ReP USP - Resultado da busca

Trabalho de evento
Mitigating dynamic stall with a movable leading-edge: the NACA0012-IK30 wing (2024)
Camacho, Emanuel A. R.; Silva, Andre R. R; Marques, Flavio Donizeti
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ROTOR, ASAS DE AERONAVES, PROPULSÃO, AERODINÂMICA DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
CAMACHO, Emanuel A. R. e SILVA, Andre R. R e MARQUES, Flavio Donizeti. Mitigating dynamic stall with a movable leading-edge: the NACA0012-IK30 wing. 2024, Anais.. Edinburgh, UK: Escola de Engenharia de São Carlos, Universidade de São Paulo, 2024. Disponível em: https://repositorio.usp.br/directbitstream/8eedf42a-b8a2-445f-9ead-f598734f1a02/icas2024_0595_paper.pdf. Acesso em: 04 maio 2026.
APA
Camacho, E. A. R., Silva, A. R. R., & Marques, F. D. (2024). Mitigating dynamic stall with a movable leading-edge: the NACA0012-IK30 wing. In Proceedings. Edinburgh, UK: Escola de Engenharia de São Carlos, Universidade de São Paulo. Recuperado de https://repositorio.usp.br/directbitstream/8eedf42a-b8a2-445f-9ead-f598734f1a02/icas2024_0595_paper.pdf
NLM
Camacho EAR, Silva ARR, Marques FD. Mitigating dynamic stall with a movable leading-edge: the NACA0012-IK30 wing [Internet]. Proceedings. 2024 ;[citado 2026 maio 04 ] Available from: https://repositorio.usp.br/directbitstream/8eedf42a-b8a2-445f-9ead-f598734f1a02/icas2024_0595_paper.pdf
Vancouver
Camacho EAR, Silva ARR, Marques FD. Mitigating dynamic stall with a movable leading-edge: the NACA0012-IK30 wing [Internet]. Proceedings. 2024 ;[citado 2026 maio 04 ] Available from: https://repositorio.usp.br/directbitstream/8eedf42a-b8a2-445f-9ead-f598734f1a02/icas2024_0595_paper.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: 04 maio 2026.
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 2026 maio 04 ] 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 2026 maio 04 ] 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
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: 04 maio 2026.
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 2026 maio 04 ] 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 2026 maio 04 ] 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 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: 04 maio 2026.
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 2026 maio 04 ] 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 2026 maio 04 ] 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: 04 maio 2026.
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 2026 maio 04 ] 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 2026 maio 04 ] 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 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
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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: 04 maio 2026.
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 2026 maio 04 ] 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 2026 maio 04 ] 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
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/AP8F33~1.PDF. Acesso em: 04 maio 2026.
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/AP8F33~1.PDF
NLM
Gigena Cuenca R, Greco Júnior PC, Martínez Rocamora Junior B. Parametric investigation of EESC-USP aeroacoustic fan rig [Internet]. Proceedings. 2018 ;[citado 2026 maio 04 ] Available from: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.PDF
Vancouver
Gigena Cuenca R, Greco Júnior PC, Martínez Rocamora Junior B. Parametric investigation of EESC-USP aeroacoustic fan rig [Internet]. Proceedings. 2018 ;[citado 2026 maio 04 ] Available from: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.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: 04 maio 2026.
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 2026 maio 04 ] 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 2026 maio 04 ] 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
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 04 maio 2026.
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 2026 maio 04 ] 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 2026 maio 04 ] 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
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: 04 maio 2026.
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 2026 maio 04 ] 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 2026 maio 04 ] 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
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 04 maio 2026.
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 2026 maio 04 ] 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 2026 maio 04 ] 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
Relevant properties and relationships for construction defect data mining on building information models (2017)
Martin Delatorre, Joyce Paula ; Santos, Eduardo Toledo
Source: Proceedings. Conference titles: Joint Conference on Computing in Construction - JC3. Unidade: EP
Subjects: GERENCIAMENTO DA CONSTRUÇÃO, MINERAÇÃO DE DADOS, CONSTRUÇÃO CIVIL, CONTROLE DA QUALIDADE
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARTIN DELATORRE, Joyce Paula e SANTOS, Eduardo Toledo. Relevant properties and relationships for construction defect data mining on building information models. 2017, Anais.. Edinburgh, UK: Heriot-Watt University, 2017. Disponível em: https://itc.scix.net/pdfs/LC3_2017_paper_227.pdf. Acesso em: 04 maio 2026.
APA
Martin Delatorre, J. P., & Santos, E. T. (2017). Relevant properties and relationships for construction defect data mining on building information models. In Proceedings. Edinburgh, UK: Heriot-Watt University. Recuperado de https://itc.scix.net/pdfs/LC3_2017_paper_227.pdf
NLM
Martin Delatorre JP, Santos ET. Relevant properties and relationships for construction defect data mining on building information models [Internet]. Proceedings. 2017 ;[citado 2026 maio 04 ] Available from: https://itc.scix.net/pdfs/LC3_2017_paper_227.pdf
Vancouver
Martin Delatorre JP, Santos ET. Relevant properties and relationships for construction defect data mining on building information models [Internet]. Proceedings. 2017 ;[citado 2026 maio 04 ] Available from: https://itc.scix.net/pdfs/LC3_2017_paper_227.pdf
Trabalho de evento
Conceptual and aerodynamic design of a UAV for superficial volcano monitoring (2016)
Bravo Mosquera, Pedro David; Abdalla, Alvaro Martins ; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERONAVES NÃO TRIPULADAS, DINÂMICA DOS FLUÍDOS COMPUTACIONAL, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David et al. Conceptual and aerodynamic design of a UAV for superficial volcano monitoring. 2016, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2016. . Acesso em: 04 maio 2026.
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 2026 maio 04 ]
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 2026 maio 04 ]
Trabalho de evento
Low reynolds propeller meta-model for multidiciplinary optimization (2016)
Tavernari, V. D.; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: HÉLICES DE AERONAVES, AEROFÓLIOS, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 04 maio 2026.
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 2026 maio 04 ]
Vancouver
Tavernari VD, Catalano FM. Low reynolds propeller meta-model for multidiciplinary optimization. Proceedings. 2016 ;[citado 2026 maio 04 ]
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
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: 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: 04 maio 2026.
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 2026 maio 04 ]
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 2026 maio 04 ]
Trabalho de evento
Knowledge-based future combat aircraft optimization (2016)
Munjulury, Raghu Chaitanya; Abdalla, Alvaro Martins ; Staack, Ingo; Krus, Petter
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERONAVES MILITARES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MUNJULURY, Raghu Chaitanya et al. Knowledge-based future combat aircraft optimization. 2016, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2016. . Acesso em: 04 maio 2026.
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 2026 maio 04 ]
Vancouver
Munjulury RC, Abdalla AM, Staack I, Krus P. Knowledge-based future combat aircraft optimization. Proceedings. 2016 ;[citado 2026 maio 04 ]
Trabalho de evento
An application of digital imaging processing for UAV's automatic landing system AID (2014)
Degrande, Mateus Pereira; Moreira, Emilio Eduardo Tressoldi; Belo, Eduardo Morgado
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: PROCESSAMENTO DIGITAL DE IMAGENS, AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
DEGRANDE, Mateus Pereira e MOREIRA, Emilio Eduardo Tressoldi e BELO, Eduardo Morgado. An application of digital imaging processing for UAV's automatic landing system AID. 2014, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2014. . Acesso em: 04 maio 2026.
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 2026 maio 04 ]
Vancouver
Degrande MP, Moreira EET, Belo EM. An application of digital imaging processing for UAV's automatic landing system AID. Proceedings. 2014 ;[citado 2026 maio 04 ]
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
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: 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: 04 maio 2026.
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 2026 maio 04 ]
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 2026 maio 04 ]
Trabalho de evento
Experimental analysis of the aerodynamics of porous flap side-edge (2014)
Moraleda, F. P.; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: 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: 04 maio 2026.
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 2026 maio 04 ]
Vancouver
Moraleda FP, Catalano FM. Experimental analysis of the aerodynamics of porous flap side-edge. Proceedings. 2014 ;[citado 2026 maio 04 ]
Trabalho de evento
Trailing edge treatment to enhance high lift system performance (2012)
Catalano, Fernando Martini ; Cerón Muñoz, Hernán Darío ; Greco Júnior, Paulo Celso
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: 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: 04 maio 2026.
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 2026 maio 04 ]
Vancouver
Catalano FM, Cerón Muñoz HD, Greco Júnior PC. Trailing edge treatment to enhance high lift system performance. Proceedings. 2012 ;[citado 2026 maio 04 ]

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