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Trabalho de evento
Computational simulation of noise generated aerodynamically via DNS and acoustic analogy (2010)
Bergamo, Leandro Fernandes; Gennaro, Elmer Mateus ; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences. Unidade: EESC
Subjects: AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BERGAMO, Leandro Fernandes e GENNARO, Elmer Mateus e MEDEIROS, Marcello Augusto Faraco de. Computational simulation of noise generated aerodynamically via DNS and acoustic analogy. 2010, Anais.. Edinburgh, UK: ICAS, 2010. Disponível em: https://repositorio.usp.br/directbitstream/ac40dddd-2a99-4358-99d0-11f3ac6cfa7c/trabalho%2053%20-%20Computational%20simulation%20of%20noise%20generated%20aerodynamically%20via%20DNS%20and%20acoustic%20analogy%20%28ICAS%202010%29_removed.pdf. Acesso em: 03 out. 2024.
APA
Bergamo, L. F., Gennaro, E. M., & Medeiros, M. A. F. de. (2010). Computational simulation of noise generated aerodynamically via DNS and acoustic analogy. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/ac40dddd-2a99-4358-99d0-11f3ac6cfa7c/trabalho%2053%20-%20Computational%20simulation%20of%20noise%20generated%20aerodynamically%20via%20DNS%20and%20acoustic%20analogy%20%28ICAS%202010%29_removed.pdf
NLM
Bergamo LF, Gennaro EM, Medeiros MAF de. Computational simulation of noise generated aerodynamically via DNS and acoustic analogy [Internet]. Proceedings. 2010 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/ac40dddd-2a99-4358-99d0-11f3ac6cfa7c/trabalho%2053%20-%20Computational%20simulation%20of%20noise%20generated%20aerodynamically%20via%20DNS%20and%20acoustic%20analogy%20%28ICAS%202010%29_removed.pdf
Vancouver
Bergamo LF, Gennaro EM, Medeiros MAF de. Computational simulation of noise generated aerodynamically via DNS and acoustic analogy [Internet]. Proceedings. 2010 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/ac40dddd-2a99-4358-99d0-11f3ac6cfa7c/trabalho%2053%20-%20Computational%20simulation%20of%20noise%20generated%20aerodynamically%20via%20DNS%20and%20acoustic%20analogy%20%28ICAS%202010%29_removed.pdf
Trabalho de evento
The new closed circuit wind tunnel of the aircraft laboratory of University of São Paulo, Brazil (2004)
Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CATALANO, Fernando Martini. The new closed circuit wind tunnel of the aircraft laboratory of University of São Paulo, Brazil. 2004, Anais.. Edinburgh, UK: ICAS, 2004. Disponível em: https://repositorio.usp.br/directbitstream/a8ee1c96-7a01-480f-87a6-4f301d70cc9a/trabalho%2053%20-%20THE%20NEW%20CLOSED%20CIRCUIT%20WIND%20TUNNEL%20OF%20THE%20AIRCRAFT%20LABORATORY%20OF%20UNIVERSITY%20OF%20S%C3%83O%20PAULO%20%28ICAS%202004%29.PDF. Acesso em: 03 out. 2024.
APA
Catalano, F. M. (2004). The new closed circuit wind tunnel of the aircraft laboratory of University of São Paulo, Brazil. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/a8ee1c96-7a01-480f-87a6-4f301d70cc9a/trabalho%2053%20-%20THE%20NEW%20CLOSED%20CIRCUIT%20WIND%20TUNNEL%20OF%20THE%20AIRCRAFT%20LABORATORY%20OF%20UNIVERSITY%20OF%20S%C3%83O%20PAULO%20%28ICAS%202004%29.PDF
NLM
Catalano FM. The new closed circuit wind tunnel of the aircraft laboratory of University of São Paulo, Brazil [Internet]. Proceedings. 2004 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/a8ee1c96-7a01-480f-87a6-4f301d70cc9a/trabalho%2053%20-%20THE%20NEW%20CLOSED%20CIRCUIT%20WIND%20TUNNEL%20OF%20THE%20AIRCRAFT%20LABORATORY%20OF%20UNIVERSITY%20OF%20S%C3%83O%20PAULO%20%28ICAS%202004%29.PDF
Vancouver
Catalano FM. The new closed circuit wind tunnel of the aircraft laboratory of University of São Paulo, Brazil [Internet]. Proceedings. 2004 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/a8ee1c96-7a01-480f-87a6-4f301d70cc9a/trabalho%2053%20-%20THE%20NEW%20CLOSED%20CIRCUIT%20WIND%20TUNNEL%20OF%20THE%20AIRCRAFT%20LABORATORY%20OF%20UNIVERSITY%20OF%20S%C3%83O%20PAULO%20%28ICAS%202004%29.PDF
Trabalho de evento
Study of the effects of synthetic jet actuators on the delay of transition of the boundary layer developed on a flat plate (2004)
Mello, Hilton Carlos de Miranda; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: PROJETO DE AERONAVES, AEROFÓLIOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MELLO, Hilton Carlos de Miranda e CATALANO, Fernando Martini. Study of the effects of synthetic jet actuators on the delay of transition of the boundary layer developed on a flat plate. 2004, Anais.. Edinburgh, UK: ICAS, 2004. Disponível em: https://repositorio.usp.br/directbitstream/e458a1fe-0c53-4f6c-9b6e-156804b70b95/trabalho%2052%20-%20Study%20of%20the%20effects%20of%20synthetic%20jet%20actuator%20on%20the%20transition%20delay%20of%20the%20boundary%20layer%20developed%20on%20a%20flat%20plate%20%28ICAS%202004%29.PDF. Acesso em: 03 out. 2024.
APA
Mello, H. C. de M., & Catalano, F. M. (2004). Study of the effects of synthetic jet actuators on the delay of transition of the boundary layer developed on a flat plate. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/e458a1fe-0c53-4f6c-9b6e-156804b70b95/trabalho%2052%20-%20Study%20of%20the%20effects%20of%20synthetic%20jet%20actuator%20on%20the%20transition%20delay%20of%20the%20boundary%20layer%20developed%20on%20a%20flat%20plate%20%28ICAS%202004%29.PDF
NLM
Mello HC de M, Catalano FM. Study of the effects of synthetic jet actuators on the delay of transition of the boundary layer developed on a flat plate [Internet]. Proceedings. 2004 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/e458a1fe-0c53-4f6c-9b6e-156804b70b95/trabalho%2052%20-%20Study%20of%20the%20effects%20of%20synthetic%20jet%20actuator%20on%20the%20transition%20delay%20of%20the%20boundary%20layer%20developed%20on%20a%20flat%20plate%20%28ICAS%202004%29.PDF
Vancouver
Mello HC de M, Catalano FM. Study of the effects of synthetic jet actuators on the delay of transition of the boundary layer developed on a flat plate [Internet]. Proceedings. 2004 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/e458a1fe-0c53-4f6c-9b6e-156804b70b95/trabalho%2052%20-%20Study%20of%20the%20effects%20of%20synthetic%20jet%20actuator%20on%20the%20transition%20delay%20of%20the%20boundary%20layer%20developed%20on%20a%20flat%20plate%20%28ICAS%202004%29.PDF
Trabalho de evento
The effect of wing tip blowing on the vortex drag (2002)
Coimbra, Rogerio Frauendorf de Faria; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences. Unidade: EESC
Subjects: ASAS DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
COIMBRA, Rogerio Frauendorf de Faria e CATALANO, Fernando Martini. The effect of wing tip blowing on the vortex drag. 2002, Anais.. Edinburgh, UK: ICAS, 2002. Disponível em: https://repositorio.usp.br/directbitstream/dae722bf-f2b1-4c9b-9634-651bd272a597/trabalho%2062%20-%20The%20Effect%20of%20Wing%20Tip%20Blowing%20on%20the%20Vortex%20Drag%20%28ICAS%202002%29%20%281%29.PDF. Acesso em: 03 out. 2024.
APA
Coimbra, R. F. de F., & Catalano, F. M. (2002). The effect of wing tip blowing on the vortex drag. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/dae722bf-f2b1-4c9b-9634-651bd272a597/trabalho%2062%20-%20The%20Effect%20of%20Wing%20Tip%20Blowing%20on%20the%20Vortex%20Drag%20%28ICAS%202002%29%20%281%29.PDF
NLM
Coimbra RF de F, Catalano FM. The effect of wing tip blowing on the vortex drag [Internet]. Proceedings. 2002 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/dae722bf-f2b1-4c9b-9634-651bd272a597/trabalho%2062%20-%20The%20Effect%20of%20Wing%20Tip%20Blowing%20on%20the%20Vortex%20Drag%20%28ICAS%202002%29%20%281%29.PDF
Vancouver
Coimbra RF de F, Catalano FM. The effect of wing tip blowing on the vortex drag [Internet]. Proceedings. 2002 ;[citado 2024 out. 03 ] Available from: https://repositorio.usp.br/directbitstream/dae722bf-f2b1-4c9b-9634-651bd272a597/trabalho%2062%20-%20The%20Effect%20of%20Wing%20Tip%20Blowing%20on%20the%20Vortex%20Drag%20%28ICAS%202002%29%20%281%29.PDF

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