ReP USP - Resultado da busca

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: 09 nov. 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 nov. 09 ] 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 nov. 09 ] Available from: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33%7E1.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: 09 nov. 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 nov. 09 ] 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 nov. 09 ] 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
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 09 nov. 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 nov. 09 ] 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 nov. 09 ] 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
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: 09 nov. 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 nov. 09 ] 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 nov. 09 ] 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
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: 09 nov. 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 nov. 09 ] 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 nov. 09 ] 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
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: 09 nov. 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 nov. 09 ] 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 nov. 09 ] 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
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: 09 nov. 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 nov. 09 ] 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 nov. 09 ] 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

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