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Trabalho de evento
Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM] (1998)
Marques, F D; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC
Subjects: TRANSPORTE AÉREO, INTELIGÊNCIA ARTIFICIAL, SISTEMAS NÃO LINEARES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, F D e BELO, Eduardo Morgado. Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM]. 1998, Anais.. Melbourne: ICAS/AIAA, 1998. . Acesso em: 31 out. 2024.
APA
Marques, F. D., & Belo, E. M. (1998). Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM]. In Proceedings. Melbourne: ICAS/AIAA.
NLM
Marques FD, Belo EM. Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM]. Proceedings. 1998 ;[citado 2024 out. 31 ]
Vancouver
Marques FD, Belo EM. Identification of aircraft non-linear dynamics using Volterra series. [CD-ROM]. Proceedings. 1998 ;[citado 2024 out. 31 ]
Trabalho de evento
Numerical and experimental analysis of the effect of a pusher propeller on a wing (1996)
Catalano, Fernando Martini; Maunsell, M G
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC
Subjects: AERODINÂMICA, ANÁLISE EXPERIMENTAL DE ESTRUTURAS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 31 out. 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 out. 31 ] 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 out. 31 ] Available from: https://repositorio.usp.br/directbitstream/d2244396-feed-4503-9f07-f90ac54fb80c/PROD_001628_SYSNO_920090.pdf
Trabalho de evento
Theoretical study of a mission adaptive wing (1996)
Martins, A L; Catalano, Fernando Martini
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC
Subjects: ENGENHARIA DE AERONAVES, AERODINÂMICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARTINS, A L e CATALANO, Fernando Martini. Theoretical study of a mission adaptive wing. 1996, Anais.. Sorrento: Aiaa/Icas, 1996. . Acesso em: 31 out. 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 out. 31 ]
Vancouver
Martins AL, Catalano FM. Theoretical study of a mission adaptive wing. Proceedings. 1996 ;[citado 2024 out. 31 ]
Trabalho de evento
Vibration alleviation of a hingeless helicopter rotor blade by state feedback (1996)
Belo, E M; Maia, A; Marques, F D
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC
Subjects: VIBRAÇÕES, ROTOR, HELICÓPTEROS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 31 out. 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 out. 31 ] 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 out. 31 ] Available from: https://repositorio.usp.br/directbitstream/d69ff488-f584-44b9-bb3a-7e546f3a498c/PROD_000767_SYSNO_912732.pdf
Trabalho de evento
Static and dynamic structural analysis of an amphibious aircraft (1996)
Faria, S C; Canale, Antonio Carlos
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC
Subjects: ENGENHARIA DE AERONAVES, AERODINÂMICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 31 out. 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 out. 31 ]
Vancouver
Faria SC, Canale AC. Static and dynamic structural analysis of an amphibious aircraft. Proceedings. 1996 ;[citado 2024 out. 31 ]
Trabalho de evento
Study of propeller-wing-body interference for a low speed twin-engined pusher configuration (1990)
Maunsell, M G
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC
Assunto: ENGENHARIA DE AERONAVES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 31 out. 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 out. 31 ]
Vancouver
Maunsell MG. Study of propeller-wing-body interference for a low speed twin-engined pusher configuration. Proceedings. 1990 ;[citado 2024 out. 31 ]
Trabalho de evento
Algorithm for decoupling vertical / horizontal motions of non-symmetric rolling aircraft (1990)
Belo, E M; Fortescue, P W
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences. Unidade: EESC
Assunto: ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 31 out. 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 out. 31 ] 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 out. 31 ] Available from: https://repositorio.usp.br/directbitstream/7b1f2454-1aa0-414a-a30b-41b5141588a6/PROD_000761_SYSNO_808638%20%283%29.pdf

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