Filtros : "AAIA Applied Aerodynamics Conference" Removido: "MEDEIROS, MARCELLO AUGUSTO FARACO DE" Limpar

Filtros



Refine with date range


  • Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidades: EEL, EESC

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

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

      EGUEA, João Paulo et al. Study on a camber adaptive winglet. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3960. Acesso em: 21 jul. 2024.
    • APA

      Eguea, J. P., Catalano, F. M., Abdalla, A. M., Santana, L. de, & Venner, C. H. (2018). Study on a camber adaptive winglet. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3960
    • NLM

      Eguea JP, Catalano FM, Abdalla AM, Santana L de, Venner CH. Study on a camber adaptive winglet [Internet]. Proceedings. 2018 ;[citado 2024 jul. 21 ] Available from: https://doi.org/10.2514/6.2018-3960
    • Vancouver

      Eguea JP, Catalano FM, Abdalla AM, Santana L de, Venner CH. Study on a camber adaptive winglet [Internet]. Proceedings. 2018 ;[citado 2024 jul. 21 ] Available from: https://doi.org/10.2514/6.2018-3960
  • Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA

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

      JOUANNET, C. et al. Aeordynamic databased of a subscale demonstrator. 2017, Anais.. Reston, VA, USA: AIAA, 2017. Disponível em: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf. Acesso em: 21 jul. 2024.
    • APA

      Jouannet, C., Lundström, D., Krus, P., Sobron, A., Silva, R. G. A. da, Catalano, F. M., & Greco Júnior, P. C. (2017). Aeordynamic databased of a subscale demonstrator. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
    • NLM

      Jouannet C, Lundström D, Krus P, Sobron A, Silva RGA da, Catalano FM, Greco Júnior PC. Aeordynamic databased of a subscale demonstrator [Internet]. Proceedings. 2017 ;[citado 2024 jul. 21 ] Available from: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
    • Vancouver

      Jouannet C, Lundström D, Krus P, Sobron A, Silva RGA da, Catalano FM, Greco Júnior PC. Aeordynamic databased of a subscale demonstrator [Internet]. Proceedings. 2017 ;[citado 2024 jul. 21 ] Available from: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
  • Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC

    Subjects: AERODINÂMICA DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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

      ZAKARIA, Mohamed Y. et al. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack. 2015, Anais.. Reston, VA, USA: AIAA, 2015. Disponível em: https://doi.org/10.2514/6.2015-3166. Acesso em: 21 jul. 2024.
    • APA

      Zakaria, M. Y., Pereira, D. A., Ragab, S., Hajj, M. R., & Marques, F. D. (2015). An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2015-3166
    • NLM

      Zakaria MY, Pereira DA, Ragab S, Hajj MR, Marques FD. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack [Internet]. Proceedings. 2015 ;[citado 2024 jul. 21 ] Available from: https://doi.org/10.2514/6.2015-3166
    • Vancouver

      Zakaria MY, Pereira DA, Ragab S, Hajj MR, Marques FD. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack [Internet]. Proceedings. 2015 ;[citado 2024 jul. 21 ] Available from: https://doi.org/10.2514/6.2015-3166
  • Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC

    Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA

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

      CAMILO, Elizangela e MARQUES, Flavio Donizeti. Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow. 2008, Anais.. Reston, VA, USA: AIAA, 2008. Disponível em: https://doi.org/10.2514/6.2008-6236. Acesso em: 21 jul. 2024.
    • APA

      Camilo, E., & Marques, F. D. (2008). Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2008-6236
    • NLM

      Camilo E, Marques FD. Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow [Internet]. Proceedings. 2008 ;[citado 2024 jul. 21 ] Available from: https://doi.org/10.2514/6.2008-6236
    • Vancouver

      Camilo E, Marques FD. Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow [Internet]. Proceedings. 2008 ;[citado 2024 jul. 21 ] Available from: https://doi.org/10.2514/6.2008-6236
  • Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC

    Subjects: ESTRUTURA DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA

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

      MARQUES, Flavio Donizeti e NAGAMINE, Renato Kazuki. Non-conventional control approach for intelligent structures. 2001, Anais.. Reston, VA, USA: AIAA, 2001. Disponível em: https://doi.org/10.2514/6.2001-1683. Acesso em: 21 jul. 2024.
    • APA

      Marques, F. D., & Nagamine, R. K. (2001). Non-conventional control approach for intelligent structures. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2001-1683
    • NLM

      Marques FD, Nagamine RK. Non-conventional control approach for intelligent structures [Internet]. Proceedings. 2001 ;[citado 2024 jul. 21 ] Available from: https://doi.org/10.2514/6.2001-1683
    • Vancouver

      Marques FD, Nagamine RK. Non-conventional control approach for intelligent structures [Internet]. Proceedings. 2001 ;[citado 2024 jul. 21 ] Available from: https://doi.org/10.2514/6.2001-1683

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