ReP USP - Resultado da busca

Trabalho de evento
Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake (2019)
Boccato, Bruno Ribeiro; Bravo Mosquera, Pedro David; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: AIAA Propulsion and Energy Forum. Unidade: EESC
Assuntos: ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES
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ABNT
BOCCATO, Bruno Ribeiro e BRAVO MOSQUERA, Pedro David e CATALANO, Fernando Martini. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-4200. Acesso em: 08 jul. 2024.
APA
Boccato, B. R., Bravo Mosquera, P. D., & Catalano, F. M. (2019). Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-4200
NLM
Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2019-4200
Vancouver
Boccato BR, Bravo Mosquera PD, Catalano FM. Experimental assessment of a non-conventional fighter aircraft: effects of canard on the performance of a dorsal intake [Internet]. Proceedings. 2019 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2019-4200
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: 08 jul. 2024.
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 2024 jul. 08 ] 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 2024 jul. 08 ] 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
A study on the 3D effects of slat cove fillers (2019)
Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C.; Pereira, Lourenço Tércio Lima; Catalano, Fernando Martini ; Lima, Leandro S. de M.
Fonte: Proceedings. Nome do evento: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Assuntos: ENGENHARIA AERONÁUTICA, AEROACÚSTICA, TERCEIRA DIMENSÃO
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ABNT
REIS, Danillo Cafaldo dos et al. A study on the 3D effects of slat cove fillers. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-2406. Acesso em: 08 jul. 2024.
APA
Reis, D. C. dos, Coelho, E. L. C., Pereira, L. T. L., Catalano, F. M., & Lima, L. S. de M. (2019). A study on the 3D effects of slat cove fillers. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-2406
NLM
Reis DC dos, Coelho ELC, Pereira LTL, Catalano FM, Lima LS de M. A study on the 3D effects of slat cove fillers [Internet]. Proceedings. 2019 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2019-2406
Vancouver
Reis DC dos, Coelho ELC, Pereira LTL, Catalano FM, Lima LS de M. A study on the 3D effects of slat cove fillers [Internet]. Proceedings. 2019 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2019-2406
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: 08 jul. 2024.
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 2024 jul. 08 ] 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 2024 jul. 08 ] 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
Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system (2019)
Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: AIAA Propulsion and Energy Forum. Unidade: EESC
Assuntos: ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES
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ABNT
BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-3850. Acesso em: 08 jul. 2024.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-3850
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2019-3850
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system [Internet]. Proceedings. 2019 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2019-3850
Trabalho de evento
Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model (2018)
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: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Assuntos: FLAPS, AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
ACEVEDO GIRALDO, Daniel et al. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3799. Acesso em: 08 jul. 2024.
APA
Acevedo Giraldo, D., Botero Bolívar, L., Pereira, L. T. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3799
NLM
Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-3799
Vancouver
Acevedo Giraldo D, Botero Bolívar L, Pereira LTL, Catalano FM, Reis DC dos, Coelho ELC. Experimental aeroacoustic and aerodynamic analysis of a large-scale flap side-edge model [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-3799
Trabalho de evento
Parametric analysis of the influence of slat geometry on acoustic noise (2018)
Botero Bolívar, Laura; Pereira, Lourenço Tércio Lima; Acevedo Giraldo, Daniel; Catalano, Fernando Martini ; Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C
Fonte: Proceedings. Nome do evento: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Assuntos: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA
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ABNT
BOTERO BOLÍVAR, Laura et al. Parametric analysis of the influence of slat geometry on acoustic noise. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3593. Acesso em: 08 jul. 2024.
APA
Botero Bolívar, L., Pereira, L. T. L., Acevedo Giraldo, D., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Parametric analysis of the influence of slat geometry on acoustic noise. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3593
NLM
Botero Bolívar L, Pereira LTL, Acevedo Giraldo D, Catalano FM, Reis DC dos, Coelho ELC. Parametric analysis of the influence of slat geometry on acoustic noise [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-3593
Vancouver
Botero Bolívar L, Pereira LTL, Acevedo Giraldo D, Catalano FM, Reis DC dos, Coelho ELC. Parametric analysis of the influence of slat geometry on acoustic noise [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-3593
Trabalho de evento
Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear (2018)
Rego, Leandro Falcão Loureiro; Pereira, Lourenço Tércio Lima; Catalano, Fernando Martini ; Speth, R.; Bent, P.; Fregnani, J. A.
Fonte: Proceedings. Nome do evento: AAIA Aerospace Sciences Meeting. Unidade: EESC
Assuntos: TRENS DE POUSO, ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES, AEROACÚSTICA
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ABNT
REGO, Leandro Falcão Loureiro et al. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0759. Acesso em: 08 jul. 2024.
APA
Rego, L. F. L., Pereira, L. T. L., Catalano, F. M., Speth, R., Bent, P., & Fregnani, J. A. (2018). Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-0759
NLM
Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-0759
Vancouver
Rego LFL, Pereira LTL, Catalano FM, Speth R, Bent P, Fregnani JA. Aerodynamic and aeroacoustic experimental investigation of a simplified nose landing gear [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-0759
Trabalho de evento
Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model (2018)
Pereira, Lourenço Tércio Lima; Botero Bolívar, Laura; Araujo, Matheus Tozo de ; Catalano, Fernando Martini ; Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C
Fonte: Proceedings. Nome do evento: AIAA/CEAS Aeroacoustics Conference. Unidades: EESC, ICMC
Assuntos: AERODINÂMICA DE AERONAVES, ASAS DE AERONAVES, ANÁLISE NUMÉRICA, ENGENHARIA AERONÁUTICA
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ABNT
PEREIRA, Lourenço Tércio Lima et al. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3458. Acesso em: 08 jul. 2024.
APA
Pereira, L. T. L., Botero Bolívar, L., Araujo, M. T. de, Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3458
NLM
Pereira LTL, Botero Bolívar L, Araujo MT de, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-3458
Vancouver
Pereira LTL, Botero Bolívar L, Araujo MT de, Catalano FM, Reis DC dos, Coelho ELC. Experimental and numerical analysis of the aerodynamic and aeroacoustic properties of a 2D high-lift wing model [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-3458
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: 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
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
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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
Experimental slat noise assessment through phased array and hot-film anemometry measurements (2018)
Pereira, Lourenço Tércio Lima; Rego, Leandro Falcão Loureiro; Catalano, Fernando Martini ; Reis, Danillo Cafaldo dos; Coelho, Eduardo L. C
Fonte: Proceedings. Nome do evento: AAIA Aerospace Sciences Meeting. Unidade: EESC
Assuntos: SLATS, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
PEREIRA, Lourenço Tércio Lima et al. Experimental slat noise assessment through phased array and hot-film anemometry measurements. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-0758. Acesso em: 08 jul. 2024.
APA
Pereira, L. T. L., Rego, L. F. L., Catalano, F. M., Reis, D. C. dos, & Coelho, E. L. C. (2018). Experimental slat noise assessment through phased array and hot-film anemometry measurements. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-0758
NLM
Pereira LTL, Rego LFL, Catalano FM, Reis DC dos, Coelho ELC. Experimental slat noise assessment through phased array and hot-film anemometry measurements [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-0758
Vancouver
Pereira LTL, Rego LFL, Catalano FM, Reis DC dos, Coelho ELC. Experimental slat noise assessment through phased array and hot-film anemometry measurements [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-0758
Trabalho de evento
Noise reductions on a pusher propeller configuration through pylon tangential blowing (2018)
Rego, Leandro Falcão Loureiro; Pereira, Lourenço Tércio Lima; Catalano, Fernando Martini
Fonte: Proceedings. Nome do evento: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Assuntos: HÉLICES DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
REGO, Leandro Falcão Loureiro e PEREIRA, Lourenço Tércio Lima e CATALANO, Fernando Martini. Noise reductions on a pusher propeller configuration through pylon tangential blowing. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-4194. Acesso em: 08 jul. 2024.
APA
Rego, L. F. L., Pereira, L. T. L., & Catalano, F. M. (2018). Noise reductions on a pusher propeller configuration through pylon tangential blowing. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-4194
NLM
Rego LFL, Pereira LTL, Catalano FM. Noise reductions on a pusher propeller configuration through pylon tangential blowing [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-4194
Vancouver
Rego LFL, Pereira LTL, Catalano FM. Noise reductions on a pusher propeller configuration through pylon tangential blowing [Internet]. Proceedings. 2018 ;[citado 2024 jul. 08 ] Available from: https://doi.org/10.2514/6.2018-4194
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
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: 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
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
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: 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
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
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
Aeordynamic databased of a subscale demonstrator (2017)
Jouannet, C.; Lundström, D.; Krus, P.; Sobron, A.; Silva, Roberto Gil Annes da; Catalano, Fernando Martini ; Greco Júnior, Paulo Celso
Fonte: Proceedings. Nome do evento: AAIA Applied Aerodynamics Conference. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
JOUANNET, C. et al. Aeordynamic databased of a subscale demonstrator. 2017, Anais.. Reston, VA, USA: AIAA, 2017. Disponível em: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf. Acesso em: 08 jul. 2024.
APA
Jouannet, C., Lundström, D., Krus, P., Sobron, A., Silva, R. G. A. da, Catalano, F. M., & Greco Júnior, P. C. (2017). Aeordynamic databased of a subscale demonstrator. In Proceedings. Reston, VA, USA: AIAA. Recuperado de https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
NLM
Jouannet C, Lundström D, Krus P, Sobron A, Silva RGA da, Catalano FM, Greco Júnior PC. Aeordynamic databased of a subscale demonstrator [Internet]. Proceedings. 2017 ;[citado 2024 jul. 08 ] Available from: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%29.pdf
Vancouver
Jouannet C, Lundström D, Krus P, Sobron A, Silva RGA da, Catalano FM, Greco Júnior PC. Aeordynamic databased of a subscale demonstrator [Internet]. Proceedings. 2017 ;[citado 2024 jul. 08 ] Available from: https://repositorio.usp.br/directbitstream/38fa39ae-7494-4553-804a-d323744a4cd2/trabalho%2018%20-%20Aeordynamic%20databased%20of%20a%20subscale%20demonstrator.%20%2835th%20AIAA%20Applied%20Aerodynamics%20Conference%2C%202017%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
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: 08 jul. 2024.
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 2024 jul. 08 ]
Vancouver
Tavernari VD, Catalano FM. Low reynolds propeller meta-model for multidiciplinary optimization. Proceedings. 2016 ;[citado 2024 jul. 08 ]
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: 08 jul. 2024.
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 2024 jul. 08 ]
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 2024 jul. 08 ]
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: 08 jul. 2024.
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 2024 jul. 08 ]
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 2024 jul. 08 ]

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