Filtros : "AEROELASTICIDADE DE AERONAVES" Removido: "Brasil" 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: 14 out. 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 out. 14 ] 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 out. 14 ] Available from: http://dx.doi.org/10.1007/s11071-024-09515-w
  • Source: Aerospace Science and Technology. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, SIMULADORES DE VOO, ALGORITMOS, ENGENHARIA AERONÁUTICA

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      PALADINI, Andre Luis Aguiar e DREWIACKI, Daniel e BIDINOTTO, Jorge Henrique. Aeroelastic effects in PIO occurrences: A dual approach on flight simulator tests. Aerospace Science and Technology, v. 151, p. 1-12, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.ast.2024.109337. Acesso em: 14 out. 2024.
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      Paladini, A. L. A., Drewiacki, D., & Bidinotto, J. H. (2024). Aeroelastic effects in PIO occurrences: A dual approach on flight simulator tests. Aerospace Science and Technology, 151, 1-12. doi:10.1016/j.ast.2024.109337
    • NLM

      Paladini ALA, Drewiacki D, Bidinotto JH. Aeroelastic effects in PIO occurrences: A dual approach on flight simulator tests [Internet]. Aerospace Science and Technology. 2024 ; 151 1-12.[citado 2024 out. 14 ] Available from: http://dx.doi.org/10.1016/j.ast.2024.109337
    • Vancouver

      Paladini ALA, Drewiacki D, Bidinotto JH. Aeroelastic effects in PIO occurrences: A dual approach on flight simulator tests [Internet]. Aerospace Science and Technology. 2024 ; 151 1-12.[citado 2024 out. 14 ] Available from: http://dx.doi.org/10.1016/j.ast.2024.109337
  • 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: 14 out. 2024.
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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
    • NLM

      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 2024 out. 14 ] 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 2024 out. 14 ] Available from: https://doi.org/10.1007/s40430-022-03783-6
  • Source: Journal of the Brazilian Society of Mechanical Sciences and Engineering. Unidade: EESC

    Subjects: VIBRAÇÕES, AEROELASTICIDADE DE AERONAVES, GEOMETRIA, ENGENHARIA AERONÁUTICA

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      PALADINI, Andre Luis Aguiar et al. Control of airfow induced vibrations on a cantilever beam by actuating on the exposure of its machined surface notch pattern. Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 45, p. 1-16, 2023Tradução . . Disponível em: https://doi.org/10.1007/s40430-023-04255-1. Acesso em: 14 out. 2024.
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      Paladini, A. L. A., Rodrigues, A. L. G., Bidinotto, J. H., & Franco, V. R. (2023). Control of airfow induced vibrations on a cantilever beam by actuating on the exposure of its machined surface notch pattern. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 45, 1-16. doi:10.1007/s40430-023-04255-1
    • NLM

      Paladini ALA, Rodrigues ALG, Bidinotto JH, Franco VR. Control of airfow induced vibrations on a cantilever beam by actuating on the exposure of its machined surface notch pattern [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2023 ; 45 1-16.[citado 2024 out. 14 ] Available from: https://doi.org/10.1007/s40430-023-04255-1
    • Vancouver

      Paladini ALA, Rodrigues ALG, Bidinotto JH, Franco VR. Control of airfow induced vibrations on a cantilever beam by actuating on the exposure of its machined surface notch pattern [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2023 ; 45 1-16.[citado 2024 out. 14 ] Available from: https://doi.org/10.1007/s40430-023-04255-1
  • Source: Aerospace. Unidade: EESC

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

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    • ABNT

      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: 14 out. 2024.
    • APA

      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 out. 14 ] 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 out. 14 ] 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: 14 out. 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 out. 14 ] 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 out. 14 ] 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: 14 out. 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 out. 14 ] 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 out. 14 ] 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: 14 out. 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
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      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 out. 14 ] 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 out. 14 ] Available from: https://doi.org/10.1115/1.4050792
  • 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: 14 out. 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 out. 14 ] 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 out. 14 ] Available from: https://doi.org/10.1016/j.tws.2020.107379
  • 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: 14 out. 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 out. 14 ] 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 out. 14 ] Available from: https://doi.org/10.1177/10775463211000161
  • 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: 14 out. 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 out. 14 ] 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 out. 14 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2021.103730
  • 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: 14 out. 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 out. 14 ] 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 out. 14 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2021.103250
  • 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: 14 out. 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 out. 14 ] 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 out. 14 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2020.103545
  • 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: 14 out. 2024.
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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
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      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 2024 out. 14 ] 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 2024 out. 14 ] Available from: https://doi.org/10.1088/1361-665X/ab9add
  • 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: 14 out. 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 out. 14 ] 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 out. 14 ] Available from: https://doi.org/10.2514/6.2020-2665
  • Source: Physical Review Applied. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, PIEZOELETRICIDADE, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA

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      BELI, Danilo e RUZZENE, Massimo e DE MARQUI JÚNIOR, Carlos. Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers. Physical Review Applied, v. 14, p. 1-14, 2020Tradução . . Disponível em: https://doi.org/10.1103/PhysRevApplied.14.034032. Acesso em: 14 out. 2024.
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      Beli, D., Ruzzene, M., & De Marqui Júnior, C. (2020). Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers. Physical Review Applied, 14, 1-14. doi:10.1103/PhysRevApplied.14.034032
    • NLM

      Beli D, Ruzzene M, De Marqui Júnior C. Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers [Internet]. Physical Review Applied. 2020 ; 14 1-14.[citado 2024 out. 14 ] Available from: https://doi.org/10.1103/PhysRevApplied.14.034032
    • Vancouver

      Beli D, Ruzzene M, De Marqui Júnior C. Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers [Internet]. Physical Review Applied. 2020 ; 14 1-14.[citado 2024 out. 14 ] Available from: https://doi.org/10.1103/PhysRevApplied.14.034032
  • 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: 14 out. 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
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      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 out. 14 ] 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 out. 14 ] 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: 14 out. 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
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      Marques FD, Ferreira AJM. Nonlinear dynamics of fluttering multibay panels in supersonic regime [Internet]. Proceedings. 2019 ;[citado 2024 out. 14 ] 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 out. 14 ] 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: 14 out. 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
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      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 out. 14 ] 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 out. 14 ] 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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      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: 14 out. 2024.
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      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 out. 14 ] 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 out. 14 ] Available from: https://doi.org/10.2514/6.2020-0941

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