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Trabalho de evento
Numerical analysis of the instabilities behind a blunt slat trailing-edge (2019)
Botero Bolívar, Laura; Acevedo Giraldo, Daniel; Pereira, Lourenço Tércio Lima; Catalano, Fernando Martini ; Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C
Fonte: Proceedings. Nome do evento: International Congress and Exhibition on Noise Control Engineering. Unidade: EESC
Assuntos: FUSELAGEM DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
BOTERO BOLÍVAR, Laura et al. Numerical analysis of the instabilities behind a blunt slat trailing-edge. 2019, Anais.. Madrid, Espanha: SEA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf. Acesso em: 29 nov. 2025.
APA
Botero Bolívar, L., Acevedo Giraldo, D., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2019). Numerical analysis of the instabilities behind a blunt slat trailing-edge. In Proceedings. Madrid, Espanha: SEA. Recuperado de https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf
NLM
Botero Bolívar L, Acevedo Giraldo D, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Numerical analysis of the instabilities behind a blunt slat trailing-edge [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf
Vancouver
Botero Bolívar L, Acevedo Giraldo D, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Numerical analysis of the instabilities behind a blunt slat trailing-edge [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/dcd29da1-7d14-4d78-a1ae-543b60c12178/trabalho%2003%20-%20Numerical%20analysis%20of%20the%20instabilities%20behind%20a%20blunt%20slat%20trailing-edge%20%28internoise%202019%29.pdf
Trabalho de evento
Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model (2019)
Acevedo Giraldo, Daniel; Botero Bolívar, Laura; Pereira, Lourenço Tércio Lima; Catalano, Fernando Martini ; Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C
Fonte: Proceedings. Nome do evento: International Congress and Exhibition on Noise Control Engineering. Unidade: EESC
Assuntos: FUSELAGEM DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
ACEVEDO GIRALDO, Daniel et al. Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model. 2019, Anais.. Madrid, Espanha: SEA, 2019. Disponível em: https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf. Acesso em: 29 nov. 2025.
APA
Acevedo Giraldo, D., Botero Bolívar, L., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2019). Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model. In Proceedings. Madrid, Espanha: SEA. Recuperado de https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf
NLM
Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf
Vancouver
Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical aeroacoustic analyses of a large-scale flap side-edge model [Internet]. Proceedings. 2019 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/3de08e9e-beab-4d74-a11f-1565256469b2/trabalho%2004%20-%20Experimental%20and%20Numerical%20Aeroacoustic%20Analyses%20of%20a%20Large-scale%20Flap%20Side-edge%20Model%20%28internoise%202019%29_removed.pdf
Trabalho de evento
Evaluation of wind tunnel wall boundarylayer control for 2-D high-lift aerodynamic and aeroacoustic testing (2018)
Catalano, Fernando Martini ; Pereira, Lourenço Tércio Lima
Fonte: Proceedings. Nome do evento: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
CATALANO, Fernando Martini e PEREIRA, Lourenço Tércio Lima. Evaluation of wind tunnel wall boundarylayer control for 2-D high-lift aerodynamic and aeroacoustic testing. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/8868ad20-52da-4512-a88d-a20413b31958/trabalho%2016%20-%20EVALUATION%20OF%20WIND%20TUNNEL%20WALL%20BOUNDARY-LAYER%20CONTROL%20FOR%202-D%20HIGH-LIFT%20AERODYNAMIC%20AND%20AEROACOUSTIC%20TESTING%20%28ICAS%202018%29.pdf. Acesso em: 29 nov. 2025.
APA
Catalano, F. M., & Pereira, L. T. L. (2018). Evaluation of wind tunnel wall boundarylayer control for 2-D high-lift aerodynamic and aeroacoustic testing. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/8868ad20-52da-4512-a88d-a20413b31958/trabalho%2016%20-%20EVALUATION%20OF%20WIND%20TUNNEL%20WALL%20BOUNDARY-LAYER%20CONTROL%20FOR%202-D%20HIGH-LIFT%20AERODYNAMIC%20AND%20AEROACOUSTIC%20TESTING%20%28ICAS%202018%29.pdf
NLM
Catalano FM, Pereira LTL. Evaluation of wind tunnel wall boundarylayer control for 2-D high-lift aerodynamic and aeroacoustic testing [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/8868ad20-52da-4512-a88d-a20413b31958/trabalho%2016%20-%20EVALUATION%20OF%20WIND%20TUNNEL%20WALL%20BOUNDARY-LAYER%20CONTROL%20FOR%202-D%20HIGH-LIFT%20AERODYNAMIC%20AND%20AEROACOUSTIC%20TESTING%20%28ICAS%202018%29.pdf
Vancouver
Catalano FM, Pereira LTL. Evaluation of wind tunnel wall boundarylayer control for 2-D high-lift aerodynamic and aeroacoustic testing [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/8868ad20-52da-4512-a88d-a20413b31958/trabalho%2016%20-%20EVALUATION%20OF%20WIND%20TUNNEL%20WALL%20BOUNDARY-LAYER%20CONTROL%20FOR%202-D%20HIGH-LIFT%20AERODYNAMIC%20AND%20AEROACOUSTIC%20TESTING%20%28ICAS%202018%29.pdf
Trabalho de evento
Experimental and computational analysis of a UAV for superficial volcano surveillance (2018)
Bravo Mosquera, Pedro David; Botero Bolívar, Laura; Acevedo Giraldo, Daniel; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: AERONAVES NÃO TRIPULADAS, 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. Experimental and computational analysis of a UAV for superficial volcano surveillance. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/84ca0c03-3933-4ac3-acb9-e79514b8bd96/trabalho%2015%20-%20EXPERIMENTAL%20AND%20COMPUTATIONAL%20ANALYSIS%20OF%20A%20UAV%20FOR%20SUPERFICIAL%20VOLCANO%20SURVEILLANCE%20%28ICAS%202018%29.pdf. Acesso em: 29 nov. 2025.
APA
Bravo Mosquera, P. D., Botero Bolívar, L., Acevedo Giraldo, D., Cerón Muñoz, H. D., & Catalano, F. M. (2018). Experimental and computational analysis of a UAV for superficial volcano surveillance. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/84ca0c03-3933-4ac3-acb9-e79514b8bd96/trabalho%2015%20-%20EXPERIMENTAL%20AND%20COMPUTATIONAL%20ANALYSIS%20OF%20A%20UAV%20FOR%20SUPERFICIAL%20VOLCANO%20SURVEILLANCE%20%28ICAS%202018%29.pdf
NLM
Bravo Mosquera PD, Botero Bolívar L, Acevedo Giraldo D, Cerón Muñoz HD, Catalano FM. Experimental and computational analysis of a UAV for superficial volcano surveillance [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/84ca0c03-3933-4ac3-acb9-e79514b8bd96/trabalho%2015%20-%20EXPERIMENTAL%20AND%20COMPUTATIONAL%20ANALYSIS%20OF%20A%20UAV%20FOR%20SUPERFICIAL%20VOLCANO%20SURVEILLANCE%20%28ICAS%202018%29.pdf
Vancouver
Bravo Mosquera PD, Botero Bolívar L, Acevedo Giraldo D, Cerón Muñoz HD, Catalano FM. Experimental and computational analysis of a UAV for superficial volcano surveillance [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/84ca0c03-3933-4ac3-acb9-e79514b8bd96/trabalho%2015%20-%20EXPERIMENTAL%20AND%20COMPUTATIONAL%20ANALYSIS%20OF%20A%20UAV%20FOR%20SUPERFICIAL%20VOLCANO%20SURVEILLANCE%20%28ICAS%202018%29.pdf
Trabalho de evento
Design and performance assessment of an inverted rectangular dorsal intake for military aviation (2018)
Bravo Mosquera, Pedro David; Abdalla, Alvaro Martins ; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: AERONAVES MILITARES, FUSELAGEM DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
BRAVO MOSQUERA, Pedro David et al. Design and performance assessment of an inverted rectangular dorsal intake for military aviation. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/f61f0f51-4199-4f6a-af2a-132b70c86bd1/trabalho%2003%20-%20DESIGN%20AND%20PERFORMANCE%20ASSESSMENT%20OF%20AN%20INVERTED%20RECTANGULAR%20DORSAL%20INTAKE%20FOR%20MILITARY%20AVIATION%20%28ICAS%202018%29.pdf. Acesso em: 29 nov. 2025.
APA
Bravo Mosquera, P. D., Abdalla, A. M., Cerón Muñoz, H. D., & Catalano, F. M. (2018). Design and performance assessment of an inverted rectangular dorsal intake for military aviation. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/f61f0f51-4199-4f6a-af2a-132b70c86bd1/trabalho%2003%20-%20DESIGN%20AND%20PERFORMANCE%20ASSESSMENT%20OF%20AN%20INVERTED%20RECTANGULAR%20DORSAL%20INTAKE%20FOR%20MILITARY%20AVIATION%20%28ICAS%202018%29.pdf
NLM
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Design and performance assessment of an inverted rectangular dorsal intake for military aviation [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/f61f0f51-4199-4f6a-af2a-132b70c86bd1/trabalho%2003%20-%20DESIGN%20AND%20PERFORMANCE%20ASSESSMENT%20OF%20AN%20INVERTED%20RECTANGULAR%20DORSAL%20INTAKE%20FOR%20MILITARY%20AVIATION%20%28ICAS%202018%29.pdf
Vancouver
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Design and performance assessment of an inverted rectangular dorsal intake for military aviation [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/f61f0f51-4199-4f6a-af2a-132b70c86bd1/trabalho%2003%20-%20DESIGN%20AND%20PERFORMANCE%20ASSESSMENT%20OF%20AN%20INVERTED%20RECTANGULAR%20DORSAL%20INTAKE%20FOR%20MILITARY%20AVIATION%20%28ICAS%202018%29.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: 29 nov. 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 nov. 29 ] 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 nov. 29 ] 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
Multi-disciplinary design optimization of a blended winglet (2018)
Souza, Joabe Marcos de; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
SOUZA, Joabe Marcos de e CATALANO, Fernando Martini. Multi-disciplinary design optimization of a blended winglet. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf. Acesso em: 29 nov. 2025.
APA
Souza, J. M. de, & Catalano, F. M. (2018). Multi-disciplinary design optimization of a blended winglet. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf
NLM
Souza JM de, Catalano FM. Multi-disciplinary design optimization of a blended winglet [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf
Vancouver
Souza JM de, Catalano FM. Multi-disciplinary design optimization of a blended winglet [Internet]. Proceedings. 2018 ;[citado 2025 nov. 29 ] Available from: https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.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: 29 nov. 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 nov. 29 ]
Vancouver
Tavernari VD, Catalano FM. Low reynolds propeller meta-model for multidiciplinary optimization. Proceedings. 2016 ;[citado 2025 nov. 29 ]
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
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: 29 nov. 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 nov. 29 ]
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 nov. 29 ]
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 29 nov. 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 nov. 29 ]
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 nov. 29 ]
Trabalho de evento
SquidCop: design and evaluation of a novel quadrotor MAV for in-flight launching air-to-ground missions (2014)
Sampaio, Rafael Coronel Bueno; Hernandes, André Carmona; Becker, Marcelo ; Catalano, Fernando Martini ; Zanini, Fábio; Nobrega, João Lucas Entringer Melo da; Martins, Caio
Fonte: Proceedings. Nome do evento: IEEE Aerospace Conference. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, DINÂMICA DOS FLUÍDOS COMPUTACIONAL, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SAMPAIO, Rafael Coronel Bueno et al. SquidCop: design and evaluation of a novel quadrotor MAV for in-flight launching air-to-ground missions. 2014, Anais.. Piscataway, NJ, USA: IEEE, 2014. Disponível em: https://doi.org/10.1109/AERO.2014.6836413. Acesso em: 29 nov. 2025.
APA
Sampaio, R. C. B., Hernandes, A. C., Becker, M., Catalano, F. M., Zanini, F., Nobrega, J. L. E. M. da, & Martins, C. (2014). SquidCop: design and evaluation of a novel quadrotor MAV for in-flight launching air-to-ground missions. In Proceedings. Piscataway, NJ, USA: IEEE. doi:10.1109/AERO.2014.6836413
NLM
Sampaio RCB, Hernandes AC, Becker M, Catalano FM, Zanini F, Nobrega JLEM da, Martins C. SquidCop: design and evaluation of a novel quadrotor MAV for in-flight launching air-to-ground missions [Internet]. Proceedings. 2014 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.1109/AERO.2014.6836413
Vancouver
Sampaio RCB, Hernandes AC, Becker M, Catalano FM, Zanini F, Nobrega JLEM da, Martins C. SquidCop: design and evaluation of a novel quadrotor MAV for in-flight launching air-to-ground missions [Internet]. Proceedings. 2014 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.1109/AERO.2014.6836413
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: 29 nov. 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 nov. 29 ]
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 nov. 29 ]
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: 29 nov. 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 nov. 29 ]
Vancouver
Moraleda FP, Catalano FM. Experimental analysis of the aerodynamics of porous flap side-edge. Proceedings. 2014 ;[citado 2025 nov. 29 ]
Trabalho de evento
Novel hybrid electric motor glider-quadrotor MAV for in-flight/V-STOL launching (2014)
Sampaio, Rafael Coronel Bueno; Hernandes, André Carmona; Becker, Marcelo ; Catalano, Fernando Martini ; Zanini, Fábio; Nobrega, João Lucas Entringer Melo da; Martins, Caio
Fonte: Proceedings. Nome do evento: IEEE Aerospace Conference. Unidade: EESC
Assuntos: AERONAVES QUADRIMOTORAS, MOTORES ELÉTRICOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SAMPAIO, Rafael Coronel Bueno et al. Novel hybrid electric motor glider-quadrotor MAV for in-flight/V-STOL launching. 2014, Anais.. Piscataway, NJ, USA: IEEE, 2014. Disponível em: https://doi.org/10.1109/AERO.2014.6836414. Acesso em: 29 nov. 2025.
APA
Sampaio, R. C. B., Hernandes, A. C., Becker, M., Catalano, F. M., Zanini, F., Nobrega, J. L. E. M. da, & Martins, C. (2014). Novel hybrid electric motor glider-quadrotor MAV for in-flight/V-STOL launching. In Proceedings. Piscataway, NJ, USA: IEEE. doi:10.1109/AERO.2014.6836414
NLM
Sampaio RCB, Hernandes AC, Becker M, Catalano FM, Zanini F, Nobrega JLEM da, Martins C. Novel hybrid electric motor glider-quadrotor MAV for in-flight/V-STOL launching [Internet]. Proceedings. 2014 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.1109/AERO.2014.6836414
Vancouver
Sampaio RCB, Hernandes AC, Becker M, Catalano FM, Zanini F, Nobrega JLEM da, Martins C. Novel hybrid electric motor glider-quadrotor MAV for in-flight/V-STOL launching [Internet]. Proceedings. 2014 ;[citado 2025 nov. 29 ] Available from: https://doi.org/10.1109/AERO.2014.6836414
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 29 nov. 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 nov. 29 ]
Vancouver
Cosin R, Catalano FM, Correa LGN, Entz RMU. Aerodynamic analysis of multi-winglets for low speed aircraft. Proceedings. 2012 ;[citado 2025 nov. 29 ]
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: 29 nov. 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 nov. 29 ]
Vancouver
Bortholin T, Catalano FM. Computational investigation of icing contamination on airfoil. Proceedings. 2012 ;[citado 2025 nov. 29 ]
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: 29 nov. 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 nov. 29 ]
Vancouver
Catalano FM, Cerón Muñoz HD, Greco Júnior PC. Trailing edge treatment to enhance high lift system performance. Proceedings. 2012 ;[citado 2025 nov. 29 ]
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: 29 nov. 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 nov. 29 ]
Vancouver
Catalano FM, Santana LD. Airfoil self noise reduction by application of different types of trailing edge serrations. Proceedings. 2012 ;[citado 2025 nov. 29 ]
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: 29 nov. 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 nov. 29 ]
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 nov. 29 ]
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: 29 nov. 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 nov. 29 ] 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 nov. 29 ] 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

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