Filtros : "AERODINÂMICA DE AERONAVES" "Proceedings of COBEM" Removido: "CABRAL, EDUARDO LOBO LUSTOSA" Limpar

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  • Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

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

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    • ABNT

      CONSTANZO, Fernão de Melo e CATALANO, Fernando Martini. Theoretical and experimental analysis of the fuselage influence on the wing aerodynamic center position at low speed conditions. 2013, Anais.. Rio de Janeiro, RJ: ABCM, 2013. Disponível em: https://repositorio.usp.br/directbitstream/cea4b79f-d23a-449c-bce7-1f7daa2eae1a/trabalho%2030%20-%20THEORETICAL%20AND%20EXPERIMENTAL%20ANALYSIS%20OF%20THE%20FUSELAGE%20INFLUENCE%20ON%20THE%20WING%20AERODYNAMIC%20CENTER%20POSITION%20AT%20LOW%20SPEED%20CONDITIONS%20%28COBEM%202013%29.pdf. Acesso em: 30 set. 2024.
    • APA

      Constanzo, F. de M., & Catalano, F. M. (2013). Theoretical and experimental analysis of the fuselage influence on the wing aerodynamic center position at low speed conditions. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/cea4b79f-d23a-449c-bce7-1f7daa2eae1a/trabalho%2030%20-%20THEORETICAL%20AND%20EXPERIMENTAL%20ANALYSIS%20OF%20THE%20FUSELAGE%20INFLUENCE%20ON%20THE%20WING%20AERODYNAMIC%20CENTER%20POSITION%20AT%20LOW%20SPEED%20CONDITIONS%20%28COBEM%202013%29.pdf
    • NLM

      Constanzo F de M, Catalano FM. Theoretical and experimental analysis of the fuselage influence on the wing aerodynamic center position at low speed conditions [Internet]. Proceedings of COBEM. 2013 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/cea4b79f-d23a-449c-bce7-1f7daa2eae1a/trabalho%2030%20-%20THEORETICAL%20AND%20EXPERIMENTAL%20ANALYSIS%20OF%20THE%20FUSELAGE%20INFLUENCE%20ON%20THE%20WING%20AERODYNAMIC%20CENTER%20POSITION%20AT%20LOW%20SPEED%20CONDITIONS%20%28COBEM%202013%29.pdf
    • Vancouver

      Constanzo F de M, Catalano FM. Theoretical and experimental analysis of the fuselage influence on the wing aerodynamic center position at low speed conditions [Internet]. Proceedings of COBEM. 2013 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/cea4b79f-d23a-449c-bce7-1f7daa2eae1a/trabalho%2030%20-%20THEORETICAL%20AND%20EXPERIMENTAL%20ANALYSIS%20OF%20THE%20FUSELAGE%20INFLUENCE%20ON%20THE%20WING%20AERODYNAMIC%20CENTER%20POSITION%20AT%20LOW%20SPEED%20CONDITIONS%20%28COBEM%202013%29.pdf
  • Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

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

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    • ABNT

      DIAZ IZQUIERDO, David Orlando e SOLARTE PINEDA, Jhonathan e CERÓN MUÑOZ, Hernán Darío. Aerodynamic study of wingtip devices on non-conventional configuration BWB. 2013, Anais.. Rio de Janeiro, RJ: ABCM, 2013. . Acesso em: 30 set. 2024.
    • APA

      Diaz Izquierdo, D. O., Solarte Pineda, J., & Cerón Muñoz, H. D. (2013). Aerodynamic study of wingtip devices on non-conventional configuration BWB. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM.
    • NLM

      Diaz Izquierdo DO, Solarte Pineda J, Cerón Muñoz HD. Aerodynamic study of wingtip devices on non-conventional configuration BWB. Proceedings of COBEM. 2013 ;[citado 2024 set. 30 ]
    • Vancouver

      Diaz Izquierdo DO, Solarte Pineda J, Cerón Muñoz HD. Aerodynamic study of wingtip devices on non-conventional configuration BWB. Proceedings of COBEM. 2013 ;[citado 2024 set. 30 ]
  • Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

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

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    • ABNT

      CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Aerodynamic interference of power plant system on a blended wing body. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. . Acesso em: 30 set. 2024.
    • APA

      Cerón Muñoz, H. D., & Catalano, F. M. (2011). Aerodynamic interference of power plant system on a blended wing body. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM.
    • NLM

      Cerón Muñoz HD, Catalano FM. Aerodynamic interference of power plant system on a blended wing body. Proceedings of COBEM. 2011 ;[citado 2024 set. 30 ]
    • Vancouver

      Cerón Muñoz HD, Catalano FM. Aerodynamic interference of power plant system on a blended wing body. Proceedings of COBEM. 2011 ;[citado 2024 set. 30 ]
  • Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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    • ABNT

      MOSER, Carlos Anissem Soares e MEDEIROS, Marcello Augusto Faraco de e SILVESTRINI, Jorge Hugo. Large-eddy simulation of noise radiated by a mach 0.9 round jet at high reynolds number. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. Disponível em: https://repositorio.usp.br/directbitstream/270f240d-8f2a-49dd-ae6b-55a78f1b1d2b/trabalho%2045%20-%20Large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.9%20round%20jet%20at%20high%20Reynolds%20number%20%28COBEM%202011%29.pdf. Acesso em: 30 set. 2024.
    • APA

      Moser, C. A. S., Medeiros, M. A. F. de, & Silvestrini, J. H. (2011). Large-eddy simulation of noise radiated by a mach 0.9 round jet at high reynolds number. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/270f240d-8f2a-49dd-ae6b-55a78f1b1d2b/trabalho%2045%20-%20Large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.9%20round%20jet%20at%20high%20Reynolds%20number%20%28COBEM%202011%29.pdf
    • NLM

      Moser CAS, Medeiros MAF de, Silvestrini JH. Large-eddy simulation of noise radiated by a mach 0.9 round jet at high reynolds number [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/270f240d-8f2a-49dd-ae6b-55a78f1b1d2b/trabalho%2045%20-%20Large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.9%20round%20jet%20at%20high%20Reynolds%20number%20%28COBEM%202011%29.pdf
    • Vancouver

      Moser CAS, Medeiros MAF de, Silvestrini JH. Large-eddy simulation of noise radiated by a mach 0.9 round jet at high reynolds number [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/270f240d-8f2a-49dd-ae6b-55a78f1b1d2b/trabalho%2045%20-%20Large-eddy%20simulation%20of%20noise%20radiated%20by%20a%20Mach%200.9%20round%20jet%20at%20high%20Reynolds%20number%20%28COBEM%202011%29.pdf
  • Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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      MORETO, José Roberto e GENNARO, Elmer Mateus e MEDEIROS, Marcello Augusto Faraco de. Direct numerical simulation of a transitional bubble in a compressible boundary layer. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. Disponível em: https://repositorio.usp.br/directbitstream/94d2a140-bd0c-487f-bc64-043d8d54e50c/trabalho%20DIRECT%20NUMERICAL%20SIMULATION%20OF%20A%20TRANSITIONAL%20BUBBLE%20IN%20A%20COMPRESSIBLE%20BOUNDARY%20LAYER%20%28COBEM%202011%29.pdf. Acesso em: 30 set. 2024.
    • APA

      Moreto, J. R., Gennaro, E. M., & Medeiros, M. A. F. de. (2011). Direct numerical simulation of a transitional bubble in a compressible boundary layer. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/94d2a140-bd0c-487f-bc64-043d8d54e50c/trabalho%20DIRECT%20NUMERICAL%20SIMULATION%20OF%20A%20TRANSITIONAL%20BUBBLE%20IN%20A%20COMPRESSIBLE%20BOUNDARY%20LAYER%20%28COBEM%202011%29.pdf
    • NLM

      Moreto JR, Gennaro EM, Medeiros MAF de. Direct numerical simulation of a transitional bubble in a compressible boundary layer [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/94d2a140-bd0c-487f-bc64-043d8d54e50c/trabalho%20DIRECT%20NUMERICAL%20SIMULATION%20OF%20A%20TRANSITIONAL%20BUBBLE%20IN%20A%20COMPRESSIBLE%20BOUNDARY%20LAYER%20%28COBEM%202011%29.pdf
    • Vancouver

      Moreto JR, Gennaro EM, Medeiros MAF de. Direct numerical simulation of a transitional bubble in a compressible boundary layer [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/94d2a140-bd0c-487f-bc64-043d8d54e50c/trabalho%20DIRECT%20NUMERICAL%20SIMULATION%20OF%20A%20TRANSITIONAL%20BUBBLE%20IN%20A%20COMPRESSIBLE%20BOUNDARY%20LAYER%20%28COBEM%202011%29.pdf
  • Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering - COBEM. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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    • ABNT

      SOUZA, Daniel Sampaio e MEDEIROS, Marcello Augusto Faraco de. Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code. 2011, Anais.. Rio de Janeiro, RJ: ABCM, 2011. Disponível em: https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf. Acesso em: 30 set. 2024.
    • APA

      Souza, D. S., & Medeiros, M. A. F. de. (2011). Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code. In Proceedings of COBEM. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf
    • NLM

      Souza DS, Medeiros MAF de. Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf
    • Vancouver

      Souza DS, Medeiros MAF de. Steady aerodynamic simulation of a high-lift geometry by meams of a hybrid euler/integral boundary layer code [Internet]. Proceedings of COBEM. 2011 ;[citado 2024 set. 30 ] Available from: https://repositorio.usp.br/directbitstream/6e49e879-a73f-4d4f-9de3-7fab0c7cc644/trabalho%2047%20-%20Steady%20Aerodynamic%20Simulation%20of%20a%20High-Lift%20Geometry%20by%20Means%20of%20a%20Hybrid%20Euler-IBL%20Code%20%28COBEM%202011%29.pdf
  • Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering. Unidade: EESC

    Assunto: AERODINÂMICA DE AERONAVES

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    • ABNT

      MOSER, Carlos Anissem e MEDEIROS, Marcello Augusto Faraco de e SILVESTRINI, Jorge Hugo. Investigation of mach number effects on aerodynamic noise radiation by subsonic jets. 2009, Anais.. Rio de Janeiro: ABCM, 2009. . Acesso em: 30 set. 2024.
    • APA

      Moser, C. A., Medeiros, M. A. F. de, & Silvestrini, J. H. (2009). Investigation of mach number effects on aerodynamic noise radiation by subsonic jets. In Proceedings of COBEM. Rio de Janeiro: ABCM.
    • NLM

      Moser CA, Medeiros MAF de, Silvestrini JH. Investigation of mach number effects on aerodynamic noise radiation by subsonic jets. Proceedings of COBEM. 2009 ;[citado 2024 set. 30 ]
    • Vancouver

      Moser CA, Medeiros MAF de, Silvestrini JH. Investigation of mach number effects on aerodynamic noise radiation by subsonic jets. Proceedings of COBEM. 2009 ;[citado 2024 set. 30 ]
  • Source: Proceedings of COBEM. Conference titles: International Congress of Mechanical Engineering. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, RUGOSIDADE SUPERFICIAL

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      PAULA, Igor Braga de et al. Effect of an isolated three-dimensional roughness element on the boundary layer transition to turbulence. 2007, Anais.. Brasília: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2007. . Acesso em: 30 set. 2024.
    • APA

      Paula, I. B. de, Würz, W., Mendonça, M. T. de, & Medeiros, M. A. F. de. (2007). Effect of an isolated three-dimensional roughness element on the boundary layer transition to turbulence. In Proceedings of COBEM. Brasília: Escola de Engenharia de São Carlos, Universidade de São Paulo.
    • NLM

      Paula IB de, Würz W, Mendonça MT de, Medeiros MAF de. Effect of an isolated three-dimensional roughness element on the boundary layer transition to turbulence. Proceedings of COBEM. 2007 ;[citado 2024 set. 30 ]
    • Vancouver

      Paula IB de, Würz W, Mendonça MT de, Medeiros MAF de. Effect of an isolated three-dimensional roughness element on the boundary layer transition to turbulence. Proceedings of COBEM. 2007 ;[citado 2024 set. 30 ]

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