Filtros : "Composite Structures" "CARRAZEDO, ROGÉRIO" Limpar

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  • 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
  • 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
  • Source: Composite Structures. Unidade: EESC

    Subjects: ANÁLISE NÃO LINEAR DE ESTRUTURAS, LAMINADOS, PLACAS, ESTRUTURAS

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    • ABNT

      CODA, Humberto Breves e PACCOLA, Rodrigo Ribeiro e CARRAZEDO, Rogério. Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells. Composite Structures, v. 161, p. 32-50, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2016.10.129. Acesso em: 17 nov. 2025.
    • APA

      Coda, H. B., Paccola, R. R., & Carrazedo, R. (2017). Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells. Composite Structures, 161, 32-50. doi:10.1016/j.compstruct.2016.10.129
    • NLM

      Coda HB, Paccola RR, Carrazedo R. Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells [Internet]. Composite Structures. 2017 ; 161 32-50.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.129
    • Vancouver

      Coda HB, Paccola RR, Carrazedo R. Zig-Zag effect without degrees of freedom in linear and non linear analysis of laminated plates and shells [Internet]. Composite Structures. 2017 ; 161 32-50.[citado 2025 nov. 17 ] Available from: https://doi.org/10.1016/j.compstruct.2016.10.129

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