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  • Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC

    Subjects: VOO (ENGENHARIA AERONÁUTICA), ACIDENTES, SIMULADORES DE VOO, ENGENHARIA AERONÁUTICA

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      MACEDO, João Paulo Costa Antunes de e BIDINOTTO, Jorge Henrique e BROMFIELD, Michael A. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data. 2020, Anais.. Reston, VA, USA: AIAA, 2020. Disponível em: https://doi.org/10.2514/6.2020-2911. Acesso em: 12 dez. 2025.
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      Macedo, J. P. C. A. de, Bidinotto, J. H., & Bromfield, M. A. (2020). Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-2911
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      Macedo JPCA de, Bidinotto JH, Bromfield MA. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data [Internet]. Proceedings. 2020 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2020-2911
    • Vancouver

      Macedo JPCA de, Bidinotto JH, Bromfield MA. Loss of control in flight: comparing qualitative pilot opinion with quantitative flight data [Internet]. Proceedings. 2020 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2020-2911
  • Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES

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      BOCCATO, Bruno Ribeiro e BRAVO MOSQUERA, Pedro David e CATALANO, Fernando Martini. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-4200. Acesso em: 12 dez. 2025.
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      Boccato, B. R., Bravo Mosquera, P. D., & Catalano, F. M. (2019). Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-4200
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      Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2019-4200
    • Vancouver

      Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2019-4200
  • 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: 12 dez. 2025.
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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 2025 dez. 12 ] 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 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2019-1867
  • Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES

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      BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3850. Acesso em: 12 dez. 2025.
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      Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3850
    • NLM

      Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2019-3850
    • Vancouver

      Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2019-3850
  • Source: Proceedings. Conference titles: AIAA Aviation Forum. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      MATHIAS, Marlon Sproesser e MEDEIROS, Marcello Augusto Faraco de. Global instability analysis of a boundary layer flow over a small cavity. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3535. Acesso em: 12 dez. 2025.
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      Mathias, M. S., & Medeiros, M. A. F. de. (2019). Global instability analysis of a boundary layer flow over a small cavity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3535
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      Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2019-3535
    • Vancouver

      Mathias MS, Medeiros MAF de. Global instability analysis of a boundary layer flow over a small cavity [Internet]. Proceedings. 2019 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2019-3535
  • Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC

    Subjects: TRANSFERÊNCIA DE CALOR, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      RIBEIRO, Daniel Garcia e BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf. Acesso em: 12 dez. 2025.
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      Ribeiro, D. G., Bravo Mosquera, P. D., & Cerón Muñoz, H. D. (2019). Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
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      Ribeiro DG, Bravo Mosquera PD, Cerón Muñoz HD. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application [Internet]. Proceedings. 2019 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
    • Vancouver

      Ribeiro DG, Bravo Mosquera PD, Cerón Muñoz HD. Heat transfer effects on aerodynamic performance of a S809 airfoil for wind turbine application [Internet]. Proceedings. 2019 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/558bdbaf-a0df-406a-aee5-d60273db8fa1/trabalho%2001%20-%20Heat%20transfer%20effects%20on%20aerodynamic%20performance%20of%20a%20S809%20airfoil%20for%20wind%20turbine%20application%20%28AIAA%20Propulsion%20and%20Energy%202019%20Forum%29.pdf
  • Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: EESC

    Subjects: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA

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      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 dez. 2025.
    • 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
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      Santos CR dos, Marques FD. Stall-induced oscillations of typical aeroelastic sections in low airspeeds [Internet]. Proceedings. 2019 ;[citado 2025 dez. 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 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2019-0610
  • 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 dez. 2025.
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      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
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      Santos CR dos, Marques FD, Hajj MR. Structural nonlinearities influence on the energy harvesting from stall-induced oscillations [Internet]. Proceedings. 2018 ;[citado 2025 dez. 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 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2018-0464
  • Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC

    Subjects: AEROACÚSTICA, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA

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      MATHIAS, Marlon Sproesser e MEDEIROS, Marcello Augusto Faraco de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3386. Acesso em: 12 dez. 2025.
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      Mathias, M. S., & Medeiros, M. A. F. de. (2018). The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3386
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      Mathias MS, Medeiros MAF de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity [Internet]. Proceedings. 2018 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2018-3386
    • Vancouver

      Mathias MS, Medeiros MAF de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity [Internet]. Proceedings. 2018 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2018-3386
  • Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidades: EEL, EESC

    Subjects: ESTRUTURA DE AERONAVES, VOO (ENGENHARIA AERONÁUTICA), ENGENHARIA AERONÁUTICA

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      EGUEA, João Paulo et al. Study on a camber adaptive winglet. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3960. Acesso em: 12 dez. 2025.
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      Eguea, J. P., Catalano, F. M., Abdalla, A. M., Santana, L. de, & Venner, C. H. (2018). Study on a camber adaptive winglet. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3960
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      Eguea JP, Catalano FM, Abdalla AM, Santana L de, Venner CH. Study on a camber adaptive winglet [Internet]. Proceedings. 2018 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2018-3960
    • Vancouver

      Eguea JP, Catalano FM, Abdalla AM, Santana L de, Venner CH. Study on a camber adaptive winglet [Internet]. Proceedings. 2018 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2018-3960
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: HÉLICES DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      REGO, Leandro Falcão Loureiro e PEREIRA, Lourenço Tércio Lima e CATALANO, Fernando Martini. Noise reductions on a pusher propeller configuration through pylon tangential blowing. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-4194. Acesso em: 12 dez. 2025.
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      Rego, L. F. L., Pereira, L. T. L., & Catalano, F. M. (2018). Noise reductions on a pusher propeller configuration through pylon tangential blowing. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-4194
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      Rego LFL, Pereira LTL, Catalano FM. Noise reductions on a pusher propeller configuration through pylon tangential blowing [Internet]. Proceedings. 2018 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2018-4194
    • Vancouver

      Rego LFL, Pereira LTL, Catalano FM. Noise reductions on a pusher propeller configuration through pylon tangential blowing [Internet]. Proceedings. 2018 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2018-4194
  • 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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      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 dez. 2025.
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      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 2025 dez. 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 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2018-0463
  • Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC

    Subjects: TÚNEIS DE VENTO, AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      SERRANO RICO, Juan Carlos et al. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3960. Acesso em: 12 dez. 2025.
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      Serrano Rico, J. C., Amaral, F. R. do, Bresci, C. S., Beraldo, M. M., & Medeiros, M. A. F. de. (2018). Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3960
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      Serrano Rico JC, Amaral FR do, Bresci CS, Beraldo MM, Medeiros MAF de. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC [Internet]. Proceedings. 2018 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2018-3960
    • Vancouver

      Serrano Rico JC, Amaral FR do, Bresci CS, Beraldo MM, Medeiros MAF de. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC [Internet]. Proceedings. 2018 ;[citado 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2018-3960
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidades: EESC, EP

    Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      CALDAS, Luciano Coutinho et al. In-duct rotating beamforming and mode detection of fan noise sources. 2016, Anais.. Reston, VA, USA: AIAA, 2016. Disponível em: https://repositorio.usp.br/directbitstream/4acb8caf-395c-48e9-891b-42a1c246fcaa/trabalho%2007%20-%20%20In-duct%20Rotating%20Beamforming%20and%20Mode%20Detection%20of%20Fan%20Noise%20Sources%20%2822nd%20AIAACEAS%20Aeroacoustics%20Conference%202016%29%20%282%29%20%281%29_removed.pdf. Acesso em: 12 dez. 2025.
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      Caldas, L. C., Herold, G., Greco Júnior, P. C., & Baccalá, L. A. (2016). In-duct rotating beamforming and mode detection of fan noise sources. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/4acb8caf-395c-48e9-891b-42a1c246fcaa/trabalho%2007%20-%20%20In-duct%20Rotating%20Beamforming%20and%20Mode%20Detection%20of%20Fan%20Noise%20Sources%20%2822nd%20AIAACEAS%20Aeroacoustics%20Conference%202016%29%20%282%29%20%281%29_removed.pdf
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      Caldas LC, Herold G, Greco Júnior PC, Baccalá LA. In-duct rotating beamforming and mode detection of fan noise sources [Internet]. Proceedings. 2016 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/4acb8caf-395c-48e9-891b-42a1c246fcaa/trabalho%2007%20-%20%20In-duct%20Rotating%20Beamforming%20and%20Mode%20Detection%20of%20Fan%20Noise%20Sources%20%2822nd%20AIAACEAS%20Aeroacoustics%20Conference%202016%29%20%282%29%20%281%29_removed.pdf
    • Vancouver

      Caldas LC, Herold G, Greco Júnior PC, Baccalá LA. In-duct rotating beamforming and mode detection of fan noise sources [Internet]. Proceedings. 2016 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/4acb8caf-395c-48e9-891b-42a1c246fcaa/trabalho%2007%20-%20%20In-duct%20Rotating%20Beamforming%20and%20Mode%20Detection%20of%20Fan%20Noise%20Sources%20%2822nd%20AIAACEAS%20Aeroacoustics%20Conference%202016%29%20%282%29%20%281%29_removed.pdf
  • Source: Proceedings. Conference titles: AIAA Fluid Dynamics Conference & Exhibit. Unidade: EESC

    Subjects: AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      GAVIRIA MARTÍNEZ, Germán Andrés e MEDEIROS, Marcello Augusto Faraco de. Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9. 2016, Anais.. Reston, VA, USA: AIAA, 2016. Disponível em: https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf. Acesso em: 12 dez. 2025.
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      Gaviria Martínez, G. A., & Medeiros, M. A. F. de. (2016). Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
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      Gaviria Martínez GA, Medeiros MAF de. Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9 [Internet]. Proceedings. 2016 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
    • Vancouver

      Gaviria Martínez GA, Medeiros MAF de. Direct numerical simulation of a wavepacket in a boundary layer at Mach 0.9 [Internet]. Proceedings. 2016 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/df087384-f496-47c5-9df7-634fbd8ac6bb/trabalho%2018%20-%20Direct%20numerical%20simulation%20of%20a%20wavepacket%20in%20a%20boundary%20layer%20at%20Mach%200.9%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
  • Source: Proceedings. Conference titles: AIAA Fluid Dynamics Conference & Exhibit. Unidade: EESC

    Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      AMARAL, Filipe Ramos do e PAGANI JÚNIOR, Carlos do Carmo e MEDEIROS, Marcello Augusto Faraco de. Experiments on slat noise from −6◦ to 18◦ angles of attack. 2016, Anais.. Reston, VA, USA: AIAA, 2016. Disponível em: https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf. Acesso em: 12 dez. 2025.
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      Amaral, F. R. do, Pagani Júnior, C. do C., & Medeiros, M. A. F. de. (2016). Experiments on slat noise from −6◦ to 18◦ angles of attack. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
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      Amaral FR do, Pagani Júnior C do C, Medeiros MAF de. Experiments on slat noise from −6◦ to 18◦ angles of attack [Internet]. Proceedings. 2016 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
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      Amaral FR do, Pagani Júnior C do C, Medeiros MAF de. Experiments on slat noise from −6◦ to 18◦ angles of attack [Internet]. Proceedings. 2016 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/22944961-1231-4c8b-83df-579d6d68e5df/trabalho%2019%20-%20Experiments%20on%20Slat%20Noise%20from%20-6%C2%B0%20to%2018%C2%B0%20Angles%20of%20Attack%20%2846th%20AIAA%20Fluid%20Dynamics%20Conference%2C%202016%29.pdf
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      AMARAL, Filipe Ramos do et al. Experimental study of the effect of a small 2D excrescence placed on the slat cove surface of an airfoil on its acoustic noise. 2015, Anais.. Reston, VA, USA: AIAA, 2015. Disponível em: https://repositorio.usp.br/directbitstream/ac1cb72d-ea75-49d8-bba4-27e0e561cf61/trabalho%2022%20-%20Experimental%20study%20of%20the%20effect%20of%20a%20small%202D%20excrescence%20placed%20on%20the%20slat%20cove%20surface%20of%20an%20airfoil%20on%20its%20acoustic%20noise%20%2821st%20AIAACEAS%20Aeroacoustics%20Conference%202015%29.pdf. Acesso em: 12 dez. 2025.
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      Amaral, F. R. do, Souza, D. S., Pagani Júnior, C. do C., Himeno, F. H. T., & Medeiros, M. A. F. de. (2015). Experimental study of the effect of a small 2D excrescence placed on the slat cove surface of an airfoil on its acoustic noise. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/ac1cb72d-ea75-49d8-bba4-27e0e561cf61/trabalho%2022%20-%20Experimental%20study%20of%20the%20effect%20of%20a%20small%202D%20excrescence%20placed%20on%20the%20slat%20cove%20surface%20of%20an%20airfoil%20on%20its%20acoustic%20noise%20%2821st%20AIAACEAS%20Aeroacoustics%20Conference%202015%29.pdf
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      Amaral FR do, Souza DS, Pagani Júnior C do C, Himeno FHT, Medeiros MAF de. Experimental study of the effect of a small 2D excrescence placed on the slat cove surface of an airfoil on its acoustic noise [Internet]. Proceedings. 2015 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/ac1cb72d-ea75-49d8-bba4-27e0e561cf61/trabalho%2022%20-%20Experimental%20study%20of%20the%20effect%20of%20a%20small%202D%20excrescence%20placed%20on%20the%20slat%20cove%20surface%20of%20an%20airfoil%20on%20its%20acoustic%20noise%20%2821st%20AIAACEAS%20Aeroacoustics%20Conference%202015%29.pdf
    • Vancouver

      Amaral FR do, Souza DS, Pagani Júnior C do C, Himeno FHT, Medeiros MAF de. Experimental study of the effect of a small 2D excrescence placed on the slat cove surface of an airfoil on its acoustic noise [Internet]. Proceedings. 2015 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/ac1cb72d-ea75-49d8-bba4-27e0e561cf61/trabalho%2022%20-%20Experimental%20study%20of%20the%20effect%20of%20a%20small%202D%20excrescence%20placed%20on%20the%20slat%20cove%20surface%20of%20an%20airfoil%20on%20its%20acoustic%20noise%20%2821st%20AIAACEAS%20Aeroacoustics%20Conference%202015%29.pdf
  • 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 dez. 2025.
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      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
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      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 2025 dez. 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 2025 dez. 12 ] Available from: https://doi.org/10.2514/6.2015-3166
  • Source: Proceedings. Conference titles: AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Unidade: EESC

    Subjects: PIEZOELETRICIDADE, ENGENHARIA AERONÁUTICA, ENERGIA, AEROFÓLIOS

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      DIAS, José Augusto de Carvalho e DE MARQUI JÚNIOR, Carlos e ERTURK, Alper. Dimensionless analysis and scaling of a hybrid 3DOF airfoilbased piezoelectric-inductive aeroelastic energy harvester. 2013, Anais.. Reston, VA: AIAA, 2013. Disponível em: https://repositorio.usp.br/directbitstream/db8e9f0f-d1ee-4e22-98f6-11ba03e33e5e/trabalho%2021%20-%20%20Dimensionless%20analysis%20and%20scaling%20of%20a%20hybrid%203DOF%20airfoil-based%20piezoelectric-inductive%20aeroelastic%20energy%20harvester.%20%2854th%20AIAA-ASME-ASCE-AHS-ASC%20Structures%2C%20Structural%20Dynamics%2C%20and%20Materials%20C.pdf. Acesso em: 12 dez. 2025.
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      Dias, J. A. de C., De Marqui Júnior, C., & Erturk, A. (2013). Dimensionless analysis and scaling of a hybrid 3DOF airfoilbased piezoelectric-inductive aeroelastic energy harvester. In Proceedings. Reston, VA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/db8e9f0f-d1ee-4e22-98f6-11ba03e33e5e/trabalho%2021%20-%20%20Dimensionless%20analysis%20and%20scaling%20of%20a%20hybrid%203DOF%20airfoil-based%20piezoelectric-inductive%20aeroelastic%20energy%20harvester.%20%2854th%20AIAA-ASME-ASCE-AHS-ASC%20Structures%2C%20Structural%20Dynamics%2C%20and%20Materials%20C.pdf
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      Dias JA de C, De Marqui Júnior C, Erturk A. Dimensionless analysis and scaling of a hybrid 3DOF airfoilbased piezoelectric-inductive aeroelastic energy harvester [Internet]. Proceedings. 2013 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/db8e9f0f-d1ee-4e22-98f6-11ba03e33e5e/trabalho%2021%20-%20%20Dimensionless%20analysis%20and%20scaling%20of%20a%20hybrid%203DOF%20airfoil-based%20piezoelectric-inductive%20aeroelastic%20energy%20harvester.%20%2854th%20AIAA-ASME-ASCE-AHS-ASC%20Structures%2C%20Structural%20Dynamics%2C%20and%20Materials%20C.pdf
    • Vancouver

      Dias JA de C, De Marqui Júnior C, Erturk A. Dimensionless analysis and scaling of a hybrid 3DOF airfoilbased piezoelectric-inductive aeroelastic energy harvester [Internet]. Proceedings. 2013 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/db8e9f0f-d1ee-4e22-98f6-11ba03e33e5e/trabalho%2021%20-%20%20Dimensionless%20analysis%20and%20scaling%20of%20a%20hybrid%203DOF%20airfoil-based%20piezoelectric-inductive%20aeroelastic%20energy%20harvester.%20%2854th%20AIAA-ASME-ASCE-AHS-ASC%20Structures%2C%20Structural%20Dynamics%2C%20and%20Materials%20C.pdf
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: SLATS, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      SOUZA, Daniel Sampaio e RODRIGUEZ, Daniel e MEDEIROS, Marcello Augusto Faraco de. A study of the sources of slat noise using proper orthogonal decomposition. 2013, Anais.. Reston, VA, USA: AIAA, 2013. Disponível em: https://repositorio.usp.br/directbitstream/fdc144b2-1c1d-4ea3-a1d8-84f66f3a61a1/trabalho%2031%20-%20A%20Study%20of%20the%20Sources%20of%20Slat%20Noise%20using%20Proper%20Orthogonal%20Decomposition%20%2819th%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202013%2C%20Berlin%29.pdf. Acesso em: 12 dez. 2025.
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      Souza, D. S., Rodriguez, D., & Medeiros, M. A. F. de. (2013). A study of the sources of slat noise using proper orthogonal decomposition. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/fdc144b2-1c1d-4ea3-a1d8-84f66f3a61a1/trabalho%2031%20-%20A%20Study%20of%20the%20Sources%20of%20Slat%20Noise%20using%20Proper%20Orthogonal%20Decomposition%20%2819th%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202013%2C%20Berlin%29.pdf
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      Souza DS, Rodriguez D, Medeiros MAF de. A study of the sources of slat noise using proper orthogonal decomposition [Internet]. Proceedings. 2013 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/fdc144b2-1c1d-4ea3-a1d8-84f66f3a61a1/trabalho%2031%20-%20A%20Study%20of%20the%20Sources%20of%20Slat%20Noise%20using%20Proper%20Orthogonal%20Decomposition%20%2819th%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202013%2C%20Berlin%29.pdf
    • Vancouver

      Souza DS, Rodriguez D, Medeiros MAF de. A study of the sources of slat noise using proper orthogonal decomposition [Internet]. Proceedings. 2013 ;[citado 2025 dez. 12 ] Available from: https://repositorio.usp.br/directbitstream/fdc144b2-1c1d-4ea3-a1d8-84f66f3a61a1/trabalho%2031%20-%20A%20Study%20of%20the%20Sources%20of%20Slat%20Noise%20using%20Proper%20Orthogonal%20Decomposition%20%2819th%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202013%2C%20Berlin%29.pdf

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