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  • Source: Journal of Aerospace Technology and Management. Unidade: EESC

    Subjects: AEROACÚSTICA, TURBULÊNCIA, ROTOR, ENGENHARIA AERONÁUTICA

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      LAVAGNINO SANCHEZ, Gino Rodrigo e ALMEIDA, Odenir de e CATALANO, Fernando Martini. Aeroacoustics effects generated by the interaction rotor-airframe in a sUAS. Journal of Aerospace Technology and Management, v. 16, p. 1-13, 2024Tradução . . Disponível em: http://dx.doi.org/10.1590/jatm.v16.1327. Acesso em: 11 dez. 2024.
    • APA

      Lavagnino Sanchez, G. R., Almeida, O. de, & Catalano, F. M. (2024). Aeroacoustics effects generated by the interaction rotor-airframe in a sUAS. Journal of Aerospace Technology and Management, 16, 1-13. doi:10.1590/jatm.v16.1327
    • NLM

      Lavagnino Sanchez GR, Almeida O de, Catalano FM. Aeroacoustics effects generated by the interaction rotor-airframe in a sUAS [Internet]. Journal of Aerospace Technology and Management. 2024 ; 16 1-13.[citado 2024 dez. 11 ] Available from: http://dx.doi.org/10.1590/jatm.v16.1327
    • Vancouver

      Lavagnino Sanchez GR, Almeida O de, Catalano FM. Aeroacoustics effects generated by the interaction rotor-airframe in a sUAS [Internet]. Journal of Aerospace Technology and Management. 2024 ; 16 1-13.[citado 2024 dez. 11 ] Available from: http://dx.doi.org/10.1590/jatm.v16.1327
  • Source: Aerospace. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA

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      BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study. Aerospace, v. 10, n. 7, p. 1-26, 2023Tradução . . Disponível em: https://doi.org/10.3390/aerospace10070651. Acesso em: 11 dez. 2024.
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      Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2023). Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study. Aerospace, 10( 7), 1-26. doi:10.3390/aerospace10070651
    • NLM

      Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study [Internet]. Aerospace. 2023 ; 10( 7): 1-26.[citado 2024 dez. 11 ] Available from: https://doi.org/10.3390/aerospace10070651
    • Vancouver

      Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study [Internet]. Aerospace. 2023 ; 10( 7): 1-26.[citado 2024 dez. 11 ] Available from: https://doi.org/10.3390/aerospace10070651
  • Source: Journal of the Brazilian Society of Mechanical Sciences and Engineering. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner. Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 44, p. 1-22, 2022Tradução . . Disponível em: https://doi.org/10.1007/s40430-022-03924-x. Acesso em: 11 dez. 2024.
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      Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2022). Design, aerodynamic analysis and optimization of a next‑generation commercial airliner. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 44, 1-22. doi:10.1007/s40430-022-03924-x
    • NLM

      Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2022 ; 44 1-22.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1007/s40430-022-03924-x
    • Vancouver

      Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2022 ; 44 1-22.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1007/s40430-022-03924-x
  • Source: Progress in Aerospace Sciences. Unidade: EESC

    Subjects: AVALIAÇÃO AMBIENTAL, COMBUSTÍVEIS, IMPACTOS AMBIENTAIS, ENGENHARIA AERONÁUTICA

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      BRAVO MOSQUERA, Pedro David e CATALANO, Fernando Martini e ZINGG, David W. Unconventional aircraft for civil aviation. Progress in Aerospace Sciences, v. 131, p. 1-29, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.paerosci.2022.100813. Acesso em: 11 dez. 2024.
    • APA

      Bravo Mosquera, P. D., Catalano, F. M., & Zingg, D. W. (2022). Unconventional aircraft for civil aviation. Progress in Aerospace Sciences, 131, 1-29. doi:10.1016/j.paerosci.2022.100813
    • NLM

      Bravo Mosquera PD, Catalano FM, Zingg DW. Unconventional aircraft for civil aviation [Internet]. Progress in Aerospace Sciences. 2022 ; 131 1-29.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1016/j.paerosci.2022.100813
    • Vancouver

      Bravo Mosquera PD, Catalano FM, Zingg DW. Unconventional aircraft for civil aviation [Internet]. Progress in Aerospace Sciences. 2022 ; 131 1-29.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1016/j.paerosci.2022.100813
  • Source: Aerospace Science and Technology. Unidade: EESC

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

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      SILVA, Gabriel Pereira Gouveia da et al. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators. Aerospace Science and Technology, v. 97, p. 1-11, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.105642. Acesso em: 11 dez. 2024.
    • APA

      Silva, G. P. G. da, Eguea, J. P., Croce, J. A. G., & Catalano, F. M. (2020). Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators. Aerospace Science and Technology, 97, 1-11. doi:10.1016/j.ast.2019.105642
    • NLM

      Silva GPG da, Eguea JP, Croce JAG, Catalano FM. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators [Internet]. Aerospace Science and Technology. 2020 ; 97 1-11.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1016/j.ast.2019.105642
    • Vancouver

      Silva GPG da, Eguea JP, Croce JAG, Catalano FM. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators [Internet]. Aerospace Science and Technology. 2020 ; 97 1-11.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1016/j.ast.2019.105642
  • Source: Aerospace Science and Technology. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, COMBUSTÍVEIS, ENGENHARIA AERONÁUTICA

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      EGUEA, João Paulo e SILVA, Gabriel Pereira Gouveia da e CATALANO, Fernando Martini. Fuel efficiency improvement on a business jet using a camber morphing winglet concept. Aerospace Science and Technology, v. 96, p. 1-9, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.105542. Acesso em: 11 dez. 2024.
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      Eguea, J. P., Silva, G. P. G. da, & Catalano, F. M. (2020). Fuel efficiency improvement on a business jet using a camber morphing winglet concept. Aerospace Science and Technology, 96, 1-9. doi:10.1016/j.ast.2019.105542
    • NLM

      Eguea JP, Silva GPG da, Catalano FM. Fuel efficiency improvement on a business jet using a camber morphing winglet concept [Internet]. Aerospace Science and Technology. 2020 ; 96 1-9.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
    • Vancouver

      Eguea JP, Silva GPG da, Catalano FM. Fuel efficiency improvement on a business jet using a camber morphing winglet concept [Internet]. Aerospace Science and Technology. 2020 ; 96 1-9.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
  • Source: Proceedings. Conference titles: International Congress and Exhibition on Noise Control Engineering. Unidade: EESC

    Subjects: FUSELAGEM DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      BOTERO BOLÍVAR, Laura et al. Numerical analysis of the instabilities behind a blunt slat trailing-edge. 2019, Anais.. Madrid, Espanha: SEA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf. Acesso em: 11 dez. 2024.
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      Botero Bolívar, L., Acevedo Giraldo, D., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2019). Numerical analysis of the instabilities behind a blunt slat trailing-edge. In Proceedings. Madrid, Espanha: SEA. Recuperado de https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf
    • NLM

      Botero Bolívar L, Acevedo Giraldo D, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Numerical analysis of the instabilities behind a blunt slat trailing-edge [Internet]. Proceedings. 2019 ;[citado 2024 dez. 11 ] Available from: https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf
    • Vancouver

      Botero Bolívar L, Acevedo Giraldo D, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Numerical analysis of the instabilities behind a blunt slat trailing-edge [Internet]. Proceedings. 2019 ;[citado 2024 dez. 11 ] Available from: https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf
  • 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: 11 dez. 2024.
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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
    • NLM

      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 2024 dez. 11 ] 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 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2019-4200
  • Source: Proceedings. Conference titles: International Congress and Exhibition on Noise Control Engineering. Unidade: EESC

    Subjects: FUSELAGEM DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA

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      ACEVEDO GIRALDO, Daniel et al. Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model. 2019, Anais.. Madrid, Espanha: SEA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf. Acesso em: 11 dez. 2024.
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      Acevedo Giraldo, D., Botero Bolívar, L., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2019). Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model. In Proceedings. Madrid, Espanha: SEA. Recuperado de https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf
    • NLM

      Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model [Internet]. Proceedings. 2019 ;[citado 2024 dez. 11 ] Available from: https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf
    • Vancouver

      Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model [Internet]. Proceedings. 2019 ;[citado 2024 dez. 11 ] Available from: https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AEROACÚSTICA, TERCEIRA DIMENSÃO

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      REIS, Danillo Cafaldo dos et al. A study on the 3D effects of slat cove fillers. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2406. Acesso em: 11 dez. 2024.
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      Reis, D. C. dos, Coelho, E. L. C., Pereira, L. T. L., Catalano, F. M., & Lima, L. S. de M. (2019). A study on the 3D effects of slat cove fillers. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2406
    • NLM

      Reis DC dos, Coelho ELC, Pereira LTL, Catalano FM, Lima LS de M. A study on the 3D effects of slat cove fillers [Internet]. Proceedings. 2019 ;[citado 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2019-2406
    • Vancouver

      Reis DC dos, Coelho ELC, Pereira LTL, Catalano FM, Lima LS de M. A study on the 3D effects of slat cove fillers [Internet]. Proceedings. 2019 ;[citado 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2019-2406
  • Source: Aerospace Science and Technology. Unidade: EESC

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

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      BRAVO MOSQUERA, Pedro David et al. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf. Aerospace Science and Technology, v. 86, p. 497-519, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.01.059. Acesso em: 11 dez. 2024.
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      Bravo Mosquera, P. D., Abdalla, A. M., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf. Aerospace Science and Technology, 86, 497-519. doi:10.1016/j.ast.2019.01.059
    • NLM

      Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf [Internet]. Aerospace Science and Technology. 2019 ; 86 497-519.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
    • Vancouver

      Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf [Internet]. Aerospace Science and Technology. 2019 ; 86 497-519.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
  • Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, SIMULAÇÃO, AEROFÓLIOS, ENGENHARIA MECÂNICA

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      SILVA, Gabriel Pereira Gouveia da e CATALANO, Fernando Martini. Neural network metamodeling for aerodynamic optimization efficiency improvement. 2019, Anais.. São Carlos, SP: EESC-USP, 2019. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1715/1037. Acesso em: 11 dez. 2024.
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      Silva, G. P. G. da, & Catalano, F. M. (2019). Neural network metamodeling for aerodynamic optimization efficiency improvement. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1715/1037
    • NLM

      Silva GPG da, Catalano FM. Neural network metamodeling for aerodynamic optimization efficiency improvement [Internet]. Anais. 2019 ;[citado 2024 dez. 11 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1715/1037
    • Vancouver

      Silva GPG da, Catalano FM. Neural network metamodeling for aerodynamic optimization efficiency improvement [Internet]. Anais. 2019 ;[citado 2024 dez. 11 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1715/1037
  • Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC

    Subjects: AERODINÂMICA, REDES NEURAIS, ALGORITMOS GENÉTICOS, ENGENHARIA MECÂNICA

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      EGUEA, João Paulo e CAURIN, Glauco Augusto de Paula e CATALANO, Fernando Martini. Neural network application for aerodynamic modeling of a variable camber winglet. 2019, Anais.. São Carlos, SP: EESC-USP, 2019. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1814/1007. Acesso em: 11 dez. 2024.
    • APA

      Eguea, J. P., Caurin, G. A. de P., & Catalano, F. M. (2019). Neural network application for aerodynamic modeling of a variable camber winglet. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1814/1007
    • NLM

      Eguea JP, Caurin GA de P, Catalano FM. Neural network application for aerodynamic modeling of a variable camber winglet [Internet]. Anais. 2019 ;[citado 2024 dez. 11 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1814/1007
    • Vancouver

      Eguea JP, Caurin GA de P, Catalano FM. Neural network application for aerodynamic modeling of a variable camber winglet [Internet]. Anais. 2019 ;[citado 2024 dez. 11 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1814/1007
  • 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: 11 dez. 2024.
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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 2024 dez. 11 ] 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 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2019-3850
  • Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC

    Subjects: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA MECÂNICA

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      SILVA, Gabriel Pereira Gouveia da e EGUEA, João Paulo e CATALANO, Fernando Martini. Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip. 2018, Anais.. São Carlos, SP: EESC-USP, 2018. Disponível em: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811. Acesso em: 11 dez. 2024.
    • APA

      Silva, G. P. G. da, Eguea, J. P., & Catalano, F. M. (2018). Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811
    • NLM

      Silva GPG da, Eguea JP, Catalano FM. Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip [Internet]. Anais. 2018 ;[citado 2024 dez. 11 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811
    • Vancouver

      Silva GPG da, Eguea JP, Catalano FM. Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip [Internet]. Anais. 2018 ;[citado 2024 dez. 11 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA

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      BOTERO BOLÍVAR, Laura et al. Parametric analysis of the influence of slat geometry on acoustic noise. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3593. Acesso em: 11 dez. 2024.
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      Botero Bolívar, L., Pereira, L. T. L., Acevedo Giraldo, D., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Parametric analysis of the influence of slat geometry on acoustic noise. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3593
    • NLM

      Botero Bolívar L, Pereira LTL, Acevedo Giraldo D, Catalano FM, Reis DC dos, Coelho ELC. Parametric analysis of the influence of slat geometry on acoustic noise [Internet]. Proceedings. 2018 ;[citado 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2018-3593
    • Vancouver

      Botero Bolívar L, Pereira LTL, Acevedo Giraldo D, Catalano FM, Reis DC dos, Coelho ELC. Parametric analysis of the influence of slat geometry on acoustic noise [Internet]. Proceedings. 2018 ;[citado 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2018-3593
  • Source: Aerospace Science and Technology. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, AERONAVES AGRÍCOLAS, ENGENHARIA AERONÁUTICA

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      BRAVO MOSQUERA, Pedro David et al. Conceptual design and CFD analysis of a new prototype of agricultural aircraft. Aerospace Science and Technology, v. 80, p. 156-176, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2018.07.014. Acesso em: 11 dez. 2024.
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      Bravo Mosquera, P. D., Cerón Muñoz, H. D., Díaz Vázquez, G., & Catalano, F. M. (2018). Conceptual design and CFD analysis of a new prototype of agricultural aircraft. Aerospace Science and Technology, 80, 156-176. doi:10.1016/j.ast.2018.07.014
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      Bravo Mosquera PD, Cerón Muñoz HD, Díaz Vázquez G, Catalano FM. Conceptual design and CFD analysis of a new prototype of agricultural aircraft [Internet]. Aerospace Science and Technology. 2018 ; 80 156-176.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
    • Vancouver

      Bravo Mosquera PD, Cerón Muñoz HD, Díaz Vázquez G, Catalano FM. Conceptual design and CFD analysis of a new prototype of agricultural aircraft [Internet]. Aerospace Science and Technology. 2018 ; 80 156-176.[citado 2024 dez. 11 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: FLAPS, AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      ACEVEDO GIRALDO, Daniel et al. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3799. Acesso em: 11 dez. 2024.
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      Acevedo Giraldo, D., Botero Bolívar, L., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3799
    • NLM

      Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2018-3799
    • Vancouver

      Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2018-3799
  • Source: Proceedings. Conference titles: AAIA Aerospace Sciences Meeting. Unidade: EESC

    Subjects: TRENS DE POUSO, ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES, AEROACÚSTICA

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      REGO, Leandro Falcão Loureiro et al. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0759. Acesso em: 11 dez. 2024.
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      Rego, L. F. L., Pereira, L. T. L., Catalano, F. M., Speth, R., Bent, P., & Fregnani, J. A. (2018). Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-0759
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      Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2018-0759
    • Vancouver

      Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2018-0759
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidades: EESC, ICMC

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

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      PEREIRA, Lourenço Tércio Lima et al. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3458. Acesso em: 11 dez. 2024.
    • APA

      Pereira, L. T. L., Botero Bolívar, L., Araujo, M. T. de, Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3458
    • NLM

      Pereira LTL, Botero Bolívar L, Araujo MT de, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model [Internet]. Proceedings. 2018 ;[citado 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2018-3458
    • Vancouver

      Pereira LTL, Botero Bolívar L, Araujo MT de, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model [Internet]. Proceedings. 2018 ;[citado 2024 dez. 11 ] Available from: https://doi.org/10.2514/6.2018-3458

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