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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
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 05 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. 05 ] 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. 05 ] 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
Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft (2018)
Bravo Mosquera, Pedro David; Abdalla, Alvaro Martins ; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES
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ABNT
BRAVO MOSQUERA, Pedro David e ABDALLA, Alvaro Martins e CATALANO, Fernando Martini. Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf. Acesso em: 05 dez. 2025.
APA
Bravo Mosquera, P. D., Abdalla, A. M., & Catalano, F. M. (2018). Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf
NLM
Bravo Mosquera PD, Abdalla AM, Catalano FM. Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft [Internet]. Proceedings. 2018 ;[citado 2025 dez. 05 ] Available from: https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf
Vancouver
Bravo Mosquera PD, Abdalla AM, Catalano FM. Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft [Internet]. Proceedings. 2018 ;[citado 2025 dez. 05 ] Available from: https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.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
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 05 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. 05 ] 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. 05 ] 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
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 05 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. 05 ]
Vancouver
Tavernari VD, Catalano FM. Low reynolds propeller meta-model for multidiciplinary optimization. Proceedings. 2016 ;[citado 2025 dez. 05 ]
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
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: AERONAVES NÃO TRIPULADAS, DINÂMICA DOS FLUÍDOS COMPUTACIONAL, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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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: 05 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. 05 ]
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. 05 ]
Trabalho de evento
Experimental analyses of droop, wingtips and fences on a BWB model (2016)
Cerón Muñoz, Hernán Darío ; Diaz Izquierdo, David Orlando; Bravo Mosquera, Pedro David; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
CERÓN MUÑOZ, Hernán Darío et al. Experimental analyses of droop, wingtips and fences on a BWB model. 2016, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2016. . Acesso em: 05 dez. 2025.
APA
Cerón Muñoz, H. D., Diaz Izquierdo, D. O., Bravo Mosquera, P. D., & Catalano, F. M. (2016). Experimental analyses of droop, wingtips and fences on a BWB model. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cerón Muñoz HD, Diaz Izquierdo DO, Bravo Mosquera PD, Catalano FM. Experimental analyses of droop, wingtips and fences on a BWB model. Proceedings. 2016 ;[citado 2025 dez. 05 ]
Vancouver
Cerón Muñoz HD, Diaz Izquierdo DO, Bravo Mosquera PD, Catalano FM. Experimental analyses of droop, wingtips and fences on a BWB model. Proceedings. 2016 ;[citado 2025 dez. 05 ]
Trabalho de evento
Knowledge-based future combat aircraft optimization (2016)
Munjulury, Raghu Chaitanya; Abdalla, Alvaro Martins ; Staack, Ingo; Krus, Petter
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: AERONAVES MILITARES, ENGENHARIA AERONÁUTICA
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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: 05 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. 05 ]
Vancouver
Munjulury RC, Abdalla AM, Staack I, Krus P. Knowledge-based future combat aircraft optimization. Proceedings. 2016 ;[citado 2025 dez. 05 ]
Trabalho de evento
Aerodynamic interference of wingtip and wing devices on BWB model (2014)
Cerón Muñoz, Hernán Darío ; Diaz Izquierdo, David Orlando; Solarte Pineda, Jhonathan; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CERÓN MUÑOZ, Hernán Darío et al. Aerodynamic interference of wingtip and wing devices on BWB model. 2014, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2014. . Acesso em: 05 dez. 2025.
APA
Cerón Muñoz, H. D., Diaz Izquierdo, D. O., Solarte Pineda, J., & Catalano, F. M. (2014). Aerodynamic interference of wingtip and wing devices on BWB model. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cerón Muñoz HD, Diaz Izquierdo DO, Solarte Pineda J, Catalano FM. Aerodynamic interference of wingtip and wing devices on BWB model. Proceedings. 2014 ;[citado 2025 dez. 05 ]
Vancouver
Cerón Muñoz HD, Diaz Izquierdo DO, Solarte Pineda J, Catalano FM. Aerodynamic interference of wingtip and wing devices on BWB model. Proceedings. 2014 ;[citado 2025 dez. 05 ]
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
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: PROCESSAMENTO DIGITAL DE IMAGENS, AERONAVES, ENGENHARIA AERONÁUTICA
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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: 05 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. 05 ]
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. 05 ]
Trabalho de evento
Experimental analysis of the aerodynamics of porous flap side-edge (2014)
Moraleda, F. P.; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MORALEDA, F. P. e CATALANO, Fernando Martini. Experimental analysis of the aerodynamics of porous flap side-edge. 2014, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2014. . Acesso em: 05 dez. 2025.
APA
Moraleda, F. P., & Catalano, F. M. (2014). Experimental analysis of the aerodynamics of porous flap side-edge. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Moraleda FP, Catalano FM. Experimental analysis of the aerodynamics of porous flap side-edge. Proceedings. 2014 ;[citado 2025 dez. 05 ]
Vancouver
Moraleda FP, Catalano FM. Experimental analysis of the aerodynamics of porous flap side-edge. Proceedings. 2014 ;[citado 2025 dez. 05 ]
Trabalho de evento
Aerodynamic analysis of multi-winglets for low speed aircraft (2012)
Cosin, Renato; Catalano, Fernando Martini ; Correa, Luiz Guilherme Noujain; Entz, Ricardo Maiko Uehoka
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
COSIN, Renato et al. Aerodynamic analysis of multi-winglets for low speed aircraft. 2012, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2012. . Acesso em: 05 dez. 2025.
APA
Cosin, R., Catalano, F. M., Correa, L. G. N., & Entz, R. M. U. (2012). Aerodynamic analysis of multi-winglets for low speed aircraft. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cosin R, Catalano FM, Correa LGN, Entz RMU. Aerodynamic analysis of multi-winglets for low speed aircraft. Proceedings. 2012 ;[citado 2025 dez. 05 ]
Vancouver
Cosin R, Catalano FM, Correa LGN, Entz RMU. Aerodynamic analysis of multi-winglets for low speed aircraft. Proceedings. 2012 ;[citado 2025 dez. 05 ]
Trabalho de evento
Computational investigation of icing contamination on airfoil (2012)
Bortholin, Thaís; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 05 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. 05 ]
Vancouver
Bortholin T, Catalano FM. Computational investigation of icing contamination on airfoil. Proceedings. 2012 ;[citado 2025 dez. 05 ]
Trabalho de evento
Trailing edge treatment to enhance high lift system performance (2012)
Catalano, Fernando Martini ; Cerón Muñoz, Hernán Darío ; Greco Júnior, Paulo Celso
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: ASAS DE AERONAVES, AEROFÓLIOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CATALANO, Fernando Martini e CERÓN MUÑOZ, Hernán Darío e GRECO JÚNIOR, Paulo Celso. Trailing edge treatment to enhance high lift system performance. 2012, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2012. . Acesso em: 05 dez. 2025.
APA
Catalano, F. M., Cerón Muñoz, H. D., & Greco Júnior, P. C. (2012). Trailing edge treatment to enhance high lift system performance. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Catalano FM, Cerón Muñoz HD, Greco Júnior PC. Trailing edge treatment to enhance high lift system performance. Proceedings. 2012 ;[citado 2025 dez. 05 ]
Vancouver
Catalano FM, Cerón Muñoz HD, Greco Júnior PC. Trailing edge treatment to enhance high lift system performance. Proceedings. 2012 ;[citado 2025 dez. 05 ]
Trabalho de evento
Airfoil self noise reduction by application of different types of trailing edge serrations (2012)
Catalano, Fernando Martini ; Santana, Leandro Dantas
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 05 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. 05 ]
Vancouver
Catalano FM, Santana LD. Airfoil self noise reduction by application of different types of trailing edge serrations. Proceedings. 2012 ;[citado 2025 dez. 05 ]
Trabalho de evento
Wind tunnel testing of porous devices for the reduction of flap side-edge noise (2012)
Catalano, Fernando Martini ; Vanuchi, Paulo; Correa, Luiz Guilherme Noujain
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: TÚNEIS DE VENTO, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CATALANO, Fernando Martini e VANUCHI, Paulo e CORREA, Luiz Guilherme Noujain. Wind tunnel testing of porous devices for the reduction of flap side-edge noise. 2012, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2012. . Acesso em: 05 dez. 2025.
APA
Catalano, F. M., Vanuchi, P., & Correa, L. G. N. (2012). Wind tunnel testing of porous devices for the reduction of flap side-edge noise. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Catalano FM, Vanuchi P, Correa LGN. Wind tunnel testing of porous devices for the reduction of flap side-edge noise. Proceedings. 2012 ;[citado 2025 dez. 05 ]
Vancouver
Catalano FM, Vanuchi P, Correa LGN. Wind tunnel testing of porous devices for the reduction of flap side-edge noise. Proceedings. 2012 ;[citado 2025 dez. 05 ]
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
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 05 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. 05 ] 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. 05 ] 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
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 05 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. 05 ]
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. 05 ]
Trabalho de evento
Fuzzy sliding mode control of a flight simulator motion base (2010)
Becerra-Vargas, Mauricio; Belo, Eduardo Morgado
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 05 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. 05 ]
Vancouver
Becerra-Vargas M, Belo EM. Fuzzy sliding mode control of a flight simulator motion base. Proceedings. 2010 ;[citado 2025 dez. 05 ]
Trabalho de evento
Aerodynamic interference of power-plant system on a blended wing body (2010)
Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Aerodynamic interference of power-plant system on a blended wing body. 2010, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2010. . Acesso em: 05 dez. 2025.
APA
Cerón Muñoz, H. D., & Catalano, F. M. (2010). Aerodynamic interference of power-plant system on a blended wing body. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cerón Muñoz HD, Catalano FM. Aerodynamic interference of power-plant system on a blended wing body. Proceedings. 2010 ;[citado 2025 dez. 05 ]
Vancouver
Cerón Muñoz HD, Catalano FM. Aerodynamic interference of power-plant system on a blended wing body. Proceedings. 2010 ;[citado 2025 dez. 05 ]
Trabalho de evento
Acoustic control of laminar separation bubbles (2010)
Correa, Luiz Guilherme Noujain; Entz, Ricardo Maiko Uehoka; Cosin, Renato; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: AEROFÓLIOS, TÚNEIS DE VENTO, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 05 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. 05 ]
Vancouver
Correa LGN, Entz RMU, Cosin R, Catalano FM. Acoustic control of laminar separation bubbles. Proceedings. 2010 ;[citado 2025 dez. 05 ]

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