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Filtros : "Ferreira, António J. M." Limpar

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  • Artigo de periodico

    The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays (2021)

    Cabral, Myrella V.; Marques, Flavio Donizeti ; Ferreira, António J. M.

    Source: Thin-Walled Structures. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA

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    • ABNT

      CABRAL, Myrella V. e MARQUES, Flavio Donizeti e FERREIRA, António J. M. The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays. Thin-Walled Structures, v. 161, p. 1-12, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.tws.2020.107379. Acesso em: 06 nov. 2024.

    • APA

      Cabral, M. V., Marques, F. D., & Ferreira, A. J. M. (2021). The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays. Thin-Walled Structures, 161, 1-12. doi:10.1016/j.tws.2020.107379

    • NLM

      Cabral MV, Marques FD, Ferreira AJM. The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays [Internet]. Thin-Walled Structures. 2021 ; 161 1-12.[citado 2024 nov. 06 ] Available from: https://doi.org/10.1016/j.tws.2020.107379

    • Vancouver

      Cabral MV, Marques FD, Ferreira AJM. The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays [Internet]. Thin-Walled Structures. 2021 ; 161 1-12.[citado 2024 nov. 06 ] Available from: https://doi.org/10.1016/j.tws.2020.107379

  • Artigo de periodico

    Development of a finite element via unified formulation: implementation as a user element subroutine to predict stress profiles in composite plates (2020)

    Ferreira, Gregório Felipe Oliveira; Almeida Júnior, José Humberto Santos; Ribeiro, Marcelo Leite ; Ferreira, António J. M.; Tita, Volnei

    Source: Thin-Walled Structures. Unidade: EESC

    Subjects: MÉTODO DOS ELEMENTOS FINITOS, LAMINADOS, AERONÁUTICA

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    • ABNT

      FERREIRA, Gregório Felipe Oliveira et al. Development of a finite element via unified formulation: implementation as a user element subroutine to predict stress profiles in composite plates. Thin-Walled Structures, v. 157, p. 1-19, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.tws.2020.107107. Acesso em: 06 nov. 2024.

    • APA

      Ferreira, G. F. O., Almeida Júnior, J. H. S., Ribeiro, M. L., Ferreira, A. J. M., & Tita, V. (2020). Development of a finite element via unified formulation: implementation as a user element subroutine to predict stress profiles in composite plates. Thin-Walled Structures, 157, 1-19. doi:10.1016/j.tws.2020.107107

    • NLM

      Ferreira GFO, Almeida Júnior JHS, Ribeiro ML, Ferreira AJM, Tita V. Development of a finite element via unified formulation: implementation as a user element subroutine to predict stress profiles in composite plates [Internet]. Thin-Walled Structures. 2020 ; 157 1-19.[citado 2024 nov. 06 ] Available from: https://doi.org/10.1016/j.tws.2020.107107

    • Vancouver

      Ferreira GFO, Almeida Júnior JHS, Ribeiro ML, Ferreira AJM, Tita V. Development of a finite element via unified formulation: implementation as a user element subroutine to predict stress profiles in composite plates [Internet]. Thin-Walled Structures. 2020 ; 157 1-19.[citado 2024 nov. 06 ] Available from: https://doi.org/10.1016/j.tws.2020.107107

  • Artigo de periodico

    Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime (2017)

    Marques, Flávio Donizeti; Natarajan, S.; Ferreira, António J. M.

    Source: Composite Structures. Unidade: EESC

    Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, PAINÉIS, AEROELASTICIDADE DE AERONAVES

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    • ABNT

      MARQUES, Flávio Donizeti e NATARAJAN, S. e FERREIRA, António J. M. Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime. Composite Structures, v. 167, p. 30-37, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2017.01.062. Acesso em: 06 nov. 2024.

    • APA

      Marques, F. D., Natarajan, S., & Ferreira, A. J. M. (2017). Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime. Composite Structures, 167, 30-37. doi:10.1016/j.compstruct.2017.01.062

    • NLM

      Marques FD, Natarajan S, Ferreira AJM. Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime [Internet]. Composite Structures. 2017 ; 167 30-37.[citado 2024 nov. 06 ] Available from: https://doi.org/10.1016/j.compstruct.2017.01.062

    • Vancouver

      Marques FD, Natarajan S, Ferreira AJM. Evolutionary-based aeroelastic tailoring of stiffened laminate composite panels in supersonic flow regime [Internet]. Composite Structures. 2017 ; 167 30-37.[citado 2024 nov. 06 ] Available from: https://doi.org/10.1016/j.compstruct.2017.01.062
  • 1

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