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  • Source: Meccanica: An International Journal of Theoretical and Applied Mmechanics. Unidade: EESC

    Subjects: ENERGIA EÓLICA, GERAÇÃO DE ENERGIA ELÉTRICA, ENGENHARIA MECÂNICA

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    • ABNT

      SUZUKI, Pedro Kaneto e MARQUES, Flavio Donizeti e PEREIRA, Daniel A. Centimeter‑scale wind turbines design and analysis. Meccanica: An International Journal of Theoretical and Applied Mmechanics, p. 1-15, 2023Tradução . . Disponível em: https://doi.org/10.1007/s11012-023-01652-7. Acesso em: 08 nov. 2025.
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      Suzuki, P. K., Marques, F. D., & Pereira, D. A. (2023). Centimeter‑scale wind turbines design and analysis. Meccanica: An International Journal of Theoretical and Applied Mmechanics, 1-15. doi:10.1007/s11012-023-01652-7
    • NLM

      Suzuki PK, Marques FD, Pereira DA. Centimeter‑scale wind turbines design and analysis [Internet]. Meccanica: An International Journal of Theoretical and Applied Mmechanics. 2023 ; 1-15.[citado 2025 nov. 08 ] Available from: https://doi.org/10.1007/s11012-023-01652-7
    • Vancouver

      Suzuki PK, Marques FD, Pereira DA. Centimeter‑scale wind turbines design and analysis [Internet]. Meccanica: An International Journal of Theoretical and Applied Mmechanics. 2023 ; 1-15.[citado 2025 nov. 08 ] Available from: https://doi.org/10.1007/s11012-023-01652-7
  • Source: Engineering Proceedings. Unidade: EESC

    Subjects: AEROFÓLIOS, PROPULSÃO DE AERONAVES, ENGENHARIA MECÂNICA

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    • ABNT

      CAMACHO, Emanuel A. R e MARQUES, Flavio Donizeti e SILVA, Andre R. R. Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method. Engineering Proceedings, v. 56, n. 1, p. 1-8, 2023Tradução . . Disponível em: https://dx.doi.org/10.3390/ASEC2023-15886. Acesso em: 08 nov. 2025.
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      Camacho, E. A. R., Marques, F. D., & Silva, A. R. R. (2023). Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method. Engineering Proceedings, 56( 1), 1-8. doi:10.3390/ASEC2023-15886
    • NLM

      Camacho EAR, Marques FD, Silva ARR. Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method [Internet]. Engineering Proceedings. 2023 ; 56( 1): 1-8.[citado 2025 nov. 08 ] Available from: https://dx.doi.org/10.3390/ASEC2023-15886
    • Vancouver

      Camacho EAR, Marques FD, Silva ARR. Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method [Internet]. Engineering Proceedings. 2023 ; 56( 1): 1-8.[citado 2025 nov. 08 ] Available from: https://dx.doi.org/10.3390/ASEC2023-15886
  • Source: Composite Structures. Unidade: EESC

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

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    • ABNT

      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: 08 nov. 2025.
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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 2025 nov. 08 ] 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 2025 nov. 08 ] 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: 08 nov. 2025.
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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 2025 nov. 08 ] 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 2025 nov. 08 ] 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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    • ABNT

      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: 08 nov. 2025.
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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 2025 nov. 08 ] 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 2025 nov. 08 ] 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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    • 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: 08 nov. 2025.
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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 2025 nov. 08 ] 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 2025 nov. 08 ] Available from: https://doi.org/10.1016/j.tws.2020.107379
  • Source: Meccanica: An International Journal of Theoretical and Applied Mmechanics. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, AERONAVES NÃO TRIPULADAS, ENGENHARIA MECÂNICA

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      DIAZ IZQUIERDO, David Orlando e MARQUES, Flavio Donizeti. Experimental analysis of passive bio-inspired covert feathers for stall and post-stall performance enhancement. Meccanica: An International Journal of Theoretical and Applied Mmechanics, p. 1-19, 2021Tradução . . Disponível em: https://doi.org/10.1007/s11012-021-01409-0. Acesso em: 08 nov. 2025.
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      Diaz Izquierdo, D. O., & Marques, F. D. (2021). Experimental analysis of passive bio-inspired covert feathers for stall and post-stall performance enhancement. Meccanica: An International Journal of Theoretical and Applied Mmechanics, 1-19. doi:10.1007/s11012-021-01409-0
    • NLM

      Diaz Izquierdo DO, Marques FD. Experimental analysis of passive bio-inspired covert feathers for stall and post-stall performance enhancement [Internet]. Meccanica: An International Journal of Theoretical and Applied Mmechanics. 2021 ; 1-19.[citado 2025 nov. 08 ] Available from: https://doi.org/10.1007/s11012-021-01409-0
    • Vancouver

      Diaz Izquierdo DO, Marques FD. Experimental analysis of passive bio-inspired covert feathers for stall and post-stall performance enhancement [Internet]. Meccanica: An International Journal of Theoretical and Applied Mmechanics. 2021 ; 1-19.[citado 2025 nov. 08 ] Available from: https://doi.org/10.1007/s11012-021-01409-0
  • 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: 08 nov. 2025.
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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 2025 nov. 08 ] 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 2025 nov. 08 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2021.103730
  • Source: International Journal of Non-Linear Mechanics. Unidade: EESC

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

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      PACHECO, Douglas Ramalho Queiroz e MARQUES, Flavio Donizeti e FERREIRA, Antonio Joaquim Mendes. Panel flutter suppression with nonlinear energy sinks: numerical modeling and analysis. International Journal of Non-Linear Mechanics, v. 106, p. 108-114, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.ijnonlinmec.2018.08.009. Acesso em: 08 nov. 2025.
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      Pacheco, D. R. Q., Marques, F. D., & Ferreira, A. J. M. (2018). Panel flutter suppression with nonlinear energy sinks: numerical modeling and analysis. International Journal of Non-Linear Mechanics, 106, 108-114. doi:10.1016/j.ijnonlinmec.2018.08.009
    • NLM

      Pacheco DRQ, Marques FD, Ferreira AJM. Panel flutter suppression with nonlinear energy sinks: numerical modeling and analysis [Internet]. International Journal of Non-Linear Mechanics. 2018 ; 106 108-114.[citado 2025 nov. 08 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2018.08.009
    • Vancouver

      Pacheco DRQ, Marques FD, Ferreira AJM. Panel flutter suppression with nonlinear energy sinks: numerical modeling and analysis [Internet]. International Journal of Non-Linear Mechanics. 2018 ; 106 108-114.[citado 2025 nov. 08 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2018.08.009
  • Source: Journal of Sound and Vibration. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA MECÂNICA

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      PACHECO, Douglas Ramalho Queiroz e MARQUES, Flavio Donizeti e FERREIRA, Antonio Joaquim Mendes. Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach. Journal of Sound and Vibration, v. 435, p. 135-148, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.jsv.2018.07.042. Acesso em: 08 nov. 2025.
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      Pacheco, D. R. Q., Marques, F. D., & Ferreira, A. J. M. (2018). Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach. Journal of Sound and Vibration, 435, 135-148. doi:10.1016/j.jsv.2018.07.042
    • NLM

      Pacheco DRQ, Marques FD, Ferreira AJM. Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach [Internet]. Journal of Sound and Vibration. 2018 ; 435 135-148.[citado 2025 nov. 08 ] Available from: https://doi.org/10.1016/j.jsv.2018.07.042
    • Vancouver

      Pacheco DRQ, Marques FD, Ferreira AJM. Finite element analysis of fluttering plates reinforced by flexible beams: an energy-based approach [Internet]. Journal of Sound and Vibration. 2018 ; 435 135-148.[citado 2025 nov. 08 ] Available from: https://doi.org/10.1016/j.jsv.2018.07.042
  • Source: Proceedings. Conference titles: International Symposium on Dynamic Problems of Mechanics - DINAME. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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      PEREIRA, Daniel Almeida e SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf. Acesso em: 08 nov. 2025.
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      Pereira, D. A., Santos, C. R. dos, & Marques, F. D. (2017). Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils. In Proceedings. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf
    • NLM

      Pereira DA, Santos CR dos, Marques FD. Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils [Internet]. Proceedings. 2017 ;[citado 2025 nov. 08 ] Available from: https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf
    • Vancouver

      Pereira DA, Santos CR dos, Marques FD. Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils [Internet]. Proceedings. 2017 ;[citado 2025 nov. 08 ] Available from: https://repositorio.usp.br/directbitstream/2944c4eb-e02f-4c63-968d-6fe84db91245/PROD_25662_SYSNO_3123990.pdf
  • Source: Journal of Vibration and Control. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, ANÁLISE DE SÉRIES TEMPORAIS, ENGENHARIA MECÂNICA

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      VASCONCELLOS, Rui Marcos Grombone de et al. Airfoil control surface discontinuous nonlinearity experimental assessment and numerical model validation. Journal of Vibration and Control, v. 22, n. 6, p. 1633-1644, 2016Tradução . . Disponível em: https://doi.org/10.1177/1077546314543911. Acesso em: 08 nov. 2025.
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      Vasconcellos, R. M. G. de, Abdelkefi, A., Hajj, M. R., Almeida, D. P., & Marques, F. D. (2016). Airfoil control surface discontinuous nonlinearity experimental assessment and numerical model validation. Journal of Vibration and Control, 22( 6), 1633-1644. doi:10.1177/1077546314543911
    • NLM

      Vasconcellos RMG de, Abdelkefi A, Hajj MR, Almeida DP, Marques FD. Airfoil control surface discontinuous nonlinearity experimental assessment and numerical model validation [Internet]. Journal of Vibration and Control. 2016 ; 22( 6): 1633-1644.[citado 2025 nov. 08 ] Available from: https://doi.org/10.1177/1077546314543911
    • Vancouver

      Vasconcellos RMG de, Abdelkefi A, Hajj MR, Almeida DP, Marques FD. Airfoil control surface discontinuous nonlinearity experimental assessment and numerical model validation [Internet]. Journal of Vibration and Control. 2016 ; 22( 6): 1633-1644.[citado 2025 nov. 08 ] Available from: https://doi.org/10.1177/1077546314543911
  • Source: Proceedings. Conference titles: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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      PEREIRA, Daniel Almeida e VASCONCELLOS, Rui Marcos Grombone de e MARQUES, Flavio Donizeti. Nonlinear airfoil torsional response induced by separated flows. 2015, Anais.. Reston, VA: AIAA, 2015. Disponível em: https://doi.org/10.2514/6.2015-1423. Acesso em: 08 nov. 2025.
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      Pereira, D. A., Vasconcellos, R. M. G. de, & Marques, F. D. (2015). Nonlinear airfoil torsional response induced by separated flows. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2015-1423
    • NLM

      Pereira DA, Vasconcellos RMG de, Marques FD. Nonlinear airfoil torsional response induced by separated flows [Internet]. Proceedings. 2015 ;[citado 2025 nov. 08 ] Available from: https://doi.org/10.2514/6.2015-1423
    • Vancouver

      Pereira DA, Vasconcellos RMG de, Marques FD. Nonlinear airfoil torsional response induced by separated flows [Internet]. Proceedings. 2015 ;[citado 2025 nov. 08 ] Available from: https://doi.org/10.2514/6.2015-1423
  • Source: Proceedings. Conference titles: International Conference on Structural Dynamics - EURODYN. Unidade: EESC

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

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      PEREIRA, Daniel Almeida e VASCONCELLOS, Rui Marcos Grombone de e MARQUES, Flavio Donizeti. Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils. 2014, Anais.. Porto, Portugal: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2014. Disponível em: https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf. Acesso em: 08 nov. 2025.
    • APA

      Pereira, D. A., Vasconcellos, R. M. G. de, & Marques, F. D. (2014). Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils. In Proceedings. Porto, Portugal: Escola de Engenharia de São Carlos, Universidade de São Paulo. Recuperado de https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf
    • NLM

      Pereira DA, Vasconcellos RMG de, Marques FD. Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils [Internet]. Proceedings. 2014 ;[citado 2025 nov. 08 ] Available from: https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf
    • Vancouver

      Pereira DA, Vasconcellos RMG de, Marques FD. Influence of structural nonlinearities in stall-induced aeroelastic response of pitching airfoils [Internet]. Proceedings. 2014 ;[citado 2025 nov. 08 ] Available from: https://repositorio.usp.br/directbitstream/f8ac4f6e-af7f-4ff6-94a6-3ca03485f916/PROD_25657_SYSNO_3123954.pdf

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