ReP USP - Resultado da busca

Artigo de periodico
Finite wing effects on the energy harvesting from stall-induced oscillations (2022)
Santos, Carlos Renan dos ; Marques, Flavio Donizeti
Source: Journal of Vibration and Control. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ASAS DE AERONAVES, KRIGAGEM, ENGENHARIA MECÂNICA
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ABNT
SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Finite wing effects on the energy harvesting from stall-induced oscillations. Journal of Vibration and Control, p. 1-17, 2022Tradução . . Disponível em: https://doi.org/10.1177/10775463221089732. Acesso em: 09 nov. 2024.
APA
Santos, C. R. dos, & Marques, F. D. (2022). Finite wing effects on the energy harvesting from stall-induced oscillations. Journal of Vibration and Control, 1-17. doi:10.1177/10775463221089732
NLM
Santos CR dos, Marques FD. Finite wing effects on the energy harvesting from stall-induced oscillations [Internet]. Journal of Vibration and Control. 2022 ; 1-17.[citado 2024 nov. 09 ] Available from: https://doi.org/10.1177/10775463221089732
Vancouver
Santos CR dos, Marques FD. Finite wing effects on the energy harvesting from stall-induced oscillations [Internet]. Journal of Vibration and Control. 2022 ; 1-17.[citado 2024 nov. 09 ] Available from: https://doi.org/10.1177/10775463221089732
Trabalho de evento-anais periodico
Modeling and prediction of aerodynamic characteristics of free fall rotating wing based on experiments (2019)
Zakaria, Mohamed Y; Santos, Carlos Renan dos ; Dayhoum, Abdallah; Marques, Flavio Donizeti ; Hajj, Muhammad R
Source: IOP Conference. Series: Materials Science and Engineering. Conference titles: International Conference on Aerospace Sciences & Aviation Technology. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ASAS DE AERONAVES, ENGENHARIA MECÂNICA
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ZAKARIA, Mohamed Y et al. Modeling and prediction of aerodynamic characteristics of free fall rotating wing based on experiments. IOP Conference. Series: Materials Science and Engineering. Bristol, United Kingdom: IOP Publishing. Disponível em: https://doi.org/10.1088/1757-899X/610/1/012098. Acesso em: 09 nov. 2024. , 2019
APA
Zakaria, M. Y., Santos, C. R. dos, Dayhoum, A., Marques, F. D., & Hajj, M. R. (2019). Modeling and prediction of aerodynamic characteristics of free fall rotating wing based on experiments. IOP Conference. Series: Materials Science and Engineering. Bristol, United Kingdom: IOP Publishing. doi:10.1088/1757-899X/610/1/012098
NLM
Zakaria MY, Santos CR dos, Dayhoum A, Marques FD, Hajj MR. Modeling and prediction of aerodynamic characteristics of free fall rotating wing based on experiments [Internet]. IOP Conference. Series: Materials Science and Engineering. 2019 ; 610 1-15.[citado 2024 nov. 09 ] Available from: https://doi.org/10.1088/1757-899X/610/1/012098
Vancouver
Zakaria MY, Santos CR dos, Dayhoum A, Marques FD, Hajj MR. Modeling and prediction of aerodynamic characteristics of free fall rotating wing based on experiments [Internet]. IOP Conference. Series: Materials Science and Engineering. 2019 ; 610 1-15.[citado 2024 nov. 09 ] Available from: https://doi.org/10.1088/1757-899X/610/1/012098
Trabalho de evento
Evaluation of delta wing effects on the stealth-aerodynamic features for non-conventional fighter aircraft (2018)
Bravo Mosquera, Pedro David; Abdalla, Alvaro Martins ; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA, ASAS DE AERONAVES
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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: 09 nov. 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 nov. 09 ] 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 nov. 09 ] Available from: https://repositorio.usp.br/directbitstream/d5e79d68-cf3c-49f9-acbe-477649c98a5f/trabalho%2013%20-%20EVALUATION%20OF%20DELTA%20WING%20EFFECTS%20ON%20THE%20STEALTH-AERODYNAMIC%20FEATURES%20FOR%20NON-CONVENTIONAL%20FIGHTER%20AIRCRAFT%20%28ICAS%202018%29.pdf
Trabalho de evento
Multi-disciplinary design optimization of a blended winglet (2018)
Souza, Joabe Marcos de; Catalano, Fernando Martini
Source: Proceedings. Conference titles: Congress of the International Council of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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SOUZA, Joabe Marcos de e CATALANO, Fernando Martini. Multi-disciplinary design optimization of a blended winglet. 2018, Anais.. Edinburgh, UK: ICAS, 2018. Disponível em: https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf. Acesso em: 09 nov. 2024.
APA
Souza, J. M. de, & Catalano, F. M. (2018). Multi-disciplinary design optimization of a blended winglet. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf
NLM
Souza JM de, Catalano FM. Multi-disciplinary design optimization of a blended winglet [Internet]. Proceedings. 2018 ;[citado 2024 nov. 09 ] Available from: https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf
Vancouver
Souza JM de, Catalano FM. Multi-disciplinary design optimization of a blended winglet [Internet]. Proceedings. 2018 ;[citado 2024 nov. 09 ] Available from: https://repositorio.usp.br/directbitstream/ffc31cc4-3571-4812-b80b-2974af6f98c6/trabalho%2014%20-%20MULTI-DISCIPLINARY%20DESIGN%20OPTIMIZATION%20OF%20A%20BLENDED%20WINGLET%20%28ICAS%202018%29.pdf
Trabalho de evento
Experimental analyses of droop, wingtips and fences on a BWB model (2016)
Cerón Muñoz, Hernán Darío ; Diaz Izquierdo, David Orlando; Bravo Mosquera, Pedro David; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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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: 09 nov. 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 nov. 09 ]
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 nov. 09 ]
Trabalho de evento
Aerodynamic interference of wingtip and wing devices on BWB model (2014)
Cerón Muñoz, Hernán Darío ; Diaz Izquierdo, David Orlando; Solarte Pineda, Jhonathan; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
CERÓN MUÑOZ, Hernán Darío et al. Aerodynamic interference of wingtip and wing devices on BWB model. 2014, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2014. . Acesso em: 09 nov. 2024.
APA
Cerón Muñoz, H. D., Diaz Izquierdo, D. O., Solarte Pineda, J., & Catalano, F. M. (2014). Aerodynamic interference of wingtip and wing devices on BWB model. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cerón Muñoz HD, Diaz Izquierdo DO, Solarte Pineda J, Catalano FM. Aerodynamic interference of wingtip and wing devices on BWB model. Proceedings. 2014 ;[citado 2024 nov. 09 ]
Vancouver
Cerón Muñoz HD, Diaz Izquierdo DO, Solarte Pineda J, Catalano FM. Aerodynamic interference of wingtip and wing devices on BWB model. Proceedings. 2014 ;[citado 2024 nov. 09 ]
Trabalho de evento
Experimental analysis of the aerodynamics of porous flap side-edge (2014)
Moraleda, F. P.; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
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MORALEDA, F. P. e CATALANO, Fernando Martini. Experimental analysis of the aerodynamics of porous flap side-edge. 2014, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2014. . Acesso em: 09 nov. 2024.
APA
Moraleda, F. P., & Catalano, F. M. (2014). Experimental analysis of the aerodynamics of porous flap side-edge. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Moraleda FP, Catalano FM. Experimental analysis of the aerodynamics of porous flap side-edge. Proceedings. 2014 ;[citado 2024 nov. 09 ]
Vancouver
Moraleda FP, Catalano FM. Experimental analysis of the aerodynamics of porous flap side-edge. Proceedings. 2014 ;[citado 2024 nov. 09 ]
Trabalho de evento
Aerodynamic analysis of multi-winglets for low speed aircraft (2012)
Cosin, Renato; Catalano, Fernando Martini ; Correa, Luiz Guilherme Noujain; Entz, Ricardo Maiko Uehoka
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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COSIN, Renato et al. Aerodynamic analysis of multi-winglets for low speed aircraft. 2012, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2012. . Acesso em: 09 nov. 2024.
APA
Cosin, R., Catalano, F. M., Correa, L. G. N., & Entz, R. M. U. (2012). Aerodynamic analysis of multi-winglets for low speed aircraft. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cosin R, Catalano FM, Correa LGN, Entz RMU. Aerodynamic analysis of multi-winglets for low speed aircraft. Proceedings. 2012 ;[citado 2024 nov. 09 ]
Vancouver
Cosin R, Catalano FM, Correa LGN, Entz RMU. Aerodynamic analysis of multi-winglets for low speed aircraft. Proceedings. 2012 ;[citado 2024 nov. 09 ]
Trabalho de evento
Trailing edge treatment to enhance high lift system performance (2012)
Catalano, Fernando Martini ; Cerón Muñoz, Hernán Darío ; Greco Júnior, Paulo Celso
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ASAS DE AERONAVES, AEROFÓLIOS, ENGENHARIA AERONÁUTICA
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CATALANO, Fernando Martini e CERÓN MUÑOZ, Hernán Darío e GRECO JÚNIOR, Paulo Celso. Trailing edge treatment to enhance high lift system performance. 2012, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2012. . Acesso em: 09 nov. 2024.
APA
Catalano, F. M., Cerón Muñoz, H. D., & Greco Júnior, P. C. (2012). Trailing edge treatment to enhance high lift system performance. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Catalano FM, Cerón Muñoz HD, Greco Júnior PC. Trailing edge treatment to enhance high lift system performance. Proceedings. 2012 ;[citado 2024 nov. 09 ]
Vancouver
Catalano FM, Cerón Muñoz HD, Greco Júnior PC. Trailing edge treatment to enhance high lift system performance. Proceedings. 2012 ;[citado 2024 nov. 09 ]
Trabalho de evento
Wind tunnel testing of porous devices for the reduction of flap side-edge noise (2012)
Catalano, Fernando Martini ; Vanuchi, Paulo; Correa, Luiz Guilherme Noujain
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: TÚNEIS DE VENTO, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
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CATALANO, Fernando Martini e VANUCHI, Paulo e CORREA, Luiz Guilherme Noujain. Wind tunnel testing of porous devices for the reduction of flap side-edge noise. 2012, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2012. . Acesso em: 09 nov. 2024.
APA
Catalano, F. M., Vanuchi, P., & Correa, L. G. N. (2012). Wind tunnel testing of porous devices for the reduction of flap side-edge noise. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Catalano FM, Vanuchi P, Correa LGN. Wind tunnel testing of porous devices for the reduction of flap side-edge noise. Proceedings. 2012 ;[citado 2024 nov. 09 ]
Vancouver
Catalano FM, Vanuchi P, Correa LGN. Wind tunnel testing of porous devices for the reduction of flap side-edge noise. Proceedings. 2012 ;[citado 2024 nov. 09 ]
Trabalho de evento
Aerodynamic interference of power-plant system on a blended wing body (2010)
Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Aerodynamic interference of power-plant system on a blended wing body. 2010, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2010. . Acesso em: 09 nov. 2024.
APA
Cerón Muñoz, H. D., & Catalano, F. M. (2010). Aerodynamic interference of power-plant system on a blended wing body. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cerón Muñoz HD, Catalano FM. Aerodynamic interference of power-plant system on a blended wing body. Proceedings. 2010 ;[citado 2024 nov. 09 ]
Vancouver
Cerón Muñoz HD, Catalano FM. Aerodynamic interference of power-plant system on a blended wing body. Proceedings. 2010 ;[citado 2024 nov. 09 ]
Trabalho de evento
Passive, active, and adaptative systems for wing vortex drag reduction (2008)
Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini ; Coimbra, R. F.
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ASAS DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
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CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini e COIMBRA, R. F. Passive, active, and adaptative systems for wing vortex drag reduction. 2008, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2008. . Acesso em: 09 nov. 2024.
APA
Cerón Muñoz, H. D., Catalano, F. M., & Coimbra, R. F. (2008). Passive, active, and adaptative systems for wing vortex drag reduction. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Cerón Muñoz HD, Catalano FM, Coimbra RF. Passive, active, and adaptative systems for wing vortex drag reduction. Proceedings. 2008 ;[citado 2024 nov. 09 ]
Vancouver
Cerón Muñoz HD, Catalano FM, Coimbra RF. Passive, active, and adaptative systems for wing vortex drag reduction. Proceedings. 2008 ;[citado 2024 nov. 09 ]
Trabalho de evento
Aero-structural MDO of a spar-tank-type wing for aircraft conceptual design (2008)
Caixeta Junior, Paulo Roberto; Marques, Flavio Donizeti ; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, ALGORITMOS GENÉTICOS, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
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CAIXETA JUNIOR, Paulo Roberto e MARQUES, Flavio Donizeti e CATALANO, Fernando Martini. Aero-structural MDO of a spar-tank-type wing for aircraft conceptual design. 2008, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2008. . Acesso em: 09 nov. 2024.
APA
Caixeta Junior, P. R., Marques, F. D., & Catalano, F. M. (2008). Aero-structural MDO of a spar-tank-type wing for aircraft conceptual design. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Caixeta Junior PR, Marques FD, Catalano FM. Aero-structural MDO of a spar-tank-type wing for aircraft conceptual design. Proceedings. 2008 ;[citado 2024 nov. 09 ]
Vancouver
Caixeta Junior PR, Marques FD, Catalano FM. Aero-structural MDO of a spar-tank-type wing for aircraft conceptual design. Proceedings. 2008 ;[citado 2024 nov. 09 ]
Artigo de periodico
Experimental analysis of the aerodynamic characteristics adaptive of multi-winglets (2006)
Cerón Muñoz, Hernán Darío ; Catalano, Fernando Martini
Source: Proceedings of the Institution of Mechanical Engineers. Part G: Journal of Aerospace Engineering. Unidade: EESC
Subjects: ASAS DE AERONAVES, AERODINÂMICA DE AERONAVES, AERODINÂMICA DE AERONAVES, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
CERÓN MUÑOZ, Hernán Darío e CATALANO, Fernando Martini. Experimental analysis of the aerodynamic characteristics adaptive of multi-winglets. Proceedings of the Institution of Mechanical Engineers. Part G: Journal of Aerospace Engineering, v. 220, n. 3, p. 209-215, 2006Tradução . . Disponível em: https://doi.org/10.1243/09544100JAERO22. Acesso em: 09 nov. 2024.
APA
Cerón Muñoz, H. D., & Catalano, F. M. (2006). Experimental analysis of the aerodynamic characteristics adaptive of multi-winglets. Proceedings of the Institution of Mechanical Engineers. Part G: Journal of Aerospace Engineering, 220( 3), 209-215. doi:10.1243/09544100JAERO22
NLM
Cerón Muñoz HD, Catalano FM. Experimental analysis of the aerodynamic characteristics adaptive of multi-winglets [Internet]. Proceedings of the Institution of Mechanical Engineers. Part G: Journal of Aerospace Engineering. 2006 ; 220( 3): 209-215.[citado 2024 nov. 09 ] Available from: https://doi.org/10.1243/09544100JAERO22
Vancouver
Cerón Muñoz HD, Catalano FM. Experimental analysis of the aerodynamic characteristics adaptive of multi-winglets [Internet]. Proceedings of the Institution of Mechanical Engineers. Part G: Journal of Aerospace Engineering. 2006 ; 220( 3): 209-215.[citado 2024 nov. 09 ] Available from: https://doi.org/10.1243/09544100JAERO22
Trabalho de evento
Experimental and numerical study of two-element wing with gurney flap (2006)
Catalano, Fernando Martini ; Brand, Gerson Luiz
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AEROFÓLIOS, TÚNEIS DE VENTO, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CATALANO, Fernando Martini e BRAND, Gerson Luiz. Experimental and numerical study of two-element wing with gurney flap. 2006, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2006. . Acesso em: 09 nov. 2024.
APA
Catalano, F. M., & Brand, G. L. (2006). Experimental and numerical study of two-element wing with gurney flap. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Catalano FM, Brand GL. Experimental and numerical study of two-element wing with gurney flap. Proceedings. 2006 ;[citado 2024 nov. 09 ]
Vancouver
Catalano FM, Brand GL. Experimental and numerical study of two-element wing with gurney flap. Proceedings. 2006 ;[citado 2024 nov. 09 ]
Trabalho de evento
Wind tunnel wall boundary layer control for 2D high lift wing testing (2004)
Catalano, Fernando Martini ; Caixeta Junior, Paulo Roberto
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CATALANO, Fernando Martini e CAIXETA JUNIOR, Paulo Roberto. Wind tunnel wall boundary layer control for 2D high lift wing testing. 2004, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2004. . Acesso em: 09 nov. 2024.
APA
Catalano, F. M., & Caixeta Junior, P. R. (2004). Wind tunnel wall boundary layer control for 2D high lift wing testing. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Catalano FM, Caixeta Junior PR. Wind tunnel wall boundary layer control for 2D high lift wing testing. Proceedings. 2004 ;[citado 2024 nov. 09 ]
Vancouver
Catalano FM, Caixeta Junior PR. Wind tunnel wall boundary layer control for 2D high lift wing testing. Proceedings. 2004 ;[citado 2024 nov. 09 ]
Trabalho de evento
Experimental analysis of the confluent boundary layer between a flap and a main element with saw-toothed trailing edge (2004)
Lemes, Rodrigo Cristian; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ASAS DE AERONAVES, TÚNEIS DE VENTO, AERODINÂMICA DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
LEMES, Rodrigo Cristian e CATALANO, Fernando Martini. Experimental analysis of the confluent boundary layer between a flap and a main element with saw-toothed trailing edge. 2004, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2004. . Acesso em: 09 nov. 2024.
APA
Lemes, R. C., & Catalano, F. M. (2004). Experimental analysis of the confluent boundary layer between a flap and a main element with saw-toothed trailing edge. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Lemes RC, Catalano FM. Experimental analysis of the confluent boundary layer between a flap and a main element with saw-toothed trailing edge. Proceedings. 2004 ;[citado 2024 nov. 09 ]
Vancouver
Lemes RC, Catalano FM. Experimental analysis of the confluent boundary layer between a flap and a main element with saw-toothed trailing edge. Proceedings. 2004 ;[citado 2024 nov. 09 ]
Trabalho de evento
Experimental analysis of aerodynamics characteristics of adaptative multi-winglets (2004)
Catalano, Fernando Martini ; Cerón Muñoz, Hernán Darío
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CATALANO, Fernando Martini e CERÓN MUÑOZ, Hernán Darío. Experimental analysis of aerodynamics characteristics of adaptative multi-winglets. 2004, Anais.. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS, 2004. . Acesso em: 09 nov. 2024.
APA
Catalano, F. M., & Cerón Muñoz, H. D. (2004). Experimental analysis of aerodynamics characteristics of adaptative multi-winglets. In Proceedings. Edinburgh, UK: Optimage Ltd/International Council of Aeronautical Sciences - ICAS.
NLM
Catalano FM, Cerón Muñoz HD. Experimental analysis of aerodynamics characteristics of adaptative multi-winglets. Proceedings. 2004 ;[citado 2024 nov. 09 ]
Vancouver
Catalano FM, Cerón Muñoz HD. Experimental analysis of aerodynamics characteristics of adaptative multi-winglets. Proceedings. 2004 ;[citado 2024 nov. 09 ]
Trabalho de evento
The effect of wing tip blowing on the vortex drag (2002)
Coimbra, Rogerio Frauendorf de Faria; Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences. Unidade: EESC
Subjects: ASAS DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
COIMBRA, Rogerio Frauendorf de Faria e CATALANO, Fernando Martini. The effect of wing tip blowing on the vortex drag. 2002, Anais.. Edinburgh, UK: ICAS, 2002. Disponível em: https://repositorio.usp.br/directbitstream/dae722bf-f2b1-4c9b-9634-651bd272a597/trabalho%2062%20-%20The%20Effect%20of%20Wing%20Tip%20Blowing%20on%20the%20Vortex%20Drag%20%28ICAS%202002%29%20%281%29.PDF. Acesso em: 09 nov. 2024.
APA
Coimbra, R. F. de F., & Catalano, F. M. (2002). The effect of wing tip blowing on the vortex drag. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/dae722bf-f2b1-4c9b-9634-651bd272a597/trabalho%2062%20-%20The%20Effect%20of%20Wing%20Tip%20Blowing%20on%20the%20Vortex%20Drag%20%28ICAS%202002%29%20%281%29.PDF
NLM
Coimbra RF de F, Catalano FM. The effect of wing tip blowing on the vortex drag [Internet]. Proceedings. 2002 ;[citado 2024 nov. 09 ] Available from: https://repositorio.usp.br/directbitstream/dae722bf-f2b1-4c9b-9634-651bd272a597/trabalho%2062%20-%20The%20Effect%20of%20Wing%20Tip%20Blowing%20on%20the%20Vortex%20Drag%20%28ICAS%202002%29%20%281%29.PDF
Vancouver
Coimbra RF de F, Catalano FM. The effect of wing tip blowing on the vortex drag [Internet]. Proceedings. 2002 ;[citado 2024 nov. 09 ] Available from: https://repositorio.usp.br/directbitstream/dae722bf-f2b1-4c9b-9634-651bd272a597/trabalho%2062%20-%20The%20Effect%20of%20Wing%20Tip%20Blowing%20on%20the%20Vortex%20Drag%20%28ICAS%202002%29%20%281%29.PDF
Trabalho de evento
On the effects of a installed propeller slipstream on a wing boundary layer (2000)
Catalano, Fernando Martini
Source: Proceedings. Conference titles: International Congress of the Aeronautical Sciences - ICAS. Unidade: EESC
Subjects: HÉLICES DE AERONAVES, ASAS DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CATALANO, Fernando Martini. On the effects of a installed propeller slipstream on a wing boundary layer. 2000, Anais.. Edinburgh, UK: ICAS, 2000. Disponível em: https://repositorio.usp.br/directbitstream/1b10d0cd-d281-4466-ae2e-a3489451ccde/trabalho%2067%20-%20ON%20THE%20EFFECTS%20OF%20A%20INSTALLED%20PROPELLER%20SLIPSTREAM%20ON%20A%20WING%20BOUNDARY%20LAYER%20%28ICAS%202000%29.PDF. Acesso em: 09 nov. 2024.
APA
Catalano, F. M. (2000). On the effects of a installed propeller slipstream on a wing boundary layer. In Proceedings. Edinburgh, UK: ICAS. Recuperado de https://repositorio.usp.br/directbitstream/1b10d0cd-d281-4466-ae2e-a3489451ccde/trabalho%2067%20-%20ON%20THE%20EFFECTS%20OF%20A%20INSTALLED%20PROPELLER%20SLIPSTREAM%20ON%20A%20WING%20BOUNDARY%20LAYER%20%28ICAS%202000%29.PDF
NLM
Catalano FM. On the effects of a installed propeller slipstream on a wing boundary layer [Internet]. Proceedings. 2000 ;[citado 2024 nov. 09 ] Available from: https://repositorio.usp.br/directbitstream/1b10d0cd-d281-4466-ae2e-a3489451ccde/trabalho%2067%20-%20ON%20THE%20EFFECTS%20OF%20A%20INSTALLED%20PROPELLER%20SLIPSTREAM%20ON%20A%20WING%20BOUNDARY%20LAYER%20%28ICAS%202000%29.PDF
Vancouver
Catalano FM. On the effects of a installed propeller slipstream on a wing boundary layer [Internet]. Proceedings. 2000 ;[citado 2024 nov. 09 ] Available from: https://repositorio.usp.br/directbitstream/1b10d0cd-d281-4466-ae2e-a3489451ccde/trabalho%2067%20-%20ON%20THE%20EFFECTS%20OF%20A%20INSTALLED%20PROPELLER%20SLIPSTREAM%20ON%20A%20WING%20BOUNDARY%20LAYER%20%28ICAS%202000%29.PDF

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