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  • Source: Meccanica. Unidade: EESC

    Subjects: AEROFÓLIOS, MÉTODO DE DIFERENÇAS FINITAS, ENGENHARIA MECÂNICA

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    • ABNT

      TORRES, George Lucas Souto e MARQUES, Flavio Donizeti. Nonlinear geometric decomposition of airfoils into the thickness and camber contributions. Meccanica, v. 59, p. 889-907, 2024Tradução . . Disponível em: https://dx.doi.org/10.1007/s11012-024-01801-6. Acesso em: 12 ago. 2024.
    • APA

      Torres, G. L. S., & Marques, F. D. (2024). Nonlinear geometric decomposition of airfoils into the thickness and camber contributions. Meccanica, 59, 889-907. doi:10.1007/s11012-024-01801-6
    • NLM

      Torres GLS, Marques FD. Nonlinear geometric decomposition of airfoils into the thickness and camber contributions [Internet]. Meccanica. 2024 ; 59 889-907.[citado 2024 ago. 12 ] Available from: https://dx.doi.org/10.1007/s11012-024-01801-6
    • Vancouver

      Torres GLS, Marques FD. Nonlinear geometric decomposition of airfoils into the thickness and camber contributions [Internet]. Meccanica. 2024 ; 59 889-907.[citado 2024 ago. 12 ] Available from: https://dx.doi.org/10.1007/s11012-024-01801-6
  • 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: 12 ago. 2024.
    • APA

      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 2024 ago. 12 ] 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 2024 ago. 12 ] Available from: https://dx.doi.org/10.3390/ASEC2023-15886
  • 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: 12 ago. 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 ago. 12 ] 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 ago. 12 ] Available from: https://doi.org/10.3390/aerospace10070615
  • Source: International Journal of Non-Linear Mechanics. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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    • ABNT

      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: 12 ago. 2024.
    • APA

      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 ago. 12 ] 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 ago. 12 ] 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: 12 ago. 2024.
    • APA

      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 ago. 12 ] 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 ago. 12 ] Available from: https://doi.org/10.1115/1.4050792
  • Source: Journal of Vibration and Control. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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    • ABNT

      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: 12 ago. 2024.
    • APA

      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 ago. 12 ] 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 ago. 12 ] Available from: https://doi.org/10.1177/10775463211000161
  • Source: Journal of Vibration and Control. Unidade: EESC

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

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    • ABNT

      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: 12 ago. 2024.
    • APA

      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 ago. 12 ] 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 ago. 12 ] Available from: https://doi.org/10.1177/1077546319844383
  • Source: Journal of Computational and Nonlinear Dynamics. Unidade: EESC

    Subjects: VENTO, AEROFÓLIOS, BANCO DE DADOS, ENERGIA ELÉTRICA, ENGENHARIA MECÂNICA

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    • ABNT

      SANTOS, Carlos Renan dos e SILVA, Maíra Martins da e MARQUES, Flavio Donizeti. Optimization of energy harvesting from stall-induced oscillations using the multidimensional kriging metamodel. Journal of Computational and Nonlinear Dynamics, v. 14, n. 7, p. 071008-1 - 071008-9, 2019Tradução . . Disponível em: https://doi.org/10.1115/1.4043451. Acesso em: 12 ago. 2024.
    • APA

      Santos, C. R. dos, Silva, M. M. da, & Marques, F. D. (2019). Optimization of energy harvesting from stall-induced oscillations using the multidimensional kriging metamodel. Journal of Computational and Nonlinear Dynamics, 14( 7), 071008-1 - 071008-9. doi:10.1115/1.4043451
    • NLM

      Santos CR dos, Silva MM da, Marques FD. Optimization of energy harvesting from stall-induced oscillations using the multidimensional kriging metamodel [Internet]. Journal of Computational and Nonlinear Dynamics. 2019 ; 14( 7): 071008-1 - 071008-9.[citado 2024 ago. 12 ] Available from: https://doi.org/10.1115/1.4043451
    • Vancouver

      Santos CR dos, Silva MM da, Marques FD. Optimization of energy harvesting from stall-induced oscillations using the multidimensional kriging metamodel [Internet]. Journal of Computational and Nonlinear Dynamics. 2019 ; 14( 7): 071008-1 - 071008-9.[citado 2024 ago. 12 ] Available from: https://doi.org/10.1115/1.4043451
  • Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: EESC

    Subjects: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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    • ABNT

      SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Stall-induced oscillations of typical aeroelastic sections in low airspeeds. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-0610. Acesso em: 12 ago. 2024.
    • APA

      Santos, C. R. dos, & Marques, F. D. (2019). Stall-induced oscillations of typical aeroelastic sections in low airspeeds. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-0610
    • NLM

      Santos CR dos, Marques FD. Stall-induced oscillations of typical aeroelastic sections in low airspeeds [Internet]. Proceedings. 2019 ;[citado 2024 ago. 12 ] Available from: https://doi.org/10.2514/6.2019-0610
    • Vancouver

      Santos CR dos, Marques FD. Stall-induced oscillations of typical aeroelastic sections in low airspeeds [Internet]. Proceedings. 2019 ;[citado 2024 ago. 12 ] Available from: https://doi.org/10.2514/6.2019-0610
  • Source: Proceedings. Conference titles: International Conference on Noise and Vibration Engineering - ISMA. Unidade: EESC

    Subjects: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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      SANTOS, Carlos Renan dos e SILVA, Maíra Martins da e MARQUES, Flavio Donizeti. Metamodel-based optimization of an energy harvester from stall-induced pitching oscillations of airfoils. 2018, Anais.. Leuven, Belgium: KU Leuven, 2018. Disponível em: https://repositorio.usp.br/directbitstream/3bda585e-6e58-40e2-b950-b5c0889d6956/PROD_25663_SYSNO_3124029.pdf. Acesso em: 12 ago. 2024.
    • APA

      Santos, C. R. dos, Silva, M. M. da, & Marques, F. D. (2018). Metamodel-based optimization of an energy harvester from stall-induced pitching oscillations of airfoils. In Proceedings. Leuven, Belgium: KU Leuven. Recuperado de https://repositorio.usp.br/directbitstream/3bda585e-6e58-40e2-b950-b5c0889d6956/PROD_25663_SYSNO_3124029.pdf
    • NLM

      Santos CR dos, Silva MM da, Marques FD. Metamodel-based optimization of an energy harvester from stall-induced pitching oscillations of airfoils [Internet]. Proceedings. 2018 ;[citado 2024 ago. 12 ] Available from: https://repositorio.usp.br/directbitstream/3bda585e-6e58-40e2-b950-b5c0889d6956/PROD_25663_SYSNO_3124029.pdf
    • Vancouver

      Santos CR dos, Silva MM da, Marques FD. Metamodel-based optimization of an energy harvester from stall-induced pitching oscillations of airfoils [Internet]. Proceedings. 2018 ;[citado 2024 ago. 12 ] Available from: https://repositorio.usp.br/directbitstream/3bda585e-6e58-40e2-b950-b5c0889d6956/PROD_25663_SYSNO_3124029.pdf
  • 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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      SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti e HAJJ, Muhammad R. Structural nonlinearities influence on the energy harvesting from stall-induced oscillations. 2018, Anais.. Reston, VA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0464. Acesso em: 12 ago. 2024.
    • APA

      Santos, C. R. dos, Marques, F. D., & Hajj, M. R. (2018). Structural nonlinearities influence on the energy harvesting from stall-induced oscillations. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2018-0464
    • NLM

      Santos CR dos, Marques FD, Hajj MR. Structural nonlinearities influence on the energy harvesting from stall-induced oscillations [Internet]. Proceedings. 2018 ;[citado 2024 ago. 12 ] Available from: https://doi.org/10.2514/6.2018-0464
    • Vancouver

      Santos CR dos, Marques FD, Hajj MR. Structural nonlinearities influence on the energy harvesting from stall-induced oscillations [Internet]. Proceedings. 2018 ;[citado 2024 ago. 12 ] Available from: https://doi.org/10.2514/6.2018-0464
  • Source: Proceedings. Conference titles: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Unidade: EESC

    Subjects: AEROFÓLIOS, HELICÓPTEROS, ENGENHARIA MECÂNICA

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    • ABNT

      SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime. 2018, Anais.. Reston, VA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0463. Acesso em: 12 ago. 2024.
    • APA

      Santos, C. R. dos, & Marques, F. D. (2018). Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime. In Proceedings. Reston, VA: AIAA. doi:10.2514/6.2018-0463
    • NLM

      Santos CR dos, Marques FD. Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime [Internet]. Proceedings. 2018 ;[citado 2024 ago. 12 ] Available from: https://doi.org/10.2514/6.2018-0463
    • Vancouver

      Santos CR dos, Marques FD. Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime [Internet]. Proceedings. 2018 ;[citado 2024 ago. 12 ] Available from: https://doi.org/10.2514/6.2018-0463
  • Source: Engineering Journal of the Military Technical College. Unidade: EESC

    Subjects: AEROFÓLIOS, AERODINÂMICA DE AERONAVES, ENGENHARIA MECÂNICA

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      ZAKARIA, Mohamed Y et al. An experimental assessment of unsteady forces on a plunging airfoil oscillating in stationary fluid at high frequencies. Engineering Journal of the Military Technical College, v. 1, n. 2, p. 58-71, 2017Tradução . . Disponível em: https://doi.org/10.21608/ejmtc.2017.391.1009. Acesso em: 12 ago. 2024.
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      Zakaria, M. Y., Pereira, D. A., Hajj, M. R., Ragab, S. A., & Marques, F. D. (2017). An experimental assessment of unsteady forces on a plunging airfoil oscillating in stationary fluid at high frequencies. Engineering Journal of the Military Technical College, 1( 2), 58-71. doi:10.21608/ejmtc.2017.391.1009
    • NLM

      Zakaria MY, Pereira DA, Hajj MR, Ragab SA, Marques FD. An experimental assessment of unsteady forces on a plunging airfoil oscillating in stationary fluid at high frequencies [Internet]. Engineering Journal of the Military Technical College. 2017 ; 1( 2): 58-71.[citado 2024 ago. 12 ] Available from: https://doi.org/10.21608/ejmtc.2017.391.1009
    • Vancouver

      Zakaria MY, Pereira DA, Hajj MR, Ragab SA, Marques FD. An experimental assessment of unsteady forces on a plunging airfoil oscillating in stationary fluid at high frequencies [Internet]. Engineering Journal of the Military Technical College. 2017 ; 1( 2): 58-71.[citado 2024 ago. 12 ] Available from: https://doi.org/10.21608/ejmtc.2017.391.1009
  • Source: Journal of Sound and Vibration. Unidade: EESC

    Subjects: AEROFÓLIOS, VIBRAÇÕES DE AERONAVES, AEROELASTICIDADE DE AERONAVES

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      VASCONCELLOS, Rui Marcos Grombone de e PEREIRA, Daniel de Almeida e MARQUES, Flávio Donizeti. Characterization of nonlinear behavior of an airfoil under stall-induced pitching oscillations. Journal of Sound and Vibration, v. 372, p. 283-298, 2016Tradução . . Disponível em: https://doi.org/10.1016/j.jsv.2016.02.046. Acesso em: 12 ago. 2024.
    • APA

      Vasconcellos, R. M. G. de, Pereira, D. de A., & Marques, F. D. (2016). Characterization of nonlinear behavior of an airfoil under stall-induced pitching oscillations. Journal of Sound and Vibration, 372, 283-298. doi:10.1016/j.jsv.2016.02.046
    • NLM

      Vasconcellos RMG de, Pereira D de A, Marques FD. Characterization of nonlinear behavior of an airfoil under stall-induced pitching oscillations [Internet]. Journal of Sound and Vibration. 2016 ; 372 283-298.[citado 2024 ago. 12 ] Available from: https://doi.org/10.1016/j.jsv.2016.02.046
    • Vancouver

      Vasconcellos RMG de, Pereira D de A, Marques FD. Characterization of nonlinear behavior of an airfoil under stall-induced pitching oscillations [Internet]. Journal of Sound and Vibration. 2016 ; 372 283-298.[citado 2024 ago. 12 ] Available from: https://doi.org/10.1016/j.jsv.2016.02.046
  • Source: Mathematics in Engineering, Science and Aerospace. Unidade: EESC

    Subjects: SISTEMAS NÃO LINEARES, AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES

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      PEREIRA, Daniel de Almeida et al. Insights on aeroelastic bifurcation phenomena in airfoils with structural nonlinearities. Mathematics in Engineering, Science and Aerospace, v. 6, n. 3, p. 399-424, 2015Tradução . . Disponível em: http://nonlinearstudies.com/index.php/mesa/article/view/1137. Acesso em: 12 ago. 2024.
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      Pereira, D. de A., Vasconcellos, R. M. G. de, Hajj, M. R., & Marques, F. D. (2015). Insights on aeroelastic bifurcation phenomena in airfoils with structural nonlinearities. Mathematics in Engineering, Science and Aerospace, 6( 3), 399-424. Recuperado de http://nonlinearstudies.com/index.php/mesa/article/view/1137
    • NLM

      Pereira D de A, Vasconcellos RMG de, Hajj MR, Marques FD. Insights on aeroelastic bifurcation phenomena in airfoils with structural nonlinearities [Internet]. Mathematics in Engineering, Science and Aerospace. 2015 ; 6( 3): 399-424.[citado 2024 ago. 12 ] Available from: http://nonlinearstudies.com/index.php/mesa/article/view/1137
    • Vancouver

      Pereira D de A, Vasconcellos RMG de, Hajj MR, Marques FD. Insights on aeroelastic bifurcation phenomena in airfoils with structural nonlinearities [Internet]. Mathematics in Engineering, Science and Aerospace. 2015 ; 6( 3): 399-424.[citado 2024 ago. 12 ] Available from: http://nonlinearstudies.com/index.php/mesa/article/view/1137
  • Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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      ZAKARIA, Mohamed Y. et al. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack. 2015, Anais.. Reston, VA, USA: AIAA, 2015. Disponível em: https://doi.org/10.2514/6.2015-3166. Acesso em: 12 ago. 2024.
    • APA

      Zakaria, M. Y., Pereira, D. A., Ragab, S., Hajj, M. R., & Marques, F. D. (2015). An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2015-3166
    • NLM

      Zakaria MY, Pereira DA, Ragab S, Hajj MR, Marques FD. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack [Internet]. Proceedings. 2015 ;[citado 2024 ago. 12 ] Available from: https://doi.org/10.2514/6.2015-3166
    • Vancouver

      Zakaria MY, Pereira DA, Ragab S, Hajj MR, Marques FD. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack [Internet]. Proceedings. 2015 ;[citado 2024 ago. 12 ] Available from: https://doi.org/10.2514/6.2015-3166

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