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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: 08 jul. 2024.
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 2024 jul. 08 ] 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 2024 jul. 08 ] 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
Parametric investigation of EESC-USP aeroacoustic fan rig (2018)
Gigena Cuenca, Rafael; Greco Júnior, Paulo Celso ; Martínez Rocamora Junior, Bernardo
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AEROACÚSTICA, KRIGAGEM, ENGENHARIA AERONÁUTICA
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ABNT
GIGENA CUENCA, Rafael e GRECO JÚNIOR, Paulo Celso e MARTÍNEZ ROCAMORA JUNIOR, Bernardo. Parametric investigation of EESC-USP aeroacoustic fan rig. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33%7E1.PDF. Acesso em: 08 jul. 2024.
APA
Gigena Cuenca, R., Greco Júnior, P. C., & Martínez Rocamora Junior, B. (2018). Parametric investigation of EESC-USP aeroacoustic fan rig. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33%7E1.PDF
NLM
Gigena Cuenca R, Greco Júnior PC, Martínez Rocamora Junior B. Parametric investigation of EESC-USP aeroacoustic fan rig [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33%7E1.PDF
Vancouver
Gigena Cuenca R, Greco Júnior PC, Martínez Rocamora Junior B. Parametric investigation of EESC-USP aeroacoustic fan rig [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33%7E1.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
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: 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: 08 jul. 2024.
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 2024 jul. 08 ] 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 2024 jul. 08 ] 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
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERONAVES NÃO TRIPULADAS, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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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: 08 jul. 2024.
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 2024 jul. 08 ] 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 2024 jul. 08 ] 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
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: 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: 08 jul. 2024.
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 2024 jul. 08 ] 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 2024 jul. 08 ] 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
Influence of airframe stiffness on the aerodynamic coefficients of a high aspect ratio wing (2018)
Pelegrineli, Luis Antonio Vieira; Liorbano, Felipe Fernandes; Natori, Henrique Ossamu Hisano; Angélico, Ricardo Afonso
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: FUSELAGEM DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
PELEGRINELI, Luis Antonio Vieira et al. Influence of airframe stiffness on the aerodynamic coefficients of a high aspect ratio wing. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/f5e5051e-5b2d-417b-9a23-f0fc663dd1fc/trabalho%2001%20-%20Influence%20of%20airframe%20stiffness%20on%20the%20aerodynamic%20coefficients%20of%20a%20high%20aspect%20ratio%20wing%20%28ICAS%202018%29.pdf. Acesso em: 08 jul. 2024.
APA
Pelegrineli, L. A. V., Liorbano, F. F., Natori, H. O. H., & Angélico, R. A. (2018). Influence of airframe stiffness on the aerodynamic coefficients of a high aspect ratio wing. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/f5e5051e-5b2d-417b-9a23-f0fc663dd1fc/trabalho%2001%20-%20Influence%20of%20airframe%20stiffness%20on%20the%20aerodynamic%20coefficients%20of%20a%20high%20aspect%20ratio%20wing%20%28ICAS%202018%29.pdf
NLM
Pelegrineli LAV, Liorbano FF, Natori HOH, Angélico RA. Influence of airframe stiffness on the aerodynamic coefficients of a high aspect ratio wing [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://repositorio.usp.br/directbitstream/f5e5051e-5b2d-417b-9a23-f0fc663dd1fc/trabalho%2001%20-%20Influence%20of%20airframe%20stiffness%20on%20the%20aerodynamic%20coefficients%20of%20a%20high%20aspect%20ratio%20wing%20%28ICAS%202018%29.pdf
Vancouver
Pelegrineli LAV, Liorbano FF, Natori HOH, Angélico RA. Influence of airframe stiffness on the aerodynamic coefficients of a high aspect ratio wing [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://repositorio.usp.br/directbitstream/f5e5051e-5b2d-417b-9a23-f0fc663dd1fc/trabalho%2001%20-%20Influence%20of%20airframe%20stiffness%20on%20the%20aerodynamic%20coefficients%20of%20a%20high%20aspect%20ratio%20wing%20%28ICAS%202018%29.pdf
Trabalho de evento
Multi-disciplinary design optimization of a blended winglet (2018)
Souza, Joabe Marcos de; Catalano, Fernando Martini
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: 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: 08 jul. 2024.
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 2024 jul. 08 ] 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 2024 jul. 08 ] 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
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: 08 jul. 2024.
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 2024 jul. 08 ] 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 2024 jul. 08 ] 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
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
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 08 jul. 2024.
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 2024 jul. 08 ] 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 2024 jul. 08 ] 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
Design of an instrumented stator vane for unsteady pressure measurements using mems microphones (2018)
Martínez Rocamora Junior, Bernardo; Caldas, Luciano Coutinho; Gigena Cuenca, Rafael; Queiroz, Rudner Lauterjung; Greco Júnior, Paulo Celso
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AEROACÚSTICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARTÍNEZ ROCAMORA JUNIOR, Bernardo et al. Design of an instrumented stator vane for unsteady pressure measurements using mems microphones. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/7e51e7b5-9bd8-4125-9976-d891205e1faf/trabalho%2001%20-%20DESIGN%20OF%20AN%20INSTRUMENTED%20STATOR%20VANE%20FOR%20UNSTEADY%20PRESSURE%20MEASUREMENTS%20USING%20MEMS%20MICROPHONES%20%28ICAS%202018%29.pdf. Acesso em: 08 jul. 2024.
APA
Martínez Rocamora Junior, B., Caldas, L. C., Gigena Cuenca, R., Queiroz, R. L., & Greco Júnior, P. C. (2018). Design of an instrumented stator vane for unsteady pressure measurements using mems microphones. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/7e51e7b5-9bd8-4125-9976-d891205e1faf/trabalho%2001%20-%20DESIGN%20OF%20AN%20INSTRUMENTED%20STATOR%20VANE%20FOR%20UNSTEADY%20PRESSURE%20MEASUREMENTS%20USING%20MEMS%20MICROPHONES%20%28ICAS%202018%29.pdf
NLM
Martínez Rocamora Junior B, Caldas LC, Gigena Cuenca R, Queiroz RL, Greco Júnior PC. Design of an instrumented stator vane for unsteady pressure measurements using mems microphones [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://repositorio.usp.br/directbitstream/7e51e7b5-9bd8-4125-9976-d891205e1faf/trabalho%2001%20-%20DESIGN%20OF%20AN%20INSTRUMENTED%20STATOR%20VANE%20FOR%20UNSTEADY%20PRESSURE%20MEASUREMENTS%20USING%20MEMS%20MICROPHONES%20%28ICAS%202018%29.pdf
Vancouver
Martínez Rocamora Junior B, Caldas LC, Gigena Cuenca R, Queiroz RL, Greco Júnior PC. Design of an instrumented stator vane for unsteady pressure measurements using mems microphones [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://repositorio.usp.br/directbitstream/7e51e7b5-9bd8-4125-9976-d891205e1faf/trabalho%2001%20-%20DESIGN%20OF%20AN%20INSTRUMENTED%20STATOR%20VANE%20FOR%20UNSTEADY%20PRESSURE%20MEASUREMENTS%20USING%20MEMS%20MICROPHONES%20%28ICAS%202018%29.pdf
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: 08 jul. 2024.
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 2024 jul. 08 ] 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 2024 jul. 08 ] 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 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: 08 jul. 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 jul. 08 ] 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 jul. 08 ] 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: 08 jul. 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 jul. 08 ] 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 jul. 08 ] 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: 08 jul. 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 jul. 08 ] 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 jul. 08 ] 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
Trabalho de evento
On the effects of a installed propeller slipstream on a wing boundary layer (2000)
Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: HÉLICES DE AERONAVES, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CATALANO, Fernando Martini. On the effects of a installed propeller slipstream on a wing boundary layer. 2000, Anais.. Edinburgh, UK: ICAS, 2000. Disponível em: https://repositorio.usp.br/directbitstream/1b10d0cd-d281-4466-ae2e-a3489451ccde/trabalho%2067%20-%20ON%20THE%20EFFECTS%20OF%20A%20INSTALLED%20PROPELLER%20SLIPSTREAM%20ON%20A%20WING%20BOUNDARY%20LAYER%20%28ICAS%202000%29.PDF. Acesso em: 08 jul. 2024.
APA
Catalano, F. M. (2000). On the effects of a installed propeller slipstream on a wing boundary layer. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/1b10d0cd-d281-4466-ae2e-a3489451ccde/trabalho%2067%20-%20ON%20THE%20EFFECTS%20OF%20A%20INSTALLED%20PROPELLER%20SLIPSTREAM%20ON%20A%20WING%20BOUNDARY%20LAYER%20%28ICAS%202000%29.PDF
NLM
Catalano FM. On the effects of a installed propeller slipstream on a wing boundary layer [Internet]. Proceedings. 2000 ;[citado 2024 jul. 08 ] Available from: https://repositorio.usp.br/directbitstream/1b10d0cd-d281-4466-ae2e-a3489451ccde/trabalho%2067%20-%20ON%20THE%20EFFECTS%20OF%20A%20INSTALLED%20PROPELLER%20SLIPSTREAM%20ON%20A%20WING%20BOUNDARY%20LAYER%20%28ICAS%202000%29.PDF
Vancouver
Catalano FM. On the effects of a installed propeller slipstream on a wing boundary layer [Internet]. Proceedings. 2000 ;[citado 2024 jul. 08 ] Available from: https://repositorio.usp.br/directbitstream/1b10d0cd-d281-4466-ae2e-a3489451ccde/trabalho%2067%20-%20ON%20THE%20EFFECTS%20OF%20A%20INSTALLED%20PROPELLER%20SLIPSTREAM%20ON%20A%20WING%20BOUNDARY%20LAYER%20%28ICAS%202000%29.PDF

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