ReP USP - Resultado da busca

Artigo de periodico
Aeroacoustics effects generated by the interaction rotor-airframe in a sUAS (2024)
Lavagnino Sanchez, Gino Rodrigo; Almeida, Odenir de; Catalano, Fernando Martini
Source: Journal of Aerospace Technology and Management. Unidade: EESC
Subjects: AEROACÚSTICA, TURBULÊNCIA, ROTOR, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
LAVAGNINO SANCHEZ, Gino Rodrigo e ALMEIDA, Odenir de e CATALANO, Fernando Martini. Aeroacoustics effects generated by the interaction rotor-airframe in a sUAS. Journal of Aerospace Technology and Management, v. 16, p. 1-13, 2024Tradução . . Disponível em: http://dx.doi.org/10.1590/jatm.v16.1327. Acesso em: 07 nov. 2024.
APA
Lavagnino Sanchez, G. R., Almeida, O. de, & Catalano, F. M. (2024). Aeroacoustics effects generated by the interaction rotor-airframe in a sUAS. Journal of Aerospace Technology and Management, 16, 1-13. doi:10.1590/jatm.v16.1327
NLM
Lavagnino Sanchez GR, Almeida O de, Catalano FM. Aeroacoustics effects generated by the interaction rotor-airframe in a sUAS [Internet]. Journal of Aerospace Technology and Management. 2024 ; 16 1-13.[citado 2024 nov. 07 ] Available from: http://dx.doi.org/10.1590/jatm.v16.1327
Vancouver
Lavagnino Sanchez GR, Almeida O de, Catalano FM. Aeroacoustics effects generated by the interaction rotor-airframe in a sUAS [Internet]. Journal of Aerospace Technology and Management. 2024 ; 16 1-13.[citado 2024 nov. 07 ] Available from: http://dx.doi.org/10.1590/jatm.v16.1327
Artigo de periodico
Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study (2023)
Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Aerospace. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study. Aerospace, v. 10, n. 7, p. 1-26, 2023Tradução . . Disponível em: https://doi.org/10.3390/aerospace10070651. Acesso em: 07 nov. 2024.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2023). Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study. Aerospace, 10( 7), 1-26. doi:10.3390/aerospace10070651
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study [Internet]. Aerospace. 2023 ; 10( 7): 1-26.[citado 2024 nov. 07 ] Available from: https://doi.org/10.3390/aerospace10070651
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Potential propulsive and aerodynamic benefits of a new aircraft concept: a low-speed experimental study [Internet]. Aerospace. 2023 ; 10( 7): 1-26.[citado 2024 nov. 07 ] Available from: https://doi.org/10.3390/aerospace10070651
Artigo de periodico
Design, aerodynamic analysis and optimization of a next‑generation commercial airliner (2022)
Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Journal of the Brazilian Society of Mechanical Sciences and Engineering. Unidade: EESC
Subjects: 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 e CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner. Journal of the Brazilian Society of Mechanical Sciences and Engineering, v. 44, p. 1-22, 2022Tradução . . Disponível em: https://doi.org/10.1007/s40430-022-03924-x. Acesso em: 07 nov. 2024.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., & Catalano, F. M. (2022). Design, aerodynamic analysis and optimization of a next‑generation commercial airliner. Journal of the Brazilian Society of Mechanical Sciences and Engineering, 44, 1-22. doi:10.1007/s40430-022-03924-x
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2022 ; 44 1-22.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1007/s40430-022-03924-x
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Catalano FM. Design, aerodynamic analysis and optimization of a next‑generation commercial airliner [Internet]. Journal of the Brazilian Society of Mechanical Sciences and Engineering. 2022 ; 44 1-22.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1007/s40430-022-03924-x
Artigo de periodico
Unconventional aircraft for civil aviation (2022)
Bravo Mosquera, Pedro David; Catalano, Fernando Martini ; Zingg, David W.
Source: Progress in Aerospace Sciences. Unidade: EESC
Subjects: AVALIAÇÃO AMBIENTAL, COMBUSTÍVEIS, IMPACTOS AMBIENTAIS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
BRAVO MOSQUERA, Pedro David e CATALANO, Fernando Martini e ZINGG, David W. Unconventional aircraft for civil aviation. Progress in Aerospace Sciences, v. 131, p. 1-29, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.paerosci.2022.100813. Acesso em: 07 nov. 2024.
APA
Bravo Mosquera, P. D., Catalano, F. M., & Zingg, D. W. (2022). Unconventional aircraft for civil aviation. Progress in Aerospace Sciences, 131, 1-29. doi:10.1016/j.paerosci.2022.100813
NLM
Bravo Mosquera PD, Catalano FM, Zingg DW. Unconventional aircraft for civil aviation [Internet]. Progress in Aerospace Sciences. 2022 ; 131 1-29.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1016/j.paerosci.2022.100813
Vancouver
Bravo Mosquera PD, Catalano FM, Zingg DW. Unconventional aircraft for civil aviation [Internet]. Progress in Aerospace Sciences. 2022 ; 131 1-29.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1016/j.paerosci.2022.100813
Artigo de periodico
Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators (2020)
Silva, Gabriel Pereira Gouveia da; Eguea, João Paulo; Croce, José Antonio Garcia; Catalano, Fernando Martini
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, FUSELAGEM DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SILVA, Gabriel Pereira Gouveia da et al. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators. Aerospace Science and Technology, v. 97, p. 1-11, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.105642. Acesso em: 07 nov. 2024.
APA
Silva, G. P. G. da, Eguea, J. P., Croce, J. A. G., & Catalano, F. M. (2020). Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators. Aerospace Science and Technology, 97, 1-11. doi:10.1016/j.ast.2019.105642
NLM
Silva GPG da, Eguea JP, Croce JAG, Catalano FM. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators [Internet]. Aerospace Science and Technology. 2020 ; 97 1-11.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1016/j.ast.2019.105642
Vancouver
Silva GPG da, Eguea JP, Croce JAG, Catalano FM. Slat aerodynamic noise reduction using dielectric barrier discharge plasma actuators [Internet]. Aerospace Science and Technology. 2020 ; 97 1-11.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1016/j.ast.2019.105642
Artigo de periodico
Fuel efficiency improvement on a business jet using a camber morphing winglet concept (2020)
Eguea, João Paulo; Silva, Gabriel Pereira Gouveia da; Catalano, Fernando Martini
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, COMBUSTÍVEIS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
EGUEA, João Paulo e SILVA, Gabriel Pereira Gouveia da e CATALANO, Fernando Martini. Fuel efficiency improvement on a business jet using a camber morphing winglet concept. Aerospace Science and Technology, v. 96, p. 1-9, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.105542. Acesso em: 07 nov. 2024.
APA
Eguea, J. P., Silva, G. P. G. da, & Catalano, F. M. (2020). Fuel efficiency improvement on a business jet using a camber morphing winglet concept. Aerospace Science and Technology, 96, 1-9. doi:10.1016/j.ast.2019.105542
NLM
Eguea JP, Silva GPG da, Catalano FM. Fuel efficiency improvement on a business jet using a camber morphing winglet concept [Internet]. Aerospace Science and Technology. 2020 ; 96 1-9.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
Vancouver
Eguea JP, Silva GPG da, Catalano FM. Fuel efficiency improvement on a business jet using a camber morphing winglet concept [Internet]. Aerospace Science and Technology. 2020 ; 96 1-9.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1016/j.ast.2019.105542
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
Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC
Subjects: ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 07 nov. 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 nov. 07 ] 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 nov. 07 ] 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
Source: Proceedings. Conference titles: International Congress and Exhibition on Noise Control Engineering. Unidade: EESC
Subjects: FUSELAGEM DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 07 nov. 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 nov. 07 ] 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 nov. 07 ] 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
Artigo de periodico
Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf (2019)
Bravo Mosquera, Pedro David; Abdalla, Alvaro Martins ; Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: PROJETO DE AERONAVES, 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. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf. Aerospace Science and Technology, v. 86, p. 497-519, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.01.059. Acesso em: 07 nov. 2024.
APA
Bravo Mosquera, P. D., Abdalla, A. M., Cerón Muñoz, H. D., & Catalano, F. M. (2019). Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf. Aerospace Science and Technology, 86, 497-519. doi:10.1016/j.ast.2019.01.059
NLM
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf [Internet]. Aerospace Science and Technology. 2019 ; 86 497-519.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
Vancouver
Bravo Mosquera PD, Abdalla AM, Cerón Muñoz HD, Catalano FM. Integration assessment of conceptual design and intake aerodynamics of a non-conventional air-to-ground fighter aircraf [Internet]. Aerospace Science and Technology. 2019 ; 86 497-519.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1016/j.ast.2019.01.059
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
Source: Proceedings. Conference titles: International Congress and Exhibition on Noise Control Engineering. Unidade: EESC
Subjects: FUSELAGEM DE AERONAVES, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 07 nov. 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 nov. 07 ] 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 nov. 07 ] 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
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.
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: ENGENHARIA AERONÁUTICA, AEROACÚSTICA, TERCEIRA DIMENSÃO
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 07 nov. 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 nov. 07 ] 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 nov. 07 ] Available from: https://doi.org/10.2514/6.2019-2406
Trabalho de evento
Neural network application for aerodynamic modeling of a variable camber winglet (2019)
Eguea, João Paulo; Caurin, Glauco Augusto de Paula ; Catalano, Fernando Martini
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: AERODINÂMICA, REDES NEURAIS, ALGORITMOS GENÉTICOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
EGUEA, João Paulo e CAURIN, Glauco Augusto de Paula e CATALANO, Fernando Martini. Neural network application for aerodynamic modeling of a variable camber winglet. 2019, Anais.. São Carlos, SP: EESC-USP, 2019. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1814/1007. Acesso em: 07 nov. 2024.
APA
Eguea, J. P., Caurin, G. A. de P., & Catalano, F. M. (2019). Neural network application for aerodynamic modeling of a variable camber winglet. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1814/1007
NLM
Eguea JP, Caurin GA de P, Catalano FM. Neural network application for aerodynamic modeling of a variable camber winglet [Internet]. Anais. 2019 ;[citado 2024 nov. 07 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1814/1007
Vancouver
Eguea JP, Caurin GA de P, Catalano FM. Neural network application for aerodynamic modeling of a variable camber winglet [Internet]. Anais. 2019 ;[citado 2024 nov. 07 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1814/1007
Trabalho de evento
Neural network metamodeling for aerodynamic optimization efficiency improvement (2019)
Silva, Gabriel Pereira Gouveia da; Catalano, Fernando Martini
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, SIMULAÇÃO, AEROFÓLIOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SILVA, Gabriel Pereira Gouveia da e CATALANO, Fernando Martini. Neural network metamodeling for aerodynamic optimization efficiency improvement. 2019, Anais.. São Carlos, SP: EESC-USP, 2019. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1715/1037. Acesso em: 07 nov. 2024.
APA
Silva, G. P. G. da, & Catalano, F. M. (2019). Neural network metamodeling for aerodynamic optimization efficiency improvement. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1715/1037
NLM
Silva GPG da, Catalano FM. Neural network metamodeling for aerodynamic optimization efficiency improvement [Internet]. Anais. 2019 ;[citado 2024 nov. 07 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1715/1037
Vancouver
Silva GPG da, Catalano FM. Neural network metamodeling for aerodynamic optimization efficiency improvement [Internet]. Anais. 2019 ;[citado 2024 nov. 07 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1715/1037
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
Source: Proceedings. Conference titles: AIAA Propulsion and Energy Forum. Unidade: EESC
Subjects: ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 07 nov. 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 nov. 07 ] 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 nov. 07 ] Available from: https://doi.org/10.2514/6.2019-3850
Trabalho de evento
Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip (2018)
Silva, Gabriel Pereira Gouveia da; Eguea, João Paulo; Catalano, Fernando Martini
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SILVA, Gabriel Pereira Gouveia da e EGUEA, João Paulo e CATALANO, Fernando Martini. Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip. 2018, Anais.. São Carlos, SP: EESC-USP, 2018. Disponível em: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811. Acesso em: 07 nov. 2024.
APA
Silva, G. P. G. da, Eguea, J. P., & Catalano, F. M. (2018). Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811
NLM
Silva GPG da, Eguea JP, Catalano FM. Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip [Internet]. Anais. 2018 ;[citado 2024 nov. 07 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811
Vancouver
Silva GPG da, Eguea JP, Catalano FM. Aerodynamic improvement of a swept wing using a dielectric barrier discharge plasma actuator at the wing tip [Internet]. Anais. 2018 ;[citado 2024 nov. 07 ] Available from: http://www.eventos.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1345/811
Artigo de periodico
Conceptual design and CFD analysis of a new prototype of agricultural aircraft (2018)
Bravo Mosquera, Pedro David; Cerón Muñoz, Hernán Darío ; Díaz Vázquez, Guillermo; Catalano, Fernando Martini
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, AERONAVES AGRÍCOLAS, 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 design and CFD analysis of a new prototype of agricultural aircraft. Aerospace Science and Technology, v. 80, p. 156-176, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2018.07.014. Acesso em: 07 nov. 2024.
APA
Bravo Mosquera, P. D., Cerón Muñoz, H. D., Díaz Vázquez, G., & Catalano, F. M. (2018). Conceptual design and CFD analysis of a new prototype of agricultural aircraft. Aerospace Science and Technology, 80, 156-176. doi:10.1016/j.ast.2018.07.014
NLM
Bravo Mosquera PD, Cerón Muñoz HD, Díaz Vázquez G, Catalano FM. Conceptual design and CFD analysis of a new prototype of agricultural aircraft [Internet]. Aerospace Science and Technology. 2018 ; 80 156-176.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
Vancouver
Bravo Mosquera PD, Cerón Muñoz HD, Díaz Vázquez G, Catalano FM. Conceptual design and CFD analysis of a new prototype of agricultural aircraft [Internet]. Aerospace Science and Technology. 2018 ; 80 156-176.[citado 2024 nov. 07 ] Available from: https://doi.org/10.1016/j.ast.2018.07.014
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
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: FLAPS, AEROACÚSTICA, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 07 nov. 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 nov. 07 ] 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 nov. 07 ] 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
Source: Proceedings. Conference titles: AIAA/CEAS Aeroacoustics Conference. Unidade: EESC
Subjects: AEROACÚSTICA, SLATS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 07 nov. 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 nov. 07 ] 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 nov. 07 ] 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.
Source: Proceedings. Conference titles: AAIA Aerospace Sciences Meeting. Unidade: EESC
Subjects: TRENS DE POUSO, ENGENHARIA AERONÁUTICA, AERODINÂMICA DE AERONAVES, AEROACÚSTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 07 nov. 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 nov. 07 ] 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 nov. 07 ] Available from: https://doi.org/10.2514/6.2018-0759
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: 07 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. 07 ] 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. 07 ] 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

USP Schools

ReP

Filtros

Document Types

Departament

Authors

USP affiliated authors

Date published

Subjects

Source title

Publisher

Conference titles

Countries/Territories

Funding Agencies

Indexado em

Non normalized affiliation

Countries of institutions of collaboration