ReP USP - Resultado da busca

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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
Computational analysis for carbon-epoxy plates damaged by low-velocity impact (2018)
Ferreira, Gregório Felipe Oliveira; Ribeiro, Marcelo Leite ; Ferreira, Antonio Joaquim Mendes; Tita, Volnei
Fonte: Proceedings. Nome do evento: Brazilian Conference on Composite Materials - BCCM. Unidade: EESC
Assuntos: MÉTODO DOS ELEMENTOS FINITOS, MATERIAIS COMPÓSITOS, ENGENHARIA AERONÁUTICA
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ABNT
FERREIRA, Gregório Felipe Oliveira et al. Computational analysis for carbon-epoxy plates damaged by low-velocity impact. 2018, Anais.. Rio de Janeiro, RJ: PUC-RJ, 2018. Disponível em: https://repositorio.usp.br/directbitstream/8caf63c0-a832-4e07-a8fe-e17fd3bdb32d/trabalho%2013%20-%20%20Computational%20analyses%20for%20carbon-epoxy%20plates%20damaged%20by%20low-velocity%20impact%20%28BCCM%204%202018%29_removed.pdf. Acesso em: 30 nov. 2025.
APA
Ferreira, G. F. O., Ribeiro, M. L., Ferreira, A. J. M., & Tita, V. (2018). Computational analysis for carbon-epoxy plates damaged by low-velocity impact. In Proceedings. Rio de Janeiro, RJ: PUC-RJ. Recuperado de https://repositorio.usp.br/directbitstream/8caf63c0-a832-4e07-a8fe-e17fd3bdb32d/trabalho%2013%20-%20%20Computational%20analyses%20for%20carbon-epoxy%20plates%20damaged%20by%20low-velocity%20impact%20%28BCCM%204%202018%29_removed.pdf
NLM
Ferreira GFO, Ribeiro ML, Ferreira AJM, Tita V. Computational analysis for carbon-epoxy plates damaged by low-velocity impact [Internet]. Proceedings. 2018 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/8caf63c0-a832-4e07-a8fe-e17fd3bdb32d/trabalho%2013%20-%20%20Computational%20analyses%20for%20carbon-epoxy%20plates%20damaged%20by%20low-velocity%20impact%20%28BCCM%204%202018%29_removed.pdf
Vancouver
Ferreira GFO, Ribeiro ML, Ferreira AJM, Tita V. Computational analysis for carbon-epoxy plates damaged by low-velocity impact [Internet]. Proceedings. 2018 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/8caf63c0-a832-4e07-a8fe-e17fd3bdb32d/trabalho%2013%20-%20%20Computational%20analyses%20for%20carbon-epoxy%20plates%20damaged%20by%20low-velocity%20impact%20%28BCCM%204%202018%29_removed.pdf
Trabalho de evento
Parametric investigation of EESC-USP aeroacoustic fan rig (2018)
Gigena Cuenca, Rafael; Greco Júnior, Paulo Celso ; Martínez Rocamora Junior, Bernardo
Fonte: Proceedings. Nome do evento: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/dac92081-b591-461c-b6c2-36d72d42eab6/AP8F33~1.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
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica (2018)
Parra Peñuela, Héctor; Gómez Rivera, William; Cerón Muñoz, Hernán Darío
Fonte: Proceedings. Nome do evento: Congreso Latinoamericano de Ingeniería Mecánica - COLIM. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, TURBINAS, ENERGIA EÓLICA, ENGENHARIA AERONÁUTICA
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ABNT
PARRA PEÑUELA, Héctor e GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. 2018, Anais.. Pamplona, Colômbia: Universidad Pamplona, 2018. Disponível em: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf. Acesso em: 30 nov. 2025.
APA
Parra Peñuela, H., Gómez Rivera, W., & Cerón Muñoz, H. D. (2018). Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica. In Proceedings. Pamplona, Colômbia: Universidad Pamplona. Recuperado de https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
NLM
Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
Vancouver
Parra Peñuela H, Gómez Rivera W, Cerón Muñoz HD. Evaluación aerodinámica mediante CFD de dispositivos en punta de aspa para turbina eólica [Internet]. Proceedings. 2018 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/bb456d94-a424-4478-92c6-ce22d26cdd6d/trabalho%2008%20-%20AERODYNAMIC%20EVALUATION%20WITH%20CFD%20OF%20TIP%20DEVICES%20IN%20BLADE%20FOR%20WIND%20TURBINE%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29.pdf
Trabalho de evento
Influence of airframe stiffness on the aerodynamic coefficients of a high aspect ratio wing (2018)
Pelegrineli, Luis Antonio Vieira; Liorbano, Felipe Fernandes; Natori, Henrique Ossamu Hisano; Angélico, Ricardo Afonso
Fonte: Proceedings. Nome do evento: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico (2018)
Ortegon Sarmiento, Tatiana; Gómez Rivera, William; Cerón Muñoz, Hernán Darío
Fonte: Proceedings. Nome do evento: Congreso Latinoamericano de Ingeniería Mecánica - COLIM. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, DINÂMICA DOS FLUÍDOS, ENERGIA EÓLICA, ENGENHARIA AERONÁUTICA
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ABNT
ORTEGON SARMIENTO, Tatiana e GÓMEZ RIVERA, William e CERÓN MUÑOZ, Hernán Darío. Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico. 2018, Anais.. Pamplona, Colômbia: Universidad Pamplona, 2018. Disponível em: https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf. Acesso em: 30 nov. 2025.
APA
Ortegon Sarmiento, T., Gómez Rivera, W., & Cerón Muñoz, H. D. (2018). Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico. In Proceedings. Pamplona, Colômbia: Universidad Pamplona. Recuperado de https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf
NLM
Ortegon Sarmiento T, Gómez Rivera W, Cerón Muñoz HD. Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico [Internet]. Proceedings. 2018 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%29_removed.pdf
Vancouver
Ortegon Sarmiento T, Gómez Rivera W, Cerón Muñoz HD. Comparación de herramientas de simulación CFD en el estudion del efecto vórtice sobre punta de aspa para rotor eólico [Internet]. Proceedings. 2018 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/1256ebe2-a474-4f95-b89d-c41cb18c47d1/trabalho%2007%20-%20COMPARISON%20OF%20CFD%20SIMULATION%20TOOLS%20IN%20THE%20STUDY%20OF%20VORTEX%20EFFECT%20ON%20WIND%20ROTOR%20BLADE%20TIP%20%28IX%20Congreso%20Latinoamericano%20de%20Ingenier%C3%ADa%20Mec%C3%A1nica%20%28COLIM%202018%29%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
Fonte: Proceedings. Nome do evento: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
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
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ABNT
BRAVO MOSQUERA, Pedro David et al. Design and performance assessment of an inverted rectangular dorsal intake for military aviation. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/f61f0f51-4199-4f6a-af2a-132b70c86bd1/trabalho%2003%20-%20DESIGN%20AND%20PERFORMANCE%20ASSESSMENT%20OF%20AN%20INVERTED%20RECTANGULAR%20DORSAL%20INTAKE%20FOR%20MILITARY%20AVIATION%20%28ICAS%202018%29.pdf. Acesso em: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES
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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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
Pio susceptibility in fly-by-wire systems (2018)
Moura, Herlandson Cardoso de; Porto Alegre, Gabriel Setim; Bidinotto, Jorge Henrique ; Belo, Eduardo Morgado
Fonte: Proceedings. Nome do evento: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
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
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ABNT
SOUZA, Joabe Marcos de e CATALANO, Fernando Martini. Multi-disciplinary design optimization of a blended winglet. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf. Acesso em: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] 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
Fonte: Proceedings. Nome do evento: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Assuntos: 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: 30 nov. 2025.
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 2025 nov. 30 ] 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 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/7e51e7b5-9bd8-4125-9976-d891205e1faf/trabalho%2001%20-%20DESIGN%20OF%20AN%20INSTRUMENTED%20STATOR%20VANE%20FOR%20UNSTEADY%20PRESSURE%20MEASUREMENTS%20USING%20MEMS%20MICROPHONES%20%28ICAS%202018%29.pdf
Trabalho de evento
The influence of matrix impregnation on effective elastic properties of a unidirectional carbon nanotube bundled composite: a topology optimization approach (2018)
Christoff, Bruno Guilherme; Santana, Humberto Brito; Cardoso, Eduardo L.; Abot, Jandro L ; Tita, Volnei
Fonte: Proceedings. Nome do evento: Brazilian Conference on Composite Materials - BCCM. Unidade: EESC
Assuntos: TOPOLOGIA, MATERIAIS COMPÓSITOS DE FIBRAS, ENGENHARIA AERONÁUTICA
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ABNT
CHRISTOFF, Bruno Guilherme et al. The influence of matrix impregnation on effective elastic properties of a unidirectional carbon nanotube bundled composite: a topology optimization approach. 2018, Anais.. Rio de Janeiro, RJ: PUC-RJ, 2018. Disponível em: https://repositorio.usp.br/directbitstream/8a52a830-4d39-484e-a9a1-81ad77236382/trabalho%2019%20-%20The%20influence%20of%20matrix%20impregnation%20on%20effective%20elastic%20properties%20of%20a%20unidirectional%20carbon%20nanotube%20bundled%20composite%20a%20topology%20optimization%20approach%20%28BCCM4%29.pdf. Acesso em: 30 nov. 2025.
APA
Christoff, B. G., Santana, H. B., Cardoso, E. L., Abot, J. L., & Tita, V. (2018). The influence of matrix impregnation on effective elastic properties of a unidirectional carbon nanotube bundled composite: a topology optimization approach. In Proceedings. Rio de Janeiro, RJ: PUC-RJ. Recuperado de https://repositorio.usp.br/directbitstream/8a52a830-4d39-484e-a9a1-81ad77236382/trabalho%2019%20-%20The%20influence%20of%20matrix%20impregnation%20on%20effective%20elastic%20properties%20of%20a%20unidirectional%20carbon%20nanotube%20bundled%20composite%20a%20topology%20optimization%20approach%20%28BCCM4%29.pdf
NLM
Christoff BG, Santana HB, Cardoso EL, Abot JL, Tita V. The influence of matrix impregnation on effective elastic properties of a unidirectional carbon nanotube bundled composite: a topology optimization approach [Internet]. Proceedings. 2018 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/8a52a830-4d39-484e-a9a1-81ad77236382/trabalho%2019%20-%20The%20influence%20of%20matrix%20impregnation%20on%20effective%20elastic%20properties%20of%20a%20unidirectional%20carbon%20nanotube%20bundled%20composite%20a%20topology%20optimization%20approach%20%28BCCM4%29.pdf
Vancouver
Christoff BG, Santana HB, Cardoso EL, Abot JL, Tita V. The influence of matrix impregnation on effective elastic properties of a unidirectional carbon nanotube bundled composite: a topology optimization approach [Internet]. Proceedings. 2018 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/8a52a830-4d39-484e-a9a1-81ad77236382/trabalho%2019%20-%20The%20influence%20of%20matrix%20impregnation%20on%20effective%20elastic%20properties%20of%20a%20unidirectional%20carbon%20nanotube%20bundled%20composite%20a%20topology%20optimization%20approach%20%28BCCM4%29.pdf
Trabalho de evento
Linear stability theory applied in a cross-stream profile of a shear layer of a leading edge slat (2017)
Himeno, Fernando Henrique Tadashi; Amaral, Filipe Ramos do; Medeiros, Marcello Augusto Faraco de
Fonte: Proceedings. Nome do evento: Iberian Latin-American Congress on Computational Methods in Engineering - CILAMCE. Unidade: EESC
Assuntos: SLATS, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
HIMENO, Fernando Henrique Tadashi e AMARAL, Filipe Ramos do e MEDEIROS, Marcello Augusto Faraco de. Linear stability theory applied in a cross-stream profile of a shear layer of a leading edge slat. 2017, Anais.. [Belo Horizonte, MG]: ABMEC, 2017. Disponível em: https://repositorio.usp.br/directbitstream/4d9e4862-f0f4-42db-83eb-d4dbf7b966c4/trabalho%2013%20-%20Linear%20Stability%20Theory%20applied%20in%20a%20croos-stream%20profile%20of%20a%20shear%20layer%20of%20leading%20edge%20slat%20%28CILAMCE%202017%29.pdf. Acesso em: 30 nov. 2025.
APA
Himeno, F. H. T., Amaral, F. R. do, & Medeiros, M. A. F. de. (2017). Linear stability theory applied in a cross-stream profile of a shear layer of a leading edge slat. In Proceedings. [Belo Horizonte, MG]: ABMEC. Recuperado de https://repositorio.usp.br/directbitstream/4d9e4862-f0f4-42db-83eb-d4dbf7b966c4/trabalho%2013%20-%20Linear%20Stability%20Theory%20applied%20in%20a%20croos-stream%20profile%20of%20a%20shear%20layer%20of%20leading%20edge%20slat%20%28CILAMCE%202017%29.pdf
NLM
Himeno FHT, Amaral FR do, Medeiros MAF de. Linear stability theory applied in a cross-stream profile of a shear layer of a leading edge slat [Internet]. Proceedings. 2017 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/4d9e4862-f0f4-42db-83eb-d4dbf7b966c4/trabalho%2013%20-%20Linear%20Stability%20Theory%20applied%20in%20a%20croos-stream%20profile%20of%20a%20shear%20layer%20of%20leading%20edge%20slat%20%28CILAMCE%202017%29.pdf
Vancouver
Himeno FHT, Amaral FR do, Medeiros MAF de. Linear stability theory applied in a cross-stream profile of a shear layer of a leading edge slat [Internet]. Proceedings. 2017 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/4d9e4862-f0f4-42db-83eb-d4dbf7b966c4/trabalho%2013%20-%20Linear%20Stability%20Theory%20applied%20in%20a%20croos-stream%20profile%20of%20a%20shear%20layer%20of%20leading%20edge%20slat%20%28CILAMCE%202017%29.pdf
Trabalho de evento
Effects of geometric nonlinearities of shape memory alloy springs on the aeroelastic behavior of a typical airfoil section (2017)
Sousa, Vagner Candido de; De Marqui Júnior, Carlos ; Elahinia, Mohammad H
Fonte: Proceedings. Nome do evento: International Symposium on Dynamic Problems of Mechanics - DINAME. Unidade: EESC
Assuntos: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SOUSA, Vagner Candido de e DE MARQUI JÚNIOR, Carlos e ELAHINIA, Mohammad H. Effects of geometric nonlinearities of shape memory alloy springs on the aeroelastic behavior of a typical airfoil section. 2017, Anais.. Rio de Janeiro, RJ: ABCM, 2017. Disponível em: https://repositorio.usp.br/directbitstream/07ce36ee-020b-4349-85b4-ffecd3e18b47/trabalho%2016%20-%20Effects%20of%20geometric%20nonlinearities%20of%20shape%20memory%20alloy%20springs%20on%20the%20aeroelastic%20behavior%20of%20a%20typical%20airfoil%20section%20%28diname%202017%29_removed.pdf. Acesso em: 30 nov. 2025.
APA
Sousa, V. C. de, De Marqui Júnior, C., & Elahinia, M. H. (2017). Effects of geometric nonlinearities of shape memory alloy springs on the aeroelastic behavior of a typical airfoil section. In Proceedings. Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/07ce36ee-020b-4349-85b4-ffecd3e18b47/trabalho%2016%20-%20Effects%20of%20geometric%20nonlinearities%20of%20shape%20memory%20alloy%20springs%20on%20the%20aeroelastic%20behavior%20of%20a%20typical%20airfoil%20section%20%28diname%202017%29_removed.pdf
NLM
Sousa VC de, De Marqui Júnior C, Elahinia MH. Effects of geometric nonlinearities of shape memory alloy springs on the aeroelastic behavior of a typical airfoil section [Internet]. Proceedings. 2017 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/07ce36ee-020b-4349-85b4-ffecd3e18b47/trabalho%2016%20-%20Effects%20of%20geometric%20nonlinearities%20of%20shape%20memory%20alloy%20springs%20on%20the%20aeroelastic%20behavior%20of%20a%20typical%20airfoil%20section%20%28diname%202017%29_removed.pdf
Vancouver
Sousa VC de, De Marqui Júnior C, Elahinia MH. Effects of geometric nonlinearities of shape memory alloy springs on the aeroelastic behavior of a typical airfoil section [Internet]. Proceedings. 2017 ;[citado 2025 nov. 30 ] Available from: https://repositorio.usp.br/directbitstream/07ce36ee-020b-4349-85b4-ffecd3e18b47/trabalho%2016%20-%20Effects%20of%20geometric%20nonlinearities%20of%20shape%20memory%20alloy%20springs%20on%20the%20aeroelastic%20behavior%20of%20a%20typical%20airfoil%20section%20%28diname%202017%29_removed.pdf
Trabalho de evento
A finite element damage model to predict failure behavior of composite sandwich structures (2016)
Garcia, David A; Tita, Volnei ; Ribeiro, Marcelo Leite
Fonte: Proceedings. Nome do evento: Brazilian Conference on Composite Materials. Unidade: EESC
Assuntos: MATERIAIS COMPÓSITOS, MÉTODO DOS ELEMENTOS FINITOS, DANO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GARCIA, David A e TITA, Volnei e RIBEIRO, Marcelo Leite. A finite element damage model to predict failure behavior of composite sandwich structures. 2016, Anais.. Porto Alegre, RS: UFRGS, 2016. . Acesso em: 30 nov. 2025.
APA
Garcia, D. A., Tita, V., & Ribeiro, M. L. (2016). A finite element damage model to predict failure behavior of composite sandwich structures. In Proceedings. Porto Alegre, RS: UFRGS.
NLM
Garcia DA, Tita V, Ribeiro ML. A finite element damage model to predict failure behavior of composite sandwich structures. Proceedings. 2016 ;[citado 2025 nov. 30 ]
Vancouver
Garcia DA, Tita V, Ribeiro ML. A finite element damage model to predict failure behavior of composite sandwich structures. Proceedings. 2016 ;[citado 2025 nov. 30 ]
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: 30 nov. 2025.
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 2025 nov. 30 ]
Vancouver
Tavernari VD, Catalano FM. Low reynolds propeller meta-model for multidiciplinary optimization. Proceedings. 2016 ;[citado 2025 nov. 30 ]

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