Filtros : "EESC-SEM" "Congress of the International Council of the Aeronautical Sciences" Removido: "INTELIGÊNCIA ARTIFICIAL" Limpar

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  • Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC

    Subjects: PLANEJAMENTO DE TRANSPORTES, ENGENHARIA DE AERONAVES

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    • ABNT

      MARTINS, André Luiz e CATALANO, Fernando Martini. Viscous drag optimization for a transport aircraft mission adaptive wing. [CD-ROM]. 1998, Anais.. Melbourne: ICAS/AIAA, 1998. . Acesso em: 29 set. 2024.
    • APA

      Martins, A. L., & Catalano, F. M. (1998). Viscous drag optimization for a transport aircraft mission adaptive wing. [CD-ROM]. In Proceedings. Melbourne: ICAS/AIAA.
    • NLM

      Martins AL, Catalano FM. Viscous drag optimization for a transport aircraft mission adaptive wing. [CD-ROM]. Proceedings. 1998 ;[citado 2024 set. 29 ]
    • Vancouver

      Martins AL, Catalano FM. Viscous drag optimization for a transport aircraft mission adaptive wing. [CD-ROM]. Proceedings. 1998 ;[citado 2024 set. 29 ]
  • Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC

    Subjects: AERODINÂMICA, ANÁLISE EXPERIMENTAL DE ESTRUTURAS

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    • ABNT

      CATALANO, Fernando Martini e MAUNSELL, M G. Numerical and experimental analysis of the effect of a pusher propeller on a wing. 1996, Anais.. Sorrento: Aiaa/Icas, 1996. Disponível em: https://repositorio.usp.br/directbitstream/d2244396-feed-4503-9f07-f90ac54fb80c/PROD_001628_SYSNO_920090.pdf. Acesso em: 29 set. 2024.
    • APA

      Catalano, F. M., & Maunsell, M. G. (1996). Numerical and experimental analysis of the effect of a pusher propeller on a wing. In Proceedings. Sorrento: Aiaa/Icas. Recuperado de https://repositorio.usp.br/directbitstream/d2244396-feed-4503-9f07-f90ac54fb80c/PROD_001628_SYSNO_920090.pdf
    • NLM

      Catalano FM, Maunsell MG. Numerical and experimental analysis of the effect of a pusher propeller on a wing [Internet]. Proceedings. 1996 ;[citado 2024 set. 29 ] Available from: https://repositorio.usp.br/directbitstream/d2244396-feed-4503-9f07-f90ac54fb80c/PROD_001628_SYSNO_920090.pdf
    • Vancouver

      Catalano FM, Maunsell MG. Numerical and experimental analysis of the effect of a pusher propeller on a wing [Internet]. Proceedings. 1996 ;[citado 2024 set. 29 ] Available from: https://repositorio.usp.br/directbitstream/d2244396-feed-4503-9f07-f90ac54fb80c/PROD_001628_SYSNO_920090.pdf
  • Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC

    Subjects: ENGENHARIA DE AERONAVES, AERODINÂMICA

    How to cite
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    • ABNT

      MARTINS, A L e CATALANO, Fernando Martini. Theoretical study of a mission adaptive wing. 1996, Anais.. Sorrento: Aiaa/Icas, 1996. . Acesso em: 29 set. 2024.
    • APA

      Martins, A. L., & Catalano, F. M. (1996). Theoretical study of a mission adaptive wing. In Proceedings. Sorrento: Aiaa/Icas.
    • NLM

      Martins AL, Catalano FM. Theoretical study of a mission adaptive wing. Proceedings. 1996 ;[citado 2024 set. 29 ]
    • Vancouver

      Martins AL, Catalano FM. Theoretical study of a mission adaptive wing. Proceedings. 1996 ;[citado 2024 set. 29 ]
  • Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC

    Subjects: VIBRAÇÕES, ROTOR, HELICÓPTEROS

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    • ABNT

      BELO, E M e MAIA, A e MARQUES, F D. Vibration alleviation of a hingeless helicopter rotor blade by state feedback. 1996, Anais.. Sorrento: Aiaa, 1996. Disponível em: https://repositorio.usp.br/directbitstream/d69ff488-f584-44b9-bb3a-7e546f3a498c/PROD_000767_SYSNO_912732.pdf. Acesso em: 29 set. 2024.
    • APA

      Belo, E. M., Maia, A., & Marques, F. D. (1996). Vibration alleviation of a hingeless helicopter rotor blade by state feedback. In Proceedings. Sorrento: Aiaa. Recuperado de https://repositorio.usp.br/directbitstream/d69ff488-f584-44b9-bb3a-7e546f3a498c/PROD_000767_SYSNO_912732.pdf
    • NLM

      Belo EM, Maia A, Marques FD. Vibration alleviation of a hingeless helicopter rotor blade by state feedback [Internet]. Proceedings. 1996 ;[citado 2024 set. 29 ] Available from: https://repositorio.usp.br/directbitstream/d69ff488-f584-44b9-bb3a-7e546f3a498c/PROD_000767_SYSNO_912732.pdf
    • Vancouver

      Belo EM, Maia A, Marques FD. Vibration alleviation of a hingeless helicopter rotor blade by state feedback [Internet]. Proceedings. 1996 ;[citado 2024 set. 29 ] Available from: https://repositorio.usp.br/directbitstream/d69ff488-f584-44b9-bb3a-7e546f3a498c/PROD_000767_SYSNO_912732.pdf
  • Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC

    Subjects: ENGENHARIA DE AERONAVES, AERODINÂMICA

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    • ABNT

      FARIA, S C e CANALE, Antonio Carlos. Static and dynamic structural analysis of an amphibious aircraft. 1996, Anais.. Sorrento: Aiaa/Icas, 1996. . Acesso em: 29 set. 2024.
    • APA

      Faria, S. C., & Canale, A. C. (1996). Static and dynamic structural analysis of an amphibious aircraft. In Proceedings. Sorrento: Aiaa/Icas.
    • NLM

      Faria SC, Canale AC. Static and dynamic structural analysis of an amphibious aircraft. Proceedings. 1996 ;[citado 2024 set. 29 ]
    • Vancouver

      Faria SC, Canale AC. Static and dynamic structural analysis of an amphibious aircraft. Proceedings. 1996 ;[citado 2024 set. 29 ]
  • Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC

    Assunto: ENGENHARIA DE AERONAVES

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    • ABNT

      MAUNSELL, M G. Study of propeller-wing-body interference for a low speed twin-engined pusher configuration. 1990, Anais.. Washington: Icas, 1990. . Acesso em: 29 set. 2024.
    • APA

      Maunsell, M. G. (1990). Study of propeller-wing-body interference for a low speed twin-engined pusher configuration. In Proceedings. Washington: Icas.
    • NLM

      Maunsell MG. Study of propeller-wing-body interference for a low speed twin-engined pusher configuration. Proceedings. 1990 ;[citado 2024 set. 29 ]
    • Vancouver

      Maunsell MG. Study of propeller-wing-body interference for a low speed twin-engined pusher configuration. Proceedings. 1990 ;[citado 2024 set. 29 ]
  • Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC

    Assunto: ENGENHARIA MECÂNICA

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    • ABNT

      BELO, E M e FORTESCUE, P W. Algorithm for decoupling vertical / horizontal motions of non-symmetric rolling aircraft. 1990, Anais.. Stockholm: Icas, 1990. Disponível em: https://repositorio.usp.br/directbitstream/7b1f2454-1aa0-414a-a30b-41b5141588a6/PROD_000761_SYSNO_808638%20%283%29.pdf. Acesso em: 29 set. 2024.
    • APA

      Belo, E. M., & Fortescue, P. W. (1990). Algorithm for decoupling vertical / horizontal motions of non-symmetric rolling aircraft. In Proceedings. Stockholm: Icas. Recuperado de https://repositorio.usp.br/directbitstream/7b1f2454-1aa0-414a-a30b-41b5141588a6/PROD_000761_SYSNO_808638%20%283%29.pdf
    • NLM

      Belo EM, Fortescue PW. Algorithm for decoupling vertical / horizontal motions of non-symmetric rolling aircraft [Internet]. Proceedings. 1990 ;[citado 2024 set. 29 ] Available from: https://repositorio.usp.br/directbitstream/7b1f2454-1aa0-414a-a30b-41b5141588a6/PROD_000761_SYSNO_808638%20%283%29.pdf
    • Vancouver

      Belo EM, Fortescue PW. Algorithm for decoupling vertical / horizontal motions of non-symmetric rolling aircraft [Internet]. Proceedings. 1990 ;[citado 2024 set. 29 ] Available from: https://repositorio.usp.br/directbitstream/7b1f2454-1aa0-414a-a30b-41b5141588a6/PROD_000761_SYSNO_808638%20%283%29.pdf

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