Filtros : "Colômbia" "EESC-SAA" Removidos: "IFSC224" "OVALLOS, FREDY GALVIS" "Barrios populares Medellín: favelas São Paulo" Limpar

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  • Source: Energies. Unidade: EESC

    Subjects: TURBINAS, VIBRAÇÕES DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA

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      PARRA, Hector G. et al. Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil. Energies, v. 16, n. 12, p. 1-22, 2023Tradução . . Disponível em: https://doi.org/10.3390/en16124538. Acesso em: 15 nov. 2024.
    • APA

      Parra, H. G., Cerón Muñoz, H. D., Gomez, W., & Gaona, E. E. (2023). Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil. Energies, 16( 12), 1-22. doi:10.3390/en16124538
    • NLM

      Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil [Internet]. Energies. 2023 ; 16( 12): 1-22.[citado 2024 nov. 15 ] Available from: https://doi.org/10.3390/en16124538
    • Vancouver

      Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil [Internet]. Energies. 2023 ; 16( 12): 1-22.[citado 2024 nov. 15 ] Available from: https://doi.org/10.3390/en16124538
  • Source: Energies. Unidade: EESC

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

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      PARRA, Hector G. et al. Experimental analysis of oscillatory vortex generators in wind turbine blade. Energies, v. 16, n. 11, p. 1-14, 2023Tradução . . Disponível em: https://doi.org/10.3390/en16114343. Acesso em: 15 nov. 2024.
    • APA

      Parra, H. G., Cerón Muñoz, H. D., Gomez, W., & Gaona, E. E. (2023). Experimental analysis of oscillatory vortex generators in wind turbine blade. Energies, 16( 11), 1-14. doi:10.3390/en16114343
    • NLM

      Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of oscillatory vortex generators in wind turbine blade [Internet]. Energies. 2023 ; 16( 11): 1-14.[citado 2024 nov. 15 ] Available from: https://doi.org/10.3390/en16114343
    • Vancouver

      Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of oscillatory vortex generators in wind turbine blade [Internet]. Energies. 2023 ; 16( 11): 1-14.[citado 2024 nov. 15 ] Available from: https://doi.org/10.3390/en16114343
  • Source: International Journal of Distributed Sensor Networks. Unidade: EESC

    Subjects: INTEGRIDADE ESTRUTURAL, ENSAIOS NÃO DESTRUTIVOS, AERONÁUTICA

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      POZO, Francesc et al. Editorial. International Journal of Distributed Sensor Networks. Thousand Oaks, CA, USA: Escola de Engenharia de São Carlos, Universidade de São Paulo. Disponível em: https://doi.org/10.1177/1550147720963270. Acesso em: 15 nov. 2024. , 2020
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      Pozo, F., Tibaduiza, D. A., Torres-Arredondo, M. Á., Varón, M., & Cerón Muñoz, H. D. (2020). Editorial. International Journal of Distributed Sensor Networks. Thousand Oaks, CA, USA: Escola de Engenharia de São Carlos, Universidade de São Paulo. doi:10.1177/1550147720963270
    • NLM

      Pozo F, Tibaduiza DA, Torres-Arredondo MÁ, Varón M, Cerón Muñoz HD. Editorial [Internet]. International Journal of Distributed Sensor Networks. 2020 ; 16( 9): 1-2.[citado 2024 nov. 15 ] Available from: https://doi.org/10.1177/1550147720963270
    • Vancouver

      Pozo F, Tibaduiza DA, Torres-Arredondo MÁ, Varón M, Cerón Muñoz HD. Editorial [Internet]. International Journal of Distributed Sensor Networks. 2020 ; 16( 9): 1-2.[citado 2024 nov. 15 ] Available from: https://doi.org/10.1177/1550147720963270
  • Source: Proceedings. Conference titles: Congreso Latinoamericano de Ingeniería Mecánica - COLIM. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, TURBINAS, ENERGIA EÓLICA, ENGENHARIA AERONÁUTICA

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      PARRA PEÑUELA, Héctor e GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. 2018, Anais.. Pamplona, Colômbia: Universidad Pamplona, 2018. Disponível em: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf. Acesso em: 15 nov. 2024.
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      Parra Peñuela, H., Gómez Rivera, W., & Cerón Muñoz, H. D. (2018). Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. In Proceedings. Pamplona, Colômbia: Universidad Pamplona. Recuperado de https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
    • NLM

      Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
    • Vancouver

      Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
  • Source: International Journal of Applied Enginering Research. Unidade: EESC

    Subjects: AERONAVES NÃO TRIPULADAS, ENGENHARIA AERONÁUTICA

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      WHITE, Philippe et al. Redesign of an experimental Unmanned Aerial Vehicle (UAV) for its conversion into an operational laboratory platform. International Journal of Applied Enginering Research, v. 13, n. 23, p. 16438-16446, 2018Tradução . . Disponível em: https://repositorio.usp.br/directbitstream/b4c197e2-f162-4d99-a5bc-8ea9e8b28e47/artigo%2003%20-%20Redesign%20of%20an%20experimental%20Unmanned%20Aerial%20Vehicle%20%28UAV%29%20for%20its%20conversion%20into%20an%20operational%20laboratory%20platform%20%28INTERNATIONAL%20JOURNAL%20OF%20APPLIED%20ENGINEERING%20RESEARCH%29.pdf. Acesso em: 15 nov. 2024.
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      White, P., Vaca, J., Villalba, J., Martinez, D., Pardo, G., & Cerón Muñoz, H. D. (2018). Redesign of an experimental Unmanned Aerial Vehicle (UAV) for its conversion into an operational laboratory platform. International Journal of Applied Enginering Research, 13( 23), 16438-16446. Recuperado de https://repositorio.usp.br/directbitstream/b4c197e2-f162-4d99-a5bc-8ea9e8b28e47/artigo%2003%20-%20Redesign%20of%20an%20experimental%20Unmanned%20Aerial%20Vehicle%20%28UAV%29%20for%20its%20conversion%20into%20an%20operational%20laboratory%20platform%20%28INTERNATIONAL%20JOURNAL%20OF%20APPLIED%20ENGINEERING%20RESEARCH%29.pdf
    • NLM

      White P, Vaca J, Villalba J, Martinez D, Pardo G, Cerón Muñoz HD. Redesign of an experimental Unmanned Aerial Vehicle (UAV) for its conversion into an operational laboratory platform [Internet]. International Journal of Applied Enginering Research. 2018 ; 13( 23): 16438-16446.[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/b4c197e2-f162-4d99-a5bc-8ea9e8b28e47/artigo%2003%20-%20Redesign%20of%20an%20experimental%20Unmanned%20Aerial%20Vehicle%20%28UAV%29%20for%20its%20conversion%20into%20an%20operational%20laboratory%20platform%20%28INTERNATIONAL%20JOURNAL%20OF%20APPLIED%20ENGINEERING%20RESEARCH%29.pdf
    • Vancouver

      White P, Vaca J, Villalba J, Martinez D, Pardo G, Cerón Muñoz HD. Redesign of an experimental Unmanned Aerial Vehicle (UAV) for its conversion into an operational laboratory platform [Internet]. International Journal of Applied Enginering Research. 2018 ; 13( 23): 16438-16446.[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/b4c197e2-f162-4d99-a5bc-8ea9e8b28e47/artigo%2003%20-%20Redesign%20of%20an%20experimental%20Unmanned%20Aerial%20Vehicle%20%28UAV%29%20for%20its%20conversion%20into%20an%20operational%20laboratory%20platform%20%28INTERNATIONAL%20JOURNAL%20OF%20APPLIED%20ENGINEERING%20RESEARCH%29.pdf
  • Conference titles: Escola de Primavera em Transição e Turbulência. Unidade: EESC

    Subjects: AEROACÚSTICA, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA

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      BERALDO, Matheus Maia et al. Flow quality and brackground noise measurement of the USP-EESC lant wind tunnel. 2018, Anais.. São Paulo, SP: ABCM, 2018. Disponível em: https://repositorio.usp.br/directbitstream/295a002c-0397-4dc3-8a54-2ee20eb46fff/trabalho%2009%20-%20Flow%20quality%20and%20background%20noise%20measurement%20of%20the%20USP-EESC%20LANT%20wind%20tunnel%20%2811th%20Spring%20School%20on%20Transition%20and%20Turbulence%20%28EPTT%202018%29%29_removed.pdf. Acesso em: 15 nov. 2024.
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      Beraldo, M. M., Amaral, F. R. do, Bresci, C. S., Serrano Rico, J. C., & Medeiros, M. A. F. de. (2018). Flow quality and brackground noise measurement of the USP-EESC lant wind tunnel. In . São Paulo, SP: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/295a002c-0397-4dc3-8a54-2ee20eb46fff/trabalho%2009%20-%20Flow%20quality%20and%20background%20noise%20measurement%20of%20the%20USP-EESC%20LANT%20wind%20tunnel%20%2811th%20Spring%20School%20on%20Transition%20and%20Turbulence%20%28EPTT%202018%29%29_removed.pdf
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      Beraldo MM, Amaral FR do, Bresci CS, Serrano Rico JC, Medeiros MAF de. Flow quality and brackground noise measurement of the USP-EESC lant wind tunnel [Internet]. 2018 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/295a002c-0397-4dc3-8a54-2ee20eb46fff/trabalho%2009%20-%20Flow%20quality%20and%20background%20noise%20measurement%20of%20the%20USP-EESC%20LANT%20wind%20tunnel%20%2811th%20Spring%20School%20on%20Transition%20and%20Turbulence%20%28EPTT%202018%29%29_removed.pdf
    • Vancouver

      Beraldo MM, Amaral FR do, Bresci CS, Serrano Rico JC, Medeiros MAF de. Flow quality and brackground noise measurement of the USP-EESC lant wind tunnel [Internet]. 2018 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/295a002c-0397-4dc3-8a54-2ee20eb46fff/trabalho%2009%20-%20Flow%20quality%20and%20background%20noise%20measurement%20of%20the%20USP-EESC%20LANT%20wind%20tunnel%20%2811th%20Spring%20School%20on%20Transition%20and%20Turbulence%20%28EPTT%202018%29%29_removed.pdf
  • Source: Proceedings. Conference titles: Congreso Latinoamericano de Ingeniería Mecánica - COLIM. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, DINÂMICA DOS FLUÍDOS, ENERGIA EÓLICA, ENGENHARIA AERONÁUTICA

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      ORTEGON SARMIENTO, Tatiana e GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío. Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico. 2018, Anais.. Pamplona, Colômbia: Universidad Pamplona, 2018. Disponível em: https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf. Acesso em: 15 nov. 2024.
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      Ortegon Sarmiento, T., Gómez Rivera, W., & Cerón Muñoz, H. D. (2018). Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico. In Proceedings. Pamplona, Colômbia: Universidad Pamplona. Recuperado de https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf
    • NLM

      Ortegon Sarmiento T, Gómez Rivera W, Cerón Muñoz HD. Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico [Internet]. Proceedings. 2018 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf
    • Vancouver

      Ortegon Sarmiento T, Gómez Rivera W, Cerón Muñoz HD. Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico [Internet]. Proceedings. 2018 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf
  • Source: Journal of the Brazilian Society of Mechanical Sciences and Engineering. Unidade: EESC

    Subjects: AEROACÚSTICA, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA

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      AMARAL, Filipe Ramos do e SERRANO RICO, Juan Carlos e MEDEIROS, Marcello Augusto Faraco de. Design of microphone phased arrays for acoustic beamforming. Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 40, p. 1-13, 2018Tradução . . Disponível em: https://doi.org/10.1007/s40430-018-1275-5. Acesso em: 15 nov. 2024.
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      Amaral, F. R. do, Serrano Rico, J. C., & Medeiros, M. A. F. de. (2018). Design of microphone phased arrays for acoustic beamforming. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 40, 1-13. doi:10.1007/s40430-018-1275-5
    • NLM

      Amaral FR do, Serrano Rico JC, Medeiros MAF de. Design of microphone phased arrays for acoustic beamforming [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2018 ; 40 1-13.[citado 2024 nov. 15 ] Available from: https://doi.org/10.1007/s40430-018-1275-5
    • Vancouver

      Amaral FR do, Serrano Rico JC, Medeiros MAF de. Design of microphone phased arrays for acoustic beamforming [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2018 ; 40 1-13.[citado 2024 nov. 15 ] Available from: https://doi.org/10.1007/s40430-018-1275-5
  • Source: Proceedings. Conference titles: International Workshop on Structural Health Monitoring. Unidade: EESC

    Subjects: AERONAVES NÃO TRIPULADAS, ROBÓTICA, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA

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      ANAYA, Maribel et al. Damage classification based on machine learning applications for an unmanned aerial vehicle. 2017, Anais.. Stanford, CA, USA: Stanford University, 2017. Disponível em: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf. Acesso em: 15 nov. 2024.
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      Anaya, M., Cerón Muñoz, H. D., Vitola, J., Tibaduiza, D. A., & Pozo, F. (2017). Damage classification based on machine learning applications for an unmanned aerial vehicle. In Proceedings. Stanford, CA, USA: Stanford University. Recuperado de https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
    • NLM

      Anaya M, Cerón Muñoz HD, Vitola J, Tibaduiza DA, Pozo F. Damage classification based on machine learning applications for an unmanned aerial vehicle [Internet]. Proceedings. 2017 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
    • Vancouver

      Anaya M, Cerón Muñoz HD, Vitola J, Tibaduiza DA, Pozo F. Damage classification based on machine learning applications for an unmanned aerial vehicle [Internet]. Proceedings. 2017 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/8def7de2-b4c3-4430-81be-eeb78bd1b7ce/trabalho%2012%20-%20Damage%20classification%20based%20on%20machine%20learning%20applications%20for%20an%20unmanned%20aerial%20vehicle%20%28The%2011th%20International%20Workshop%20on%20Structural%20Health%20Monitoring%202017%29.pdf
  • Source: Anais. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

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

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      SERRANO RICO, Juan Carlos et al. Design of a low-speed, closed test-section wind-tunnel for aeroacoustic and low-turbulence experiments. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/48fde3c7-6af0-43d4-845a-30a3b86a272c/trabalho%2014%20-%20Design%20of%20a%20Low-Speed%2C%20Closed%20Test-Section%20Wind-Tunnel%20for%20Aeroacoustic%20and%20Low-Turbulence%20Experiments%20%28COBEM%202017%29.pdf. Acesso em: 15 nov. 2024.
    • APA

      Serrano Rico, J. C., Amaral, F. R. do, Bresci, C. S., & Medeiros, M. A. F. de. (2017). Design of a low-speed, closed test-section wind-tunnel for aeroacoustic and low-turbulence experiments. In Anais. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/48fde3c7-6af0-43d4-845a-30a3b86a272c/trabalho%2014%20-%20Design%20of%20a%20Low-Speed%2C%20Closed%20Test-Section%20Wind-Tunnel%20for%20Aeroacoustic%20and%20Low-Turbulence%20Experiments%20%28COBEM%202017%29.pdf
    • NLM

      Serrano Rico JC, Amaral FR do, Bresci CS, Medeiros MAF de. Design of a low-speed, closed test-section wind-tunnel for aeroacoustic and low-turbulence experiments [Internet]. Anais. 2017 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/48fde3c7-6af0-43d4-845a-30a3b86a272c/trabalho%2014%20-%20Design%20of%20a%20Low-Speed%2C%20Closed%20Test-Section%20Wind-Tunnel%20for%20Aeroacoustic%20and%20Low-Turbulence%20Experiments%20%28COBEM%202017%29.pdf
    • Vancouver

      Serrano Rico JC, Amaral FR do, Bresci CS, Medeiros MAF de. Design of a low-speed, closed test-section wind-tunnel for aeroacoustic and low-turbulence experiments [Internet]. Anais. 2017 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/48fde3c7-6af0-43d4-845a-30a3b86a272c/trabalho%2014%20-%20Design%20of%20a%20Low-Speed%2C%20Closed%20Test-Section%20Wind-Tunnel%20for%20Aeroacoustic%20and%20Low-Turbulence%20Experiments%20%28COBEM%202017%29.pdf
  • Source: Journal of Aerospace Technology and Management. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES, ANÁLISE DE DESEMPENHO, CÉLULAS SOLARES, MANUFATURA

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      PEDRAZA BETANCOURTH, Nelson Javier et al. Design and manufacture of a solar-powered unmanned aerial vehicle for civilian surveillance missions. Journal of Aerospace Technology and Management, v. 8, n. 4, p. 385-396, 2016Tradução . . Disponível em: https://doi.org/10.5028/jatm.v8i4.678. Acesso em: 15 nov. 2024.
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      Pedraza Betancourth, N. J., Parra Villamarin, J. E., Vaca Rios, J. J., Bravo Mosquera, P. D., & Cerón Muñoz, H. D. (2016). Design and manufacture of a solar-powered unmanned aerial vehicle for civilian surveillance missions. Journal of Aerospace Technology and Management, 8( 4), 385-396. doi:10.5028/jatm.v8i4.678
    • NLM

      Pedraza Betancourth NJ, Parra Villamarin JE, Vaca Rios JJ, Bravo Mosquera PD, Cerón Muñoz HD. Design and manufacture of a solar-powered unmanned aerial vehicle for civilian surveillance missions [Internet]. Journal of Aerospace Technology and Management. 2016 ; 8( 4): 385-396.[citado 2024 nov. 15 ] Available from: https://doi.org/10.5028/jatm.v8i4.678
    • Vancouver

      Pedraza Betancourth NJ, Parra Villamarin JE, Vaca Rios JJ, Bravo Mosquera PD, Cerón Muñoz HD. Design and manufacture of a solar-powered unmanned aerial vehicle for civilian surveillance missions [Internet]. Journal of Aerospace Technology and Management. 2016 ; 8( 4): 385-396.[citado 2024 nov. 15 ] Available from: https://doi.org/10.5028/jatm.v8i4.678
  • Source: Proceedings of EPTT. Conference titles: ABCM Spring School on Transition and Turbulence. Unidade: EESC

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

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      AMARAL, Filipe Ramos do et al. Array shading applied to beamforming technique for evaluation of slat noise from - 6º to 18º angles of attack. 2016, Anais.. Rio de Janeiro, RJ: ABCM, 2016. Disponível em: https://repositorio.usp.br/directbitstream/a18aeb5a-1b20-4c81-8143-f60f7ef1e523/trabalho%2017%20-%20Array%20shading%20applied%20to%20beamforming%20technique%20for%20evaluation%20of%20slat%20noise%20from%20-6%C2%B0%20to%2018%C2%B0%20angles%20of%20attack%20%28EPTT%202016%29.pdf. Acesso em: 15 nov. 2024.
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      Amaral, F. R. do, Pagani Júnior, C. do C., Himeno, F. H. T., Serrano Rico, J. C., & Medeiros, M. A. F. de. (2016). Array shading applied to beamforming technique for evaluation of slat noise from - 6º to 18º angles of attack. In Proceedings of EPTT. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/a18aeb5a-1b20-4c81-8143-f60f7ef1e523/trabalho%2017%20-%20Array%20shading%20applied%20to%20beamforming%20technique%20for%20evaluation%20of%20slat%20noise%20from%20-6%C2%B0%20to%2018%C2%B0%20angles%20of%20attack%20%28EPTT%202016%29.pdf
    • NLM

      Amaral FR do, Pagani Júnior C do C, Himeno FHT, Serrano Rico JC, Medeiros MAF de. Array shading applied to beamforming technique for evaluation of slat noise from - 6º to 18º angles of attack [Internet]. Proceedings of EPTT. 2016 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/a18aeb5a-1b20-4c81-8143-f60f7ef1e523/trabalho%2017%20-%20Array%20shading%20applied%20to%20beamforming%20technique%20for%20evaluation%20of%20slat%20noise%20from%20-6%C2%B0%20to%2018%C2%B0%20angles%20of%20attack%20%28EPTT%202016%29.pdf
    • Vancouver

      Amaral FR do, Pagani Júnior C do C, Himeno FHT, Serrano Rico JC, Medeiros MAF de. Array shading applied to beamforming technique for evaluation of slat noise from - 6º to 18º angles of attack [Internet]. Proceedings of EPTT. 2016 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/a18aeb5a-1b20-4c81-8143-f60f7ef1e523/trabalho%2017%20-%20Array%20shading%20applied%20to%20beamforming%20technique%20for%20evaluation%20of%20slat%20noise%20from%20-6%C2%B0%20to%2018%C2%B0%20angles%20of%20attack%20%28EPTT%202016%29.pdf
  • Source: International Journal of Mechanical Engineering and Automation. Unidade: EESC

    Subjects: COMBUSTÃO, DIFERENÇAS FINITAS, FOGUETES, ENGENHARIA AERONÁUTICA

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      GÓMEZ, Saulo e MURCIA, Jhonathan e CERÓN MUÑOZ, Hernán Darío. Finite difference method for modelling internal pressure in a solid rocket motor. International Journal of Mechanical Engineering and Automation, v. 2, n. 8, p. 365-369, 2015Tradução . . Acesso em: 15 nov. 2024.
    • APA

      Gómez, S., Murcia, J., & Cerón Muñoz, H. D. (2015). Finite difference method for modelling internal pressure in a solid rocket motor. International Journal of Mechanical Engineering and Automation, 2( 8), 365-369.
    • NLM

      Gómez S, Murcia J, Cerón Muñoz HD. Finite difference method for modelling internal pressure in a solid rocket motor. International Journal of Mechanical Engineering and Automation. 2015 ; 2( 8): 365-369.[citado 2024 nov. 15 ]
    • Vancouver

      Gómez S, Murcia J, Cerón Muñoz HD. Finite difference method for modelling internal pressure in a solid rocket motor. International Journal of Mechanical Engineering and Automation. 2015 ; 2( 8): 365-369.[citado 2024 nov. 15 ]
  • Conference titles: Congreso Iberoamericano de Ingeniería Mecánica - CIBIM. Unidade: EESC

    Subjects: ENERGIA EÓLICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      SALAS LÓPEZ, Cindy Natalia e GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío. Análisis computacional de la influencia de la succión de capa límite sobre el comportamiento aerodinámico de generadores de vórtice fijos en perfil NREL-S809. 2015, Anais.. Guayaquil, Equador: FEIBIM, 2015. . Acesso em: 15 nov. 2024.
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      Salas López, C. N., Gómez Rivera, W., & Cerón Muñoz, H. D. (2015). Análisis computacional de la influencia de la succión de capa límite sobre el comportamiento aerodinámico de generadores de vórtice fijos en perfil NREL-S809. In . Guayaquil, Equador: FEIBIM.
    • NLM

      Salas López CN, Gómez Rivera W, Cerón Muñoz HD. Análisis computacional de la influencia de la succión de capa límite sobre el comportamiento aerodinámico de generadores de vórtice fijos en perfil NREL-S809. 2015 ;[citado 2024 nov. 15 ]
    • Vancouver

      Salas López CN, Gómez Rivera W, Cerón Muñoz HD. Análisis computacional de la influencia de la succión de capa límite sobre el comportamiento aerodinámico de generadores de vórtice fijos en perfil NREL-S809. 2015 ;[citado 2024 nov. 15 ]
  • Source: Anais. Conference titles: Escola de Primavera de Transição e Turbulência - EPTT. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, AEROACÚSTICA, SLATS

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      AMARAL, Filipe Ramos do et al. Estudo experimental do efeito aeroacústico de uma excrescência bidimensional na cova do eslate. 2014, Anais.. Rio de Janeiro: ABCM, 2014. Disponível em: https://repositorio.usp.br/directbitstream/002f696a-6070-4228-9e36-5f054bdee96f/trabalho%2029%20-%20ESTUDO%20EXPERIMENTAL%20DO%20EFEITO%20AEROAC%C3%9ASTICO%20DE%20UMA%20EXCRESC%C3%8ANCIA%20BIDIMENSIONAL%20NA%20COVA%20DO%20ESLATE%20%28EPTT%202014%29_removed.pdf. Acesso em: 15 nov. 2024.
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      Amaral, F. R. do, Souza, D. S., Pagani Júnior, C. do C., Serrano Rico, J. C., Blanco, M., & Medeiros, M. A. F. de. (2014). Estudo experimental do efeito aeroacústico de uma excrescência bidimensional na cova do eslate. In Anais. Rio de Janeiro: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/002f696a-6070-4228-9e36-5f054bdee96f/trabalho%2029%20-%20ESTUDO%20EXPERIMENTAL%20DO%20EFEITO%20AEROAC%C3%9ASTICO%20DE%20UMA%20EXCRESC%C3%8ANCIA%20BIDIMENSIONAL%20NA%20COVA%20DO%20ESLATE%20%28EPTT%202014%29_removed.pdf
    • NLM

      Amaral FR do, Souza DS, Pagani Júnior C do C, Serrano Rico JC, Blanco M, Medeiros MAF de. Estudo experimental do efeito aeroacústico de uma excrescência bidimensional na cova do eslate [Internet]. Anais. 2014 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/002f696a-6070-4228-9e36-5f054bdee96f/trabalho%2029%20-%20ESTUDO%20EXPERIMENTAL%20DO%20EFEITO%20AEROAC%C3%9ASTICO%20DE%20UMA%20EXCRESC%C3%8ANCIA%20BIDIMENSIONAL%20NA%20COVA%20DO%20ESLATE%20%28EPTT%202014%29_removed.pdf
    • Vancouver

      Amaral FR do, Souza DS, Pagani Júnior C do C, Serrano Rico JC, Blanco M, Medeiros MAF de. Estudo experimental do efeito aeroacústico de uma excrescência bidimensional na cova do eslate [Internet]. Anais. 2014 ;[citado 2024 nov. 15 ] Available from: https://repositorio.usp.br/directbitstream/002f696a-6070-4228-9e36-5f054bdee96f/trabalho%2029%20-%20ESTUDO%20EXPERIMENTAL%20DO%20EFEITO%20AEROAC%C3%9ASTICO%20DE%20UMA%20EXCRESC%C3%8ANCIA%20BIDIMENSIONAL%20NA%20COVA%20DO%20ESLATE%20%28EPTT%202014%29_removed.pdf
  • Source: Proceedings. Conference titles: Iberian Latin American Congress on Computational Methods in Engineering = Congresso Ibero-Latino-Americano de Métodos Computacionais em Engenharia (CILAMCE). Unidade: EESC

    Subjects: AEROACÚSTICA, VÓRTICES DOS LÍQUIDOS, EQUAÇÕES DE NAVIER-STOKES, AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA

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      AMARAL, Filipe Ramos do et al. Study of the effect of protusions on the slat noise using beamforming techniques and lattice-boltzmann method. 2014, Anais.. Ouro Preto, MG: ABMEC, 2014. . Acesso em: 15 nov. 2024.
    • APA

      Amaral, F. R. do, Himeno, F. H. T., Souza, D. S., Pagani Júnior, C. do C., Serrano Rico, J. C., & Medeiros, M. A. F. de. (2014). Study of the effect of protusions on the slat noise using beamforming techniques and lattice-boltzmann method. In Proceedings. Ouro Preto, MG: ABMEC.
    • NLM

      Amaral FR do, Himeno FHT, Souza DS, Pagani Júnior C do C, Serrano Rico JC, Medeiros MAF de. Study of the effect of protusions on the slat noise using beamforming techniques and lattice-boltzmann method. Proceedings. 2014 ;[citado 2024 nov. 15 ]
    • Vancouver

      Amaral FR do, Himeno FHT, Souza DS, Pagani Júnior C do C, Serrano Rico JC, Medeiros MAF de. Study of the effect of protusions on the slat noise using beamforming techniques and lattice-boltzmann method. Proceedings. 2014 ;[citado 2024 nov. 15 ]
  • Source: Publicaciones. Conference titles: Congreso Argentino de Ingeniería Aeronáutica. Unidade: EESC

    Subjects: TRAJETÓRIA, SIMULADORES DE VOO, FOGUETES, ENGENHARIA AERONÁUTICA

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      MURCIA, J. et al. Flight path analysis in soundingrocket "libertador I" with computational simulation on three degrees of freedom. 2014, Anais.. Buenos Aires, Argentina: Universidad Nacional de La Plata, 2014. . Acesso em: 15 nov. 2024.
    • APA

      Murcia, J., Gómez, S., Cerón Muñoz, H. D., & Portilla, G. (2014). Flight path analysis in soundingrocket "libertador I" with computational simulation on three degrees of freedom. In Publicaciones. Buenos Aires, Argentina: Universidad Nacional de La Plata.
    • NLM

      Murcia J, Gómez S, Cerón Muñoz HD, Portilla G. Flight path analysis in soundingrocket "libertador I" with computational simulation on three degrees of freedom. Publicaciones. 2014 ;[citado 2024 nov. 15 ]
    • Vancouver

      Murcia J, Gómez S, Cerón Muñoz HD, Portilla G. Flight path analysis in soundingrocket "libertador I" with computational simulation on three degrees of freedom. Publicaciones. 2014 ;[citado 2024 nov. 15 ]
  • Source: Actas del Congreso. Conference titles: Congreso Internacional de Ingenieria Mecánica. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, TURBINAS, ENERGIA EÓLICA, ENGENHARIA AERONÁUTICA

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      GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Análisis computacional del control de la capa límite, en perfiles para uso en turbinas eólicas. 2013, Anais.. Bogotá, Colombia: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2013. . Acesso em: 15 nov. 2024.
    • APA

      Gómez Rivera, W., Cerón Muñoz, H. D., & Catalano, F. M. (2013). Análisis computacional del control de la capa límite, en perfiles para uso en turbinas eólicas. In Actas del Congreso. Bogotá, Colombia: Escola de Engenharia de São Carlos, Universidade de São Paulo.
    • NLM

      Gómez Rivera W, Cerón Muñoz HD, Catalano FM. Análisis computacional del control de la capa límite, en perfiles para uso en turbinas eólicas. Actas del Congreso. 2013 ;[citado 2024 nov. 15 ]
    • Vancouver

      Gómez Rivera W, Cerón Muñoz HD, Catalano FM. Análisis computacional del control de la capa límite, en perfiles para uso en turbinas eólicas. Actas del Congreso. 2013 ;[citado 2024 nov. 15 ]
  • Source: Proceedings. Conference titles: AAIA Aerospace Sciences Meeting. Unidade: EESC

    Subjects: PROJETO DE AERONAVES, ENGENHARIA AERONÁUTICA

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      GIRALDO, A. Felipe et al. Design of an advanced turboprop aircraft for regional operations with ninety passengers. 2013, Anais.. Reston, VA, USA: AIAA, 2013. Disponível em: https://doi.org/10.2514/6.2013-24. Acesso em: 15 nov. 2024.
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      Giraldo, A. F., Parra, J. E., Soler, R. S., Escorcia, M. F., Martínez, J. D., Fuentes, G. A., & Cerón Muñoz, H. D. (2013). Design of an advanced turboprop aircraft for regional operations with ninety passengers. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2013-24
    • NLM

      Giraldo AF, Parra JE, Soler RS, Escorcia MF, Martínez JD, Fuentes GA, Cerón Muñoz HD. Design of an advanced turboprop aircraft for regional operations with ninety passengers [Internet]. Proceedings. 2013 ;[citado 2024 nov. 15 ] Available from: https://doi.org/10.2514/6.2013-24
    • Vancouver

      Giraldo AF, Parra JE, Soler RS, Escorcia MF, Martínez JD, Fuentes GA, Cerón Muñoz HD. Design of an advanced turboprop aircraft for regional operations with ninety passengers [Internet]. Proceedings. 2013 ;[citado 2024 nov. 15 ] Available from: https://doi.org/10.2514/6.2013-24
  • Source: Actas del Congreso. Conference titles: Congreso Internacional en Ciencia y Tecnologia Aeroespacial - CICTA. Unidade: EESC

    Subjects: FOGUETES, AERODINÂMICA DE AERONAVES, DINÂMICA DOS FLUÍDOS COMPUTACIONAL, ENGENHARIA AERONÁUTICA

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      CERÓN MUÑOZ, Hernán Darío et al. Modelación dinámica del sistema de recuperación de un cohete. 2012, Anais.. Bogotá, Colombia: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2012. . Acesso em: 15 nov. 2024.
    • APA

      Cerón Muñoz, H. D., Rojas, F., Gómez, F., Murcia Piñeros, J. O., & Gómez, S. (2012). Modelación dinámica del sistema de recuperación de un cohete. In Actas del Congreso. Bogotá, Colombia: Escola de Engenharia de São Carlos, Universidade de São Paulo.
    • NLM

      Cerón Muñoz HD, Rojas F, Gómez F, Murcia Piñeros JO, Gómez S. Modelación dinámica del sistema de recuperación de un cohete. Actas del Congreso. 2012 ;[citado 2024 nov. 15 ]
    • Vancouver

      Cerón Muñoz HD, Rojas F, Gómez F, Murcia Piñeros JO, Gómez S. Modelación dinámica del sistema de recuperación de un cohete. Actas del Congreso. 2012 ;[citado 2024 nov. 15 ]

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