1177/0021998320902504
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      Tonatto MLP, Tita V, Amico SC. Composite spirals and rings under flexural loading: experimental and numerical analysis [Internet]. Journal of Composite Materials. 2020 ; 54( 20): 2697-2705.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1177/0021998320902504
    • Vancouver

      Tonatto MLP, Tita V, Amico SC. Composite spirals and rings under flexural loading: experimental and numerical analysis [Internet]. Journal of Composite Materials. 2020 ; 54( 20): 2697-2705.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1177/0021998320902504
  • Source: Finite Elements in Analysis and Design. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, HOMOGENEIZAÇÃO, ENGENHARIA AERONÁUTICA

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      CHRISTOFF, Bruno Guilherme et al. Development of an ABAQUS™ plug-in to evaluate the fourth-order elasticity tensor of a periodic material via homogenization by the asymptotic expansion method. Finite Elements in Analysis and Design, v. 181, p. 1-13, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.finel.2020.103482. Acesso em: 03 nov. 2025.
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      Christoff, B. G., Brito Santana, H., Talreja, R., & Tita, V. (2020). Development of an ABAQUS™ plug-in to evaluate the fourth-order elasticity tensor of a periodic material via homogenization by the asymptotic expansion method. Finite Elements in Analysis and Design, 181, 1-13. doi:10.1016/j.finel.2020.103482
    • NLM

      Christoff BG, Brito Santana H, Talreja R, Tita V. Development of an ABAQUS™ plug-in to evaluate the fourth-order elasticity tensor of a periodic material via homogenization by the asymptotic expansion method [Internet]. Finite Elements in Analysis and Design. 2020 ; 181 1-13.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1016/j.finel.2020.103482
    • Vancouver

      Christoff BG, Brito Santana H, Talreja R, Tita V. Development of an ABAQUS™ plug-in to evaluate the fourth-order elasticity tensor of a periodic material via homogenization by the asymptotic expansion method [Internet]. Finite Elements in Analysis and Design. 2020 ; 181 1-13.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1016/j.finel.2020.103482
  • Source: Smart Materials and Structures. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, PIEZOELETRICIDADE, ENERGIA EÓLICA, ENGENHARIA AERONÁUTICA

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      DIAS, José Augusto de Carvalho et al. Nonlinear piezoelectric plate framework for aeroelastic energy harvesting and actuation applications. Smart Materials and Structures, v. 29, p. 1-12, 2020Tradução . . Disponível em: https://doi.org/10.1088/1361-665X/ab9add. Acesso em: 03 nov. 2025.
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      Dias, J. A. de C., Sousa, V. C. de, Erturk, A., & De Marqui Júnior, C. (2020). Nonlinear piezoelectric plate framework for aeroelastic energy harvesting and actuation applications. Smart Materials and Structures, 29, 1-12. doi:10.1088/1361-665X/ab9add
    • NLM

      Dias JA de C, Sousa VC de, Erturk A, De Marqui Júnior C. Nonlinear piezoelectric plate framework for aeroelastic energy harvesting and actuation applications [Internet]. Smart Materials and Structures. 2020 ; 29 1-12.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1088/1361-665X/ab9add
    • Vancouver

      Dias JA de C, Sousa VC de, Erturk A, De Marqui Júnior C. Nonlinear piezoelectric plate framework for aeroelastic energy harvesting and actuation applications [Internet]. Smart Materials and Structures. 2020 ; 29 1-12.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1088/1361-665X/ab9add
  • Source: IEEE/ASME Transactions on Mechatronics. Unidade: EESC

    Subjects: VIBRAÇÕES, PIEZOELETRICIDADE, ENGENHARIA AERONÁUTICA

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      SILVA, Tarcísio Marinelli Pereira et al. An experimental study of a piezoelectric metastructure with adaptive resonant shunt circuits. IEEE/ASME Transactions on Mechatronics, v. 25, n. 2, p. 1076-1083, 2020Tradução . . Disponível em: https://doi.org/10.1109/TMECH.2020.2966463. Acesso em: 03 nov. 2025.
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      Silva, T. M. P., Clementino, M. A., Sousa, V. C. de, & De Marqui Júnior, C. (2020). An experimental study of a piezoelectric metastructure with adaptive resonant shunt circuits. IEEE/ASME Transactions on Mechatronics, 25( 2), 1076-1083. doi:10.1109/TMECH.2020.2966463
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      Silva TMP, Clementino MA, Sousa VC de, De Marqui Júnior C. An experimental study of a piezoelectric metastructure with adaptive resonant shunt circuits [Internet]. IEEE/ASME Transactions on Mechatronics. 2020 ; 25( 2): 1076-1083.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1109/TMECH.2020.2966463
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      Silva TMP, Clementino MA, Sousa VC de, De Marqui Júnior C. An experimental study of a piezoelectric metastructure with adaptive resonant shunt circuits [Internet]. IEEE/ASME Transactions on Mechatronics. 2020 ; 25( 2): 1076-1083.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1109/TMECH.2020.2966463
  • Source: Meccanica. Unidade: EESC

    Subjects: LAMINADOS, PIEZOELETRICIDADE, ENGENHARIA AERONÁUTICA

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      LÓPEZ REALPOZO, Juan C et al. Behavior of piezoelectric layered composites with mechanical and electrical non-uniform imperfect contacts. Meccanica, v. 55, p. 125-138, 2020Tradução . . Disponível em: https://doi.org/10.1007/s11012-019-01111-2. Acesso em: 03 nov. 2025.
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      López Realpozo, J. C., Rodríguez Ramos, R., Quintero Roba, A. J., Brito Santana, H., Guinovart Díaz, R., Tita, V., et al. (2020). Behavior of piezoelectric layered composites with mechanical and electrical non-uniform imperfect contacts. Meccanica, 55, 125-138. doi:10.1007/s11012-019-01111-2
    • NLM

      López Realpozo JC, Rodríguez Ramos R, Quintero Roba AJ, Brito Santana H, Guinovart Díaz R, Tita V, Lebon F, Camacho Montes h., Espinosa Almeyda Y, Bravo Castillero J, Sabina FJ. Behavior of piezoelectric layered composites with mechanical and electrical non-uniform imperfect contacts [Internet]. Meccanica. 2020 ; 55 125-138.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1007/s11012-019-01111-2
    • Vancouver

      López Realpozo JC, Rodríguez Ramos R, Quintero Roba AJ, Brito Santana H, Guinovart Díaz R, Tita V, Lebon F, Camacho Montes h., Espinosa Almeyda Y, Bravo Castillero J, Sabina FJ. Behavior of piezoelectric layered composites with mechanical and electrical non-uniform imperfect contacts [Internet]. Meccanica. 2020 ; 55 125-138.[citado 2025 nov. 03 ] Available from: https://doi.org/10.1007/s11012-019-01111-2

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