Filtros : "AEROELASTICIDADE DE AERONAVES" "EESC-SEM" Removidos: "Capovilla, Fernando César" "1939" Limpar

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  • Source: Nonlinear Dynamics. Unidade: EESC

    Subjects: DISSIPADORES DE ENERGIA, AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA

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    • ABNT

      ARAUJO, Gabriel Placeres e SILVA, Jose Augusto Ignácio da e MARQUES, Flavio Donizeti. Passive flutter mitigation with rotary nonlinear energy sink. Nonlinear Dynamics, p. 1-19, 2024Tradução . . Disponível em: http://dx.doi.org/10.1007/s11071-024-09515-w. Acesso em: 07 set. 2024.
    • APA

      Araujo, G. P., Silva, J. A. I. da, & Marques, F. D. (2024). Passive flutter mitigation with rotary nonlinear energy sink. Nonlinear Dynamics, 1-19. doi:10.1007/s11071-024-09515-w
    • NLM

      Araujo GP, Silva JAI da, Marques FD. Passive flutter mitigation with rotary nonlinear energy sink [Internet]. Nonlinear Dynamics. 2024 ; 1-19.[citado 2024 set. 07 ] Available from: http://dx.doi.org/10.1007/s11071-024-09515-w
    • Vancouver

      Araujo GP, Silva JAI da, Marques FD. Passive flutter mitigation with rotary nonlinear energy sink [Internet]. Nonlinear Dynamics. 2024 ; 1-19.[citado 2024 set. 07 ] Available from: http://dx.doi.org/10.1007/s11071-024-09515-w
  • Source: Aerospace. Unidade: EESC

    Subjects: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, FLAPS, ENGENHARIA MECÂNICA

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      CAMACHO, Emanuel A. R. e MARQUES, Flavio Donizeti e SILVA, Andre R. R. Influence of a deflectable leading-edge on a flapping airfoil. Aerospace, v. 10, n. 7, p. 1-17, 2023Tradução . . Disponível em: https://doi.org/10.3390/aerospace10070615. Acesso em: 07 set. 2024.
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      Camacho, E. A. R., Marques, F. D., & Silva, A. R. R. (2023). Influence of a deflectable leading-edge on a flapping airfoil. Aerospace, 10( 7), 1-17. doi:10.3390/aerospace10070615
    • NLM

      Camacho EAR, Marques FD, Silva ARR. Influence of a deflectable leading-edge on a flapping airfoil [Internet]. Aerospace. 2023 ; 10( 7): 1-17.[citado 2024 set. 07 ] Available from: https://doi.org/10.3390/aerospace10070615
    • Vancouver

      Camacho EAR, Marques FD, Silva ARR. Influence of a deflectable leading-edge on a flapping airfoil [Internet]. Aerospace. 2023 ; 10( 7): 1-17.[citado 2024 set. 07 ] Available from: https://doi.org/10.3390/aerospace10070615
  • Source: Composite Structures. Unidade: EESC

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

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      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: 07 set. 2024.
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      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 set. 07 ] 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 set. 07 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
  • Source: International Journal of Non-Linear Mechanics. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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      VASCONCELLOS, Rui et al. Aeroelastic analysis and nonlinear characterization of three-degree-of-freedom systems with discontinuous nonlinearities. International Journal of Non-Linear Mechanics, v. 145, p. 1-19, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.ijnonlinmec.2022.104100. Acesso em: 07 set. 2024.
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      Vasconcellos, R., Bouma, A., Marques, F. D., Abdelkefi, A., & Hajj, M. R. (2022). Aeroelastic analysis and nonlinear characterization of three-degree-of-freedom systems with discontinuous nonlinearities. International Journal of Non-Linear Mechanics, 145, 1-19. doi:10.1016/j.ijnonlinmec.2022.104100
    • NLM

      Vasconcellos R, Bouma A, Marques FD, Abdelkefi A, Hajj MR. Aeroelastic analysis and nonlinear characterization of three-degree-of-freedom systems with discontinuous nonlinearities [Internet]. International Journal of Non-Linear Mechanics. 2022 ; 145 1-19.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2022.104100
    • Vancouver

      Vasconcellos R, Bouma A, Marques FD, Abdelkefi A, Hajj MR. Aeroelastic analysis and nonlinear characterization of three-degree-of-freedom systems with discontinuous nonlinearities [Internet]. International Journal of Non-Linear Mechanics. 2022 ; 145 1-19.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2022.104100
  • Source: Journal of Computational and Nonlinear Dynamics. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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      CORREA, Renan F e MARQUES, Flavio Donizeti. Influence of bistable plunge stiffness on nonlinear airfoil flutter. Journal of Computational and Nonlinear Dynamics, v. 16, p. 1-14, 2021Tradução . . Disponível em: https://doi.org/10.1115/1.4050792. Acesso em: 07 set. 2024.
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      Correa, R. F., & Marques, F. D. (2021). Influence of bistable plunge stiffness on nonlinear airfoil flutter. Journal of Computational and Nonlinear Dynamics, 16, 1-14. doi:10.1115/1.4050792
    • NLM

      Correa RF, Marques FD. Influence of bistable plunge stiffness on nonlinear airfoil flutter [Internet]. Journal of Computational and Nonlinear Dynamics. 2021 ; 16 1-14.[citado 2024 set. 07 ] Available from: https://doi.org/10.1115/1.4050792
    • Vancouver

      Correa RF, Marques FD. Influence of bistable plunge stiffness on nonlinear airfoil flutter [Internet]. Journal of Computational and Nonlinear Dynamics. 2021 ; 16 1-14.[citado 2024 set. 07 ] Available from: https://doi.org/10.1115/1.4050792
  • Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC

    Subjects: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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    • ABNT

      SANTOS, Luiz Guilherme Pancini dos e MARQUES, Flavio Donizeti. Dynamic behavior of stall fluttering airfoils. 2021, Anais.. São Carlos, SP: EESC-USP, 2021. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/vsipgem/paper/view/3163/2280. Acesso em: 07 set. 2024.
    • APA

      Santos, L. G. P. dos, & Marques, F. D. (2021). Dynamic behavior of stall fluttering airfoils. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/vsipgem/paper/view/3163/2280
    • NLM

      Santos LGP dos, Marques FD. Dynamic behavior of stall fluttering airfoils [Internet]. Anais. 2021 ;[citado 2024 set. 07 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/vsipgem/paper/view/3163/2280
    • Vancouver

      Santos LGP dos, Marques FD. Dynamic behavior of stall fluttering airfoils [Internet]. Anais. 2021 ;[citado 2024 set. 07 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/vsipgem/paper/view/3163/2280
  • Source: Thin-Walled Structures. Unidade: EESC

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

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      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: 07 set. 2024.
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      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 set. 07 ] 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 set. 07 ] Available from: https://doi.org/10.1016/j.tws.2020.107379
  • Source: Livro de Resumos Expandidos. Conference titles: Simpósio Internacional de Iniciação Científica e Tecnológica da Universidade de São Paulo - SIICUSP. Unidade: EESC

    Subjects: VIBRAÇÕES, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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      RIBEIRO, Adolfo Esteves e MARQUES, Flavio Donizeti. Controle passivo de vibrações aeroelásticas empregando nonlinear energy sinks. 2021, Anais.. São Carlos, SP: EESC/USP, 2021. Disponível em: http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3262/2068. Acesso em: 07 set. 2024.
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      Ribeiro, A. E., & Marques, F. D. (2021). Controle passivo de vibrações aeroelásticas empregando nonlinear energy sinks. In Livro de Resumos Expandidos. São Carlos, SP: EESC/USP. Recuperado de http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3262/2068
    • NLM

      Ribeiro AE, Marques FD. Controle passivo de vibrações aeroelásticas empregando nonlinear energy sinks [Internet]. Livro de Resumos Expandidos. 2021 ;[citado 2024 set. 07 ] Available from: http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3262/2068
    • Vancouver

      Ribeiro AE, Marques FD. Controle passivo de vibrações aeroelásticas empregando nonlinear energy sinks [Internet]. Livro de Resumos Expandidos. 2021 ;[citado 2024 set. 07 ] Available from: http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3262/2068
  • Source: Journal of Vibration and Control. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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      SILVA, Jose Augusto Ignácio da e MARQUES, Flavio Donizeti. Characterization of typical aeroelastic sections under combined structural concentrated nonlinearities. Journal of Vibration and Control, p. 1-15, 2021Tradução . . Disponível em: https://doi.org/10.1177/10775463211000161. Acesso em: 07 set. 2024.
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      Silva, J. A. I. da, & Marques, F. D. (2021). Characterization of typical aeroelastic sections under combined structural concentrated nonlinearities. Journal of Vibration and Control, 1-15. doi:10.1177/10775463211000161
    • NLM

      Silva JAI da, Marques FD. Characterization of typical aeroelastic sections under combined structural concentrated nonlinearities [Internet]. Journal of Vibration and Control. 2021 ; 1-15.[citado 2024 set. 07 ] Available from: https://doi.org/10.1177/10775463211000161
    • Vancouver

      Silva JAI da, Marques FD. Characterization of typical aeroelastic sections under combined structural concentrated nonlinearities [Internet]. Journal of Vibration and Control. 2021 ; 1-15.[citado 2024 set. 07 ] Available from: https://doi.org/10.1177/10775463211000161
  • Source: Journal of Fluids and Structures. Unidade: EESC

    Subjects: TURBULÊNCIA ATMOSFÉRICA, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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      SANTOS, Luiz Guilherme Pancini dos e MARQUES, Flavio Donizeti. Nonlinear aeroelastic analysis of airfoil section under stall flutter oscillations and gust loads. Journal of Fluids and Structures, v. 102, p. 1-20, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.jfluidstructs.2021.103250. Acesso em: 07 set. 2024.
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      Santos, L. G. P. dos, & Marques, F. D. (2021). Nonlinear aeroelastic analysis of airfoil section under stall flutter oscillations and gust loads. Journal of Fluids and Structures, 102, 1-20. doi:10.1016/j.jfluidstructs.2021.103250
    • NLM

      Santos LGP dos, Marques FD. Nonlinear aeroelastic analysis of airfoil section under stall flutter oscillations and gust loads [Internet]. Journal of Fluids and Structures. 2021 ; 102 1-20.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2021.103250
    • Vancouver

      Santos LGP dos, Marques FD. Nonlinear aeroelastic analysis of airfoil section under stall flutter oscillations and gust loads [Internet]. Journal of Fluids and Structures. 2021 ; 102 1-20.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2021.103250
  • Source: International Journal of Non-Linear Mechanics. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, PAINÉIS

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      CABRAL, Myrella V e MARQUES, Flavio Donizeti e FERREIRA, Antonio Joaquim Mendes. Nonlinear supersonic flutter of multibay cross-stream shallow shells. International Journal of Non-Linear Mechanics, v. 133, p. 1-13, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.ijnonlinmec.2021.103730. Acesso em: 07 set. 2024.
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      Cabral, M. V., Marques, F. D., & Ferreira, A. J. M. (2021). Nonlinear supersonic flutter of multibay cross-stream shallow shells. International Journal of Non-Linear Mechanics, 133, 1-13. doi:10.1016/j.ijnonlinmec.2021.103730
    • NLM

      Cabral MV, Marques FD, Ferreira AJM. Nonlinear supersonic flutter of multibay cross-stream shallow shells [Internet]. International Journal of Non-Linear Mechanics. 2021 ; 133 1-13.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2021.103730
    • Vancouver

      Cabral MV, Marques FD, Ferreira AJM. Nonlinear supersonic flutter of multibay cross-stream shallow shells [Internet]. International Journal of Non-Linear Mechanics. 2021 ; 133 1-13.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2021.103730
  • Source: International Journal of Non-Linear Mechanics. Unidade: EESC

    Subjects: ESTRUTURA DE AERONAVES, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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      GUIMARÃES, Thiago A. M e SANCHES, Leonardo e MARQUES, Flavio Donizeti. Nonlinear supersonic post-flutter motion of panels with adjacent bays and thermal effects. International Journal of Non-Linear Mechanics, v. 125, p. 1-13, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ijnonlinmec.2020.103545. Acesso em: 07 set. 2024.
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      Guimarães, T. A. M., Sanches, L., & Marques, F. D. (2020). Nonlinear supersonic post-flutter motion of panels with adjacent bays and thermal effects. International Journal of Non-Linear Mechanics, 125, 1-13. doi:10.1016/j.ijnonlinmec.2020.103545
    • NLM

      Guimarães TAM, Sanches L, Marques FD. Nonlinear supersonic post-flutter motion of panels with adjacent bays and thermal effects [Internet]. International Journal of Non-Linear Mechanics. 2020 ; 125 1-13.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2020.103545
    • Vancouver

      Guimarães TAM, Sanches L, Marques FD. Nonlinear supersonic post-flutter motion of panels with adjacent bays and thermal effects [Internet]. International Journal of Non-Linear Mechanics. 2020 ; 125 1-13.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2020.103545
  • Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC

    Assunto: AEROELASTICIDADE DE AERONAVES

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      VASCONCELLOS, Rui Marcos Grombone de et al. Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity. 2020, Anais.. Reston, VA, USA: AIAA, 2020. Disponível em: https://doi.org/10.2514/6.2020-2665. Acesso em: 07 set. 2024.
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      Vasconcellos, R. M. G. de, Bouma, A., Marques, F. D., Abdelkefi, A., & Hajj, M. R. (2020). Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-2665
    • NLM

      Vasconcellos RMG de, Bouma A, Marques FD, Abdelkefi A, Hajj MR. Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity [Internet]. Proceedings. 2020 ;[citado 2024 set. 07 ] Available from: https://doi.org/10.2514/6.2020-2665
    • Vancouver

      Vasconcellos RMG de, Bouma A, Marques FD, Abdelkefi A, Hajj MR. Aeroelastic analysis and characterization of three-degree-of-freedom systems with discontinuous nonlinearity [Internet]. Proceedings. 2020 ;[citado 2024 set. 07 ] Available from: https://doi.org/10.2514/6.2020-2665
  • Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, MATERIAIS COMPÓSITOS, ENGENHARIA MECÂNICA

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      NAJAFI, Maliheh e MARQUES, Flavio Donizeti. Review paper on composite panel flutter. 2019, Anais.. São Carlos, SP: EESC-USP, 2019. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1826/1030. Acesso em: 07 set. 2024.
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      Najafi, M., & Marques, F. D. (2019). Review paper on composite panel flutter. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1826/1030
    • NLM

      Najafi M, Marques FD. Review paper on composite panel flutter [Internet]. Anais. 2019 ;[citado 2024 set. 07 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1826/1030
    • Vancouver

      Najafi M, Marques FD. Review paper on composite panel flutter [Internet]. Anais. 2019 ;[citado 2024 set. 07 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1826/1030
  • Source: Nonlinear Dynamics. Unidade: EESC

    Subjects: REDES NEURAIS, AERODINÂMICA DE AERONAVES, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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      PAULA, Natália Cristina Gomes de e MARQUES, Flavio Donizeti. Multi-variable Volterra kernels identification using time-delay neural networks: application to unsteady aerodynamic loading. Nonlinear Dynamics, v. 97, p. 767-780, 2019Tradução . . Disponível em: https://doi.org/10.1007/s11071-019-05011-8. Acesso em: 07 set. 2024.
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      Paula, N. C. G. de, & Marques, F. D. (2019). Multi-variable Volterra kernels identification using time-delay neural networks: application to unsteady aerodynamic loading. Nonlinear Dynamics, 97, 767-780. doi:10.1007/s11071-019-05011-8
    • NLM

      Paula NCG de, Marques FD. Multi-variable Volterra kernels identification using time-delay neural networks: application to unsteady aerodynamic loading [Internet]. Nonlinear Dynamics. 2019 ; 97 767-780.[citado 2024 set. 07 ] Available from: https://doi.org/10.1007/s11071-019-05011-8
    • Vancouver

      Paula NCG de, Marques FD. Multi-variable Volterra kernels identification using time-delay neural networks: application to unsteady aerodynamic loading [Internet]. Nonlinear Dynamics. 2019 ; 97 767-780.[citado 2024 set. 07 ] Available from: https://doi.org/10.1007/s11071-019-05011-8
  • Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: EESC

    Subjects: PAINÉIS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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      MARQUES, Flavio Donizeti e FERREIRA, A. J. M. Nonlinear dynamics of fluttering multibay panels in supersonic regime. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-1867. Acesso em: 07 set. 2024.
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      Marques, F. D., & Ferreira, A. J. M. (2019). Nonlinear dynamics of fluttering multibay panels in supersonic regime. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-1867
    • NLM

      Marques FD, Ferreira AJM. Nonlinear dynamics of fluttering multibay panels in supersonic regime [Internet]. Proceedings. 2019 ;[citado 2024 set. 07 ] Available from: https://doi.org/10.2514/6.2019-1867
    • Vancouver

      Marques FD, Ferreira AJM. Nonlinear dynamics of fluttering multibay panels in supersonic regime [Internet]. Proceedings. 2019 ;[citado 2024 set. 07 ] Available from: https://doi.org/10.2514/6.2019-1867
  • Source: Journal of Vibration and Control. Unidade: EESC

    Subjects: ENERGIA ELÉTRICA, AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, PIEZOELETRICIDADE, ENGENHARIA MECÂNICA

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      SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti e HAJJ, Muhammad R. The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations. Journal of Vibration and Control, v. 25, n. 14, p. 1991-2007, 2019Tradução . . Disponível em: https://doi.org/10.1177/1077546319844383. Acesso em: 07 set. 2024.
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      Santos, C. R. dos, Marques, F. D., & Hajj, M. R. (2019). The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations. Journal of Vibration and Control, 25( 14), 1991-2007. doi:10.1177/1077546319844383
    • NLM

      Santos CR dos, Marques FD, Hajj MR. The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations [Internet]. Journal of Vibration and Control. 2019 ; 25( 14): 1991-2007.[citado 2024 set. 07 ] Available from: https://doi.org/10.1177/1077546319844383
    • Vancouver

      Santos CR dos, Marques FD, Hajj MR. The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations [Internet]. Journal of Vibration and Control. 2019 ; 25( 14): 1991-2007.[citado 2024 set. 07 ] Available from: https://doi.org/10.1177/1077546319844383
  • Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: EESC

    Subjects: ENGENHARIA MECÂNICA, VIBRAÇÕES DE AERONAVES, AEROELASTICIDADE DE AERONAVES, PAINÉIS

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    • ABNT

      GUIMARÃES, Thiago A. M. et al. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2020-0941. Acesso em: 07 set. 2024.
    • APA

      Guimarães, T. A. M., Rade, D. A., Cesnik, C. E. S., & Marques, F. D. (2019). Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-0941
    • NLM

      Guimarães TAM, Rade DA, Cesnik CES, Marques FD. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers [Internet]. Proceedings. 2019 ;[citado 2024 set. 07 ] Available from: https://doi.org/10.2514/6.2020-0941
    • Vancouver

      Guimarães TAM, Rade DA, Cesnik CES, Marques FD. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers [Internet]. Proceedings. 2019 ;[citado 2024 set. 07 ] Available from: https://doi.org/10.2514/6.2020-0941
  • Source: Aerospace Science and Technology. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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    • ABNT

      SANCHES, Leonardo e GUIMARÃES, Thiago A. M e MARQUES, Flavio Donizeti. Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs. Aerospace Science and Technology, v. 90, p. 157-168, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.04.031. Acesso em: 07 set. 2024.
    • APA

      Sanches, L., Guimarães, T. A. M., & Marques, F. D. (2019). Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs. Aerospace Science and Technology, 90, 157-168. doi:10.1016/j.ast.2019.04.031
    • NLM

      Sanches L, Guimarães TAM, Marques FD. Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs [Internet]. Aerospace Science and Technology. 2019 ; 90 157-168.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.ast.2019.04.031
    • Vancouver

      Sanches L, Guimarães TAM, Marques FD. Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs [Internet]. Aerospace Science and Technology. 2019 ; 90 157-168.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.ast.2019.04.031
  • Source: Mechanical Systems and Signal Processing. Unidade: EESC

    Subjects: ALGORITMOS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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      SALES, Thiago P et al. Modeling and dynamic characterization of nonlinear non-smooth aeroviscoelastic systems. Mechanical Systems and Signal Processing, v. 116, p. 900-915, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.ymssp.2018.07.003. Acesso em: 07 set. 2024.
    • APA

      Sales, T. P., Pereira, D. A., Marques, F. D., & Rade, D. A. (2019). Modeling and dynamic characterization of nonlinear non-smooth aeroviscoelastic systems. Mechanical Systems and Signal Processing, 116, 900-915. doi:10.1016/j.ymssp.2018.07.003
    • NLM

      Sales TP, Pereira DA, Marques FD, Rade DA. Modeling and dynamic characterization of nonlinear non-smooth aeroviscoelastic systems [Internet]. Mechanical Systems and Signal Processing. 2019 ; 116 900-915.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.ymssp.2018.07.003
    • Vancouver

      Sales TP, Pereira DA, Marques FD, Rade DA. Modeling and dynamic characterization of nonlinear non-smooth aeroviscoelastic systems [Internet]. Mechanical Systems and Signal Processing. 2019 ; 116 900-915.[citado 2024 set. 07 ] Available from: https://doi.org/10.1016/j.ymssp.2018.07.003

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