Filtros : "Embraer. São José dos Campos, SP." Limpar

Filtros



Refine with date range


  • Source: Materials Chemistry and Physics. Unidade: EESC

    Subjects: MATERIAIS, MAGNÉSIO, TERRAS RARAS, CORROSÃO

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      PEREIRA, Gualter Silva et al. Corrosion resistance of WE43 Mg alloy in sodium chloride solution. Materials Chemistry and Physics, v. 272, p. 1-12, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.matchemphys.2021.124930. Acesso em: 09 set. 2024.
    • APA

      Pereira, G. S., Koga, G. Y., Ávila Diaz, J. A., Bittencourt, I. M., Fernandez, F., Miyazaki, M. Y., et al. (2021). Corrosion resistance of WE43 Mg alloy in sodium chloride solution. Materials Chemistry and Physics, 272, 1-12. doi:10.1016/j.matchemphys.2021.124930
    • NLM

      Pereira GS, Koga GY, Ávila Diaz JA, Bittencourt IM, Fernandez F, Miyazaki MY, Botta WJ, Bose Filho WW. Corrosion resistance of WE43 Mg alloy in sodium chloride solution [Internet]. Materials Chemistry and Physics. 2021 ; 272 1-12.[citado 2024 set. 09 ] Available from: https://doi.org/10.1016/j.matchemphys.2021.124930
    • Vancouver

      Pereira GS, Koga GY, Ávila Diaz JA, Bittencourt IM, Fernandez F, Miyazaki MY, Botta WJ, Bose Filho WW. Corrosion resistance of WE43 Mg alloy in sodium chloride solution [Internet]. Materials Chemistry and Physics. 2021 ; 272 1-12.[citado 2024 set. 09 ] Available from: https://doi.org/10.1016/j.matchemphys.2021.124930
  • Source: Proceedings. Conference titles: International Congress and Exhibition on Noise Control Engineering. Unidade: EESC

    Subjects: FUSELAGEM DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA

    PrivadoHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 09 set. 2024.
    • APA

      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 set. 09 ] 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 set. 09 ] 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: International Congress and Exhibition on Noise Control Engineering. Unidade: EESC

    Subjects: FUSELAGEM DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA

    PrivadoHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 09 set. 2024.
    • APA

      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 set. 09 ] 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 set. 09 ] 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: FLAPS, AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

    Versão PublicadaAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 09 set. 2024.
    • APA

      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 set. 09 ] 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 set. 09 ] Available from: https://doi.org/10.2514/6.2018-3799
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 09 set. 2024.
    • APA

      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 set. 09 ] 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 set. 09 ] Available from: https://doi.org/10.2514/6.2018-3593
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidades: EESC, ICMC

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

    PrivadoAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      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: 09 set. 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 set. 09 ] 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 set. 09 ] Available from: https://doi.org/10.2514/6.2018-3458
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidades: EESC, EP

    Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA

    PrivadoHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      MARTÍNEZ ROCAMORA JUNIOR, Bernardo et al. Baseline acoustic levels of the EESC-USP fan rig. 2017, Anais.. Reston, VA, USA: AIAA, 2017. Disponível em: https://repositorio.usp.br/directbitstream/db8ec149-3599-468a-b616-3e81399a078a/trabalho%2003%20-%20Baseline%20Acoustic%20Levels%20of%20the%20EESC-USP%20Fan%20Rig%20%2823rd%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202017%29.pdf. Acesso em: 09 set. 2024.
    • APA

      Martínez Rocamora Junior, B., Greco Júnior, P. C., Caldas, L. C., Baccalá, L. A., Gigena Cuenca, R., & Queiroz, R. L. (2017). Baseline acoustic levels of the EESC-USP fan rig. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/db8ec149-3599-468a-b616-3e81399a078a/trabalho%2003%20-%20Baseline%20Acoustic%20Levels%20of%20the%20EESC-USP%20Fan%20Rig%20%2823rd%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202017%29.pdf
    • NLM

      Martínez Rocamora Junior B, Greco Júnior PC, Caldas LC, Baccalá LA, Gigena Cuenca R, Queiroz RL. Baseline acoustic levels of the EESC-USP fan rig [Internet]. Proceedings. 2017 ;[citado 2024 set. 09 ] Available from: https://repositorio.usp.br/directbitstream/db8ec149-3599-468a-b616-3e81399a078a/trabalho%2003%20-%20Baseline%20Acoustic%20Levels%20of%20the%20EESC-USP%20Fan%20Rig%20%2823rd%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202017%29.pdf
    • Vancouver

      Martínez Rocamora Junior B, Greco Júnior PC, Caldas LC, Baccalá LA, Gigena Cuenca R, Queiroz RL. Baseline acoustic levels of the EESC-USP fan rig [Internet]. Proceedings. 2017 ;[citado 2024 set. 09 ] Available from: https://repositorio.usp.br/directbitstream/db8ec149-3599-468a-b616-3e81399a078a/trabalho%2003%20-%20Baseline%20Acoustic%20Levels%20of%20the%20EESC-USP%20Fan%20Rig%20%2823rd%20AIAA-CEAS%20Aeroacoustics%20Conference%2C%202017%29.pdf
  • Source: Anais. Conference titles: Congresso Nacional de Engenharia Mecânica - CONEM. Unidade: EESC

    Subjects: PROPULSÃO DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA

    Versão PublicadaHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      MASSON, Zargos Neves et al. Desenvolvimento de sistema de controle, aquisição e processamento de sinais para bancada de medição da impedância acústica de liners com escoamento. 2014, Anais.. Rio de Janeiro, RJ: ABCM, 2014. Disponível em: https://repositorio.usp.br/directbitstream/0f750df9-d645-4e7d-8a76-2d3bae992979/trabalho%2028%20-%20Desenvolvimento%20de%20sistema%20de%20controle%2C%20aquisi%C3%A7%C3%A3o%20e%20processamento%20de%20sinais%20para%20bancada%20de%20medi%C3%A7%C3%A3o%20de%20imped%C3%A2ncia%20ac%C3%BAstica%20de%20liners%20com%20escoamento%20%28CONEM%202014%29_removed.pdf. Acesso em: 09 set. 2024.
    • APA

      Masson, Z. N., Serrano, P. G., Medeiros, A. A., Cordioli, J. A., Reis, D. C. dos, & Catalano, F. M. (2014). Desenvolvimento de sistema de controle, aquisição e processamento de sinais para bancada de medição da impedância acústica de liners com escoamento. In Anais. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/0f750df9-d645-4e7d-8a76-2d3bae992979/trabalho%2028%20-%20Desenvolvimento%20de%20sistema%20de%20controle%2C%20aquisi%C3%A7%C3%A3o%20e%20processamento%20de%20sinais%20para%20bancada%20de%20medi%C3%A7%C3%A3o%20de%20imped%C3%A2ncia%20ac%C3%BAstica%20de%20liners%20com%20escoamento%20%28CONEM%202014%29_removed.pdf
    • NLM

      Masson ZN, Serrano PG, Medeiros AA, Cordioli JA, Reis DC dos, Catalano FM. Desenvolvimento de sistema de controle, aquisição e processamento de sinais para bancada de medição da impedância acústica de liners com escoamento [Internet]. Anais. 2014 ;[citado 2024 set. 09 ] Available from: https://repositorio.usp.br/directbitstream/0f750df9-d645-4e7d-8a76-2d3bae992979/trabalho%2028%20-%20Desenvolvimento%20de%20sistema%20de%20controle%2C%20aquisi%C3%A7%C3%A3o%20e%20processamento%20de%20sinais%20para%20bancada%20de%20medi%C3%A7%C3%A3o%20de%20imped%C3%A2ncia%20ac%C3%BAstica%20de%20liners%20com%20escoamento%20%28CONEM%202014%29_removed.pdf
    • Vancouver

      Masson ZN, Serrano PG, Medeiros AA, Cordioli JA, Reis DC dos, Catalano FM. Desenvolvimento de sistema de controle, aquisição e processamento de sinais para bancada de medição da impedância acústica de liners com escoamento [Internet]. Anais. 2014 ;[citado 2024 set. 09 ] Available from: https://repositorio.usp.br/directbitstream/0f750df9-d645-4e7d-8a76-2d3bae992979/trabalho%2028%20-%20Desenvolvimento%20de%20sistema%20de%20controle%2C%20aquisi%C3%A7%C3%A3o%20e%20processamento%20de%20sinais%20para%20bancada%20de%20medi%C3%A7%C3%A3o%20de%20imped%C3%A2ncia%20ac%C3%BAstica%20de%20liners%20com%20escoamento%20%28CONEM%202014%29_removed.pdf
  • Source: International Journal of Engineering Education. Unidade: EESC

    Subjects: ENGENHARIA AERONÁUTICA, ENGENHARIA AERONÁUTICA

    How to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      CATALANO, Fernando Martini e CARMO, Micael. The scientific and technological projects developed between university of São Paulo and Embraer and its impact on engineering education. International Journal of Engineering Education, v. 29, n. 6, p. 1322-1330, 2013Tradução . . Acesso em: 09 set. 2024.
    • APA

      Catalano, F. M., & Carmo, M. (2013). The scientific and technological projects developed between university of São Paulo and Embraer and its impact on engineering education. International Journal of Engineering Education, 29( 6), 1322-1330.
    • NLM

      Catalano FM, Carmo M. The scientific and technological projects developed between university of São Paulo and Embraer and its impact on engineering education. International Journal of Engineering Education. 2013 ; 29( 6): 1322-1330.[citado 2024 set. 09 ]
    • Vancouver

      Catalano FM, Carmo M. The scientific and technological projects developed between university of São Paulo and Embraer and its impact on engineering education. International Journal of Engineering Education. 2013 ; 29( 6): 1322-1330.[citado 2024 set. 09 ]
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: AEROACÚSTICA, FUSELAGEM DE AERONAVES, ENGENHARIA AERONÁUTICA

    PrivadoHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      SIMÕES, Leandro Guilherme Crenite e SOUZA, Daniel Sampaio e MEDEIROS, Marcello Augusto Faraco de. On the small effect of boundary layer thicknesses on slat noise. 2011, Anais.. Reston, VA, USA: AIAA, 2011. Disponível em: https://repositorio.usp.br/directbitstream/183d35df-df3b-4268-8d8b-65e4ba9e660d/trabalho%2043%20-%20On%20the%20Small%20Effect%20of%20Boundary%20Layer%20Thicknesses%20on%20Slat%20Noise%20%2817th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2832nd%20AIAA%20Aeroacoustics%20Conference%29%2C%202011%29.pdf. Acesso em: 09 set. 2024.
    • APA

      Simões, L. G. C., Souza, D. S., & Medeiros, M. A. F. de. (2011). On the small effect of boundary layer thicknesses on slat noise. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/183d35df-df3b-4268-8d8b-65e4ba9e660d/trabalho%2043%20-%20On%20the%20Small%20Effect%20of%20Boundary%20Layer%20Thicknesses%20on%20Slat%20Noise%20%2817th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2832nd%20AIAA%20Aeroacoustics%20Conference%29%2C%202011%29.pdf
    • NLM

      Simões LGC, Souza DS, Medeiros MAF de. On the small effect of boundary layer thicknesses on slat noise [Internet]. Proceedings. 2011 ;[citado 2024 set. 09 ] Available from: https://repositorio.usp.br/directbitstream/183d35df-df3b-4268-8d8b-65e4ba9e660d/trabalho%2043%20-%20On%20the%20Small%20Effect%20of%20Boundary%20Layer%20Thicknesses%20on%20Slat%20Noise%20%2817th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2832nd%20AIAA%20Aeroacoustics%20Conference%29%2C%202011%29.pdf
    • Vancouver

      Simões LGC, Souza DS, Medeiros MAF de. On the small effect of boundary layer thicknesses on slat noise [Internet]. Proceedings. 2011 ;[citado 2024 set. 09 ] Available from: https://repositorio.usp.br/directbitstream/183d35df-df3b-4268-8d8b-65e4ba9e660d/trabalho%2043%20-%20On%20the%20Small%20Effect%20of%20Boundary%20Layer%20Thicknesses%20on%20Slat%20Noise%20%2817th%20AIAA-CEAS%20Aeroacoustics%20Conference%20%2832nd%20AIAA%20Aeroacoustics%20Conference%29%2C%202011%29.pdf
  • Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC

    Subjects: AEROACÚSTICA, TURBULÊNCIA, ENGENHARIA AERONÁUTICA

    PrivadoHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      AFLALO, Bernardo S et al. Comparative analysis of turbulence models for slat noise source calculations employing unstructured meshes. 2010, Anais.. Reston, VA, USA: AIAA, 2010. Disponível em: https://repositorio.usp.br/directbitstream/89bd742a-6526-4bc0-86d6-624d174c8253/trabalho%2049%20-%20Comparative%20Analysis%20of%20Turbulence%20Models%20for%20Slat%20Noise%20Source%20Calculations%20Employing%20Unstructured%20Meshes%20%2816th%20AIAA-CEAS%20Aeroacoustics%20Conference%202010%29.pdf. Acesso em: 09 set. 2024.
    • APA

      Aflalo, B. S., Simões, L. G. C., Silva, R. G. da, & Medeiros, M. A. F. de. (2010). Comparative analysis of turbulence models for slat noise source calculations employing unstructured meshes. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/89bd742a-6526-4bc0-86d6-624d174c8253/trabalho%2049%20-%20Comparative%20Analysis%20of%20Turbulence%20Models%20for%20Slat%20Noise%20Source%20Calculations%20Employing%20Unstructured%20Meshes%20%2816th%20AIAA-CEAS%20Aeroacoustics%20Conference%202010%29.pdf
    • NLM

      Aflalo BS, Simões LGC, Silva RG da, Medeiros MAF de. Comparative analysis of turbulence models for slat noise source calculations employing unstructured meshes [Internet]. Proceedings. 2010 ;[citado 2024 set. 09 ] Available from: https://repositorio.usp.br/directbitstream/89bd742a-6526-4bc0-86d6-624d174c8253/trabalho%2049%20-%20Comparative%20Analysis%20of%20Turbulence%20Models%20for%20Slat%20Noise%20Source%20Calculations%20Employing%20Unstructured%20Meshes%20%2816th%20AIAA-CEAS%20Aeroacoustics%20Conference%202010%29.pdf
    • Vancouver

      Aflalo BS, Simões LGC, Silva RG da, Medeiros MAF de. Comparative analysis of turbulence models for slat noise source calculations employing unstructured meshes [Internet]. Proceedings. 2010 ;[citado 2024 set. 09 ] Available from: https://repositorio.usp.br/directbitstream/89bd742a-6526-4bc0-86d6-624d174c8253/trabalho%2049%20-%20Comparative%20Analysis%20of%20Turbulence%20Models%20for%20Slat%20Noise%20Source%20Calculations%20Employing%20Unstructured%20Meshes%20%2816th%20AIAA-CEAS%20Aeroacoustics%20Conference%202010%29.pdf
  • Source: Journal of the Brazilian Society of Mechanical Sciences and Engineering. Unidade: EESC

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

    Versão PublicadaAcesso à fonteDOIHow to cite
    A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
    • ABNT

      MARTINS, A. L. e CATALANO, Fernando Martini. Drag optimization for transport aircraft mission adaptive wing. Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 24, n. 1, p. [1-8], 2002Tradução . . Disponível em: https://doi.org/10.1590/S1678-58782003000100001. Acesso em: 09 set. 2024.
    • APA

      Martins, A. L., & Catalano, F. M. (2002). Drag optimization for transport aircraft mission adaptive wing. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 24( 1), [1-8]. doi:10.1590/S1678-58782003000100001
    • NLM

      Martins AL, Catalano FM. Drag optimization for transport aircraft mission adaptive wing [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2002 ; 24( 1): [1-8].[citado 2024 set. 09 ] Available from: https://doi.org/10.1590/S1678-58782003000100001
    • Vancouver

      Martins AL, Catalano FM. Drag optimization for transport aircraft mission adaptive wing [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2002 ; 24( 1): [1-8].[citado 2024 set. 09 ] Available from: https://doi.org/10.1590/S1678-58782003000100001

Digital Library of Intellectual Production of Universidade de São Paulo     2012 - 2024