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Trabalho de evento
Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV (2018)
Daud Filho, Antonio Carlos; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: DINÂMICA DE VOO, ENGENHARIA AERONÁUTICA
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ABNT
DAUD FILHO, Antonio Carlos e BELO, Eduardo Morgado. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf. Acesso em: 10 dez. 2025.
APA
Daud Filho, A. C., & Belo, E. M. (2018). Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
NLM
Daud Filho AC, Belo EM. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV [Internet]. Proceedings. 2018 ;[citado 2025 dez. 10 ] Available from: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
Vancouver
Daud Filho AC, Belo EM. Flight dynamics modeling and trim curves of a conceptual semi-tandem wing VTOL UAV [Internet]. Proceedings. 2018 ;[citado 2025 dez. 10 ] Available from: https://repositorio.usp.br/directbitstream/987dd969-af4d-49be-a001-64ec8719b596/trabalho%2001%20-%20FLIGHT%20DYNAMICS%20MODELING%20AND%20TRIM%20CURVES%20OF%20A%20CONCEPTUAL%20SEMI-TANDEM%20WING%20VTOL%20UAV%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
Trabalho de evento
Pio susceptibility in fly-by-wire systems (2018)
Moura, Herlandson Cardoso de; Porto Alegre, Gabriel Setim; Bidinotto, Jorge Henrique ; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: PILOTAGEM DE AERONAVES, DINÂMICA DE VOO, ENGENHARIA AERONÁUTICA
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ABNT
MOURA, Herlandson Cardoso de et al. Pio susceptibility in fly-by-wire systems. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/41346355-4d19-4c4b-9df3-fe68c5983997/trabalho%2002%20-%20PIO%20Susceptibility%20in%20Fly-by-Wire%20Systems%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf. Acesso em: 10 dez. 2025.
APA
Moura, H. C. de, Porto Alegre, G. S., Bidinotto, J. H., & Belo, E. M. (2018). Pio susceptibility in fly-by-wire systems. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/41346355-4d19-4c4b-9df3-fe68c5983997/trabalho%2002%20-%20PIO%20Susceptibility%20in%20Fly-by-Wire%20Systems%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
NLM
Moura HC de, Porto Alegre GS, Bidinotto JH, Belo EM. Pio susceptibility in fly-by-wire systems [Internet]. Proceedings. 2018 ;[citado 2025 dez. 10 ] Available from: https://repositorio.usp.br/directbitstream/41346355-4d19-4c4b-9df3-fe68c5983997/trabalho%2002%20-%20PIO%20Susceptibility%20in%20Fly-by-Wire%20Systems%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
Vancouver
Moura HC de, Porto Alegre GS, Bidinotto JH, Belo EM. Pio susceptibility in fly-by-wire systems [Internet]. Proceedings. 2018 ;[citado 2025 dez. 10 ] Available from: https://repositorio.usp.br/directbitstream/41346355-4d19-4c4b-9df3-fe68c5983997/trabalho%2002%20-%20PIO%20Susceptibility%20in%20Fly-by-Wire%20Systems%20%2831st%20Congress%20of%20the%20International%20Council%20of%20the%20Aeronautical%20Sciences%29_removed.pdf
Trabalho de evento
Low reynolds propeller meta-model for multidiciplinary optimization (2016)
Tavernari, V. D.; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: HÉLICES DE AERONAVES, AEROFÓLIOS, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
TAVERNARI, V. D. e CATALANO, Fernando Martini. Low reynolds propeller meta-model for multidiciplinary optimization. 2016, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2016. . Acesso em: 10 dez. 2025.
APA
Tavernari, V. D., & Catalano, F. M. (2016). Low reynolds propeller meta-model for multidiciplinary optimization. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Tavernari VD, Catalano FM. Low reynolds propeller meta-model for multidiciplinary optimization. Proceedings. 2016 ;[citado 2025 dez. 10 ]
Vancouver
Tavernari VD, Catalano FM. Low reynolds propeller meta-model for multidiciplinary optimization. Proceedings. 2016 ;[citado 2025 dez. 10 ]
Trabalho de evento
Conceptual and aerodynamic design of a UAV for superficial volcano monitoring (2016)
Bravo Mosquera, Pedro David; Abdalla, Alvaro Martins ; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERONAVES NÃO TRIPULADAS, DINÂMICA DOS FLUÍDOS COMPUTACIONAL, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David et al. Conceptual and aerodynamic design of a UAV for superficial volcano monitoring. 2016, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2016. . Acesso em: 10 dez. 2025.
APA
Bravo Mosquera, P. D., Abdalla, A. M., Cerón Muñoz, H. D., & Catalano, F. M. (2016). Conceptual and aerodynamic design of a UAV for superficial volcano monitoring. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Conceptual and aerodynamic design of a UAV for superficial volcano monitoring. Proceedings. 2016 ;[citado 2025 dez. 10 ]
Vancouver
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Conceptual and aerodynamic design of a UAV for superficial volcano monitoring. Proceedings. 2016 ;[citado 2025 dez. 10 ]
Trabalho de evento
Knowledge-based future combat aircraft optimization (2016)
Munjulury, Raghu Chaitanya; Abdalla, Alvaro Martins ; Staack, Ingo; Krus, Petter
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERONAVES MILITARES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MUNJULURY, Raghu Chaitanya et al. Knowledge-based future combat aircraft optimization. 2016, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2016. . Acesso em: 10 dez. 2025.
APA
Munjulury, R. C., Abdalla, A. M., Staack, I., & Krus, P. (2016). Knowledge-based future combat aircraft optimization. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Munjulury RC, Abdalla AM, Staack I, Krus P. Knowledge-based future combat aircraft optimization. Proceedings. 2016 ;[citado 2025 dez. 10 ]
Vancouver
Munjulury RC, Abdalla AM, Staack I, Krus P. Knowledge-based future combat aircraft optimization. Proceedings. 2016 ;[citado 2025 dez. 10 ]
Trabalho de evento
An application of digital imaging processing for UAV's automatic landing system AID (2014)
Degrande, Mateus Pereira; Moreira, Emilio Eduardo Tressoldi; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: PROCESSAMENTO DIGITAL DE IMAGENS, AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
DEGRANDE, Mateus Pereira e MOREIRA, Emilio Eduardo Tressoldi e BELO, Eduardo Morgado. An application of digital imaging processing for UAV's automatic landing system AID. 2014, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2014. . Acesso em: 10 dez. 2025.
APA
Degrande, M. P., Moreira, E. E. T., & Belo, E. M. (2014). An application of digital imaging processing for UAV's automatic landing system AID. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Degrande MP, Moreira EET, Belo EM. An application of digital imaging processing for UAV's automatic landing system AID. Proceedings. 2014 ;[citado 2025 dez. 10 ]
Vancouver
Degrande MP, Moreira EET, Belo EM. An application of digital imaging processing for UAV's automatic landing system AID. Proceedings. 2014 ;[citado 2025 dez. 10 ]
Trabalho de evento
Computational investigation of icing contamination on airfoil (2012)
Bortholin, Thaís; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AEROFÓLIOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BORTHOLIN, Thaís e CATALANO, Fernando Martini. Computational investigation of icing contamination on airfoil. 2012, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2012. . Acesso em: 10 dez. 2025.
APA
Bortholin, T., & Catalano, F. M. (2012). Computational investigation of icing contamination on airfoil. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Bortholin T, Catalano FM. Computational investigation of icing contamination on airfoil. Proceedings. 2012 ;[citado 2025 dez. 10 ]
Vancouver
Bortholin T, Catalano FM. Computational investigation of icing contamination on airfoil. Proceedings. 2012 ;[citado 2025 dez. 10 ]
Trabalho de evento
Airfoil self noise reduction by application of different types of trailing edge serrations (2012)
Catalano, Fernando Martini ; Santana, Leandro Dantas
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AEROFÓLIOS, RUÍDO DOS TRANSPORTES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CATALANO, Fernando Martini e SANTANA, Leandro Dantas. Airfoil self noise reduction by application of different types of trailing edge serrations. 2012, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2012. . Acesso em: 10 dez. 2025.
APA
Catalano, F. M., & Santana, L. D. (2012). Airfoil self noise reduction by application of different types of trailing edge serrations. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Catalano FM, Santana LD. Airfoil self noise reduction by application of different types of trailing edge serrations. Proceedings. 2012 ;[citado 2025 dez. 10 ]
Vancouver
Catalano FM, Santana LD. Airfoil self noise reduction by application of different types of trailing edge serrations. Proceedings. 2012 ;[citado 2025 dez. 10 ]
Trabalho de evento
The influence of demoiselle aircraft on light and general aviation design (2012)
Abdalla, Alvaro Martins ; Catalano, Fernando Martini ; Greco Júnior, Paulo Celso ; Waterhouse, James Rojas
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERONAVES, DESIGN, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ABDALLA, Alvaro Martins et al. The influence of demoiselle aircraft on light and general aviation design. 2012, Anais.. Edinburgh, UK: ICAS, 2012. Disponível em: https://repositorio.usp.br/directbitstream/acb8db00-b3b3-48b1-b9b8-a0084db1d7df/trabalho%2035%20-%20THE%20INFLUENCE%20OF%20DEMOISELLE%20AIRCRAFT%20ON%20LIGHT%20AND%20GENERAL%20AVIATION%20DESIGN%20%28ICAS%202012%29.pdf. Acesso em: 10 dez. 2025.
APA
Abdalla, A. M., Catalano, F. M., Greco Júnior, P. C., & Waterhouse, J. R. (2012). The influence of demoiselle aircraft on light and general aviation design. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/acb8db00-b3b3-48b1-b9b8-a0084db1d7df/trabalho%2035%20-%20THE%20INFLUENCE%20OF%20DEMOISELLE%20AIRCRAFT%20ON%20LIGHT%20AND%20GENERAL%20AVIATION%20DESIGN%20%28ICAS%202012%29.pdf
NLM
Abdalla AM, Catalano FM, Greco Júnior PC, Waterhouse JR. The influence of demoiselle aircraft on light and general aviation design [Internet]. Proceedings. 2012 ;[citado 2025 dez. 10 ] Available from: https://repositorio.usp.br/directbitstream/acb8db00-b3b3-48b1-b9b8-a0084db1d7df/trabalho%2035%20-%20THE%20INFLUENCE%20OF%20DEMOISELLE%20AIRCRAFT%20ON%20LIGHT%20AND%20GENERAL%20AVIATION%20DESIGN%20%28ICAS%202012%29.pdf
Vancouver
Abdalla AM, Catalano FM, Greco Júnior PC, Waterhouse JR. The influence of demoiselle aircraft on light and general aviation design [Internet]. Proceedings. 2012 ;[citado 2025 dez. 10 ] Available from: https://repositorio.usp.br/directbitstream/acb8db00-b3b3-48b1-b9b8-a0084db1d7df/trabalho%2035%20-%20THE%20INFLUENCE%20OF%20DEMOISELLE%20AIRCRAFT%20ON%20LIGHT%20AND%20GENERAL%20AVIATION%20DESIGN%20%28ICAS%202012%29.pdf
Trabalho de evento
The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing (2010)
Santana, Leandro Dantas; Catalano, Fernando Martini ; Medeiros, Marcello Augusto Faraco de ; Carmo, Micael
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AEROACÚSTICA, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SANTANA, Leandro Dantas et al. The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing. 2010, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2010. . Acesso em: 10 dez. 2025.
APA
Santana, L. D., Catalano, F. M., Medeiros, M. A. F. de, & Carmo, M. (2010). The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Santana LD, Catalano FM, Medeiros MAF de, Carmo M. The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing. Proceedings. 2010 ;[citado 2025 dez. 10 ]
Vancouver
Santana LD, Catalano FM, Medeiros MAF de, Carmo M. The update process and characterization of the Sao Paulo University wind-tunnel for aeroacoustics testing. Proceedings. 2010 ;[citado 2025 dez. 10 ]
Trabalho de evento
Fuzzy sliding mode control of a flight simulator motion base (2010)
Becerra-Vargas, Mauricio; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ESTABILIDADE DE LIAPUNOV, SIMULADORES DE VOO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BECERRA-VARGAS, Mauricio e BELO, Eduardo Morgado. Fuzzy sliding mode control of a flight simulator motion base. 2010, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2010. . Acesso em: 10 dez. 2025.
APA
Becerra-Vargas, M., & Belo, E. M. (2010). Fuzzy sliding mode control of a flight simulator motion base. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Becerra-Vargas M, Belo EM. Fuzzy sliding mode control of a flight simulator motion base. Proceedings. 2010 ;[citado 2025 dez. 10 ]
Vancouver
Becerra-Vargas M, Belo EM. Fuzzy sliding mode control of a flight simulator motion base. Proceedings. 2010 ;[citado 2025 dez. 10 ]
Trabalho de evento
Acoustic control of laminar separation bubbles (2010)
Correa, Luiz Guilherme Noujain; Entz, Ricardo Maiko Uehoka; Cosin, Renato; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AEROFÓLIOS, TÚNEIS DE VENTO, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
CORREA, Luiz Guilherme Noujain et al. Acoustic control of laminar separation bubbles. 2010, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2010. . Acesso em: 10 dez. 2025.
APA
Correa, L. G. N., Entz, R. M. U., Cosin, R., & Catalano, F. M. (2010). Acoustic control of laminar separation bubbles. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Correa LGN, Entz RMU, Cosin R, Catalano FM. Acoustic control of laminar separation bubbles. Proceedings. 2010 ;[citado 2025 dez. 10 ]
Vancouver
Correa LGN, Entz RMU, Cosin R, Catalano FM. Acoustic control of laminar separation bubbles. Proceedings. 2010 ;[citado 2025 dez. 10 ]
Trabalho de evento
Active aeroelastic control of variable camber airfoil in the presence of strucutral non-linearities (2006)
Marques, Flavio Donizeti ; De Marqui Júnior, Carlos ; Caixeta Junior, Paulo Roberto
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, Flavio Donizeti e DE MARQUI JÚNIOR, Carlos e CAIXETA JUNIOR, Paulo Roberto. Active aeroelastic control of variable camber airfoil in the presence of strucutral non-linearities. 2006, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2006. Disponível em: https://repositorio.usp.br/directbitstream/d29943ac-0c1c-4e11-a0eb-96efb8c9c44e/PROD_25649_SYSNO_3123926.pdf. Acesso em: 10 dez. 2025.
APA
Marques, F. D., De Marqui Júnior, C., & Caixeta Junior, P. R. (2006). Active aeroelastic control of variable camber airfoil in the presence of strucutral non-linearities. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS. Recuperado de https://repositorio.usp.br/directbitstream/d29943ac-0c1c-4e11-a0eb-96efb8c9c44e/PROD_25649_SYSNO_3123926.pdf
NLM
Marques FD, De Marqui Júnior C, Caixeta Junior PR. Active aeroelastic control of variable camber airfoil in the presence of strucutral non-linearities [Internet]. Proceedings. 2006 ;[citado 2025 dez. 10 ] Available from: https://repositorio.usp.br/directbitstream/d29943ac-0c1c-4e11-a0eb-96efb8c9c44e/PROD_25649_SYSNO_3123926.pdf
Vancouver
Marques FD, De Marqui Júnior C, Caixeta Junior PR. Active aeroelastic control of variable camber airfoil in the presence of strucutral non-linearities [Internet]. Proceedings. 2006 ;[citado 2025 dez. 10 ] Available from: https://repositorio.usp.br/directbitstream/d29943ac-0c1c-4e11-a0eb-96efb8c9c44e/PROD_25649_SYSNO_3123926.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: 10 dez. 2025.
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 2025 dez. 10 ] 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 2025 dez. 10 ] 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: 10 dez. 2025.
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 2025 dez. 10 ] 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 2025 dez. 10 ] 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
Conceptual design and optimization of a high aspect ratio UAV wing made of composite material (2000)
Widmaier, K; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assunto: ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
WIDMAIER, K e CATALANO, Fernando Martini. Conceptual design and optimization of a high aspect ratio UAV wing made of composite material. 2000, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2000. . Acesso em: 10 dez. 2025.
APA
Widmaier, K., & Catalano, F. M. (2000). Conceptual design and optimization of a high aspect ratio UAV wing made of composite material. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Widmaier K, Catalano FM. Conceptual design and optimization of a high aspect ratio UAV wing made of composite material. Proceedings. 2000 ;[citado 2025 dez. 10 ]
Vancouver
Widmaier K, Catalano FM. Conceptual design and optimization of a high aspect ratio UAV wing made of composite material. Proceedings. 2000 ;[citado 2025 dez. 10 ]

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