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Trabalho de evento
The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity (2018)
Mathias, Marlon Sproesser; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC
Subjects: AEROACÚSTICA, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
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ABNT
MATHIAS, Marlon Sproesser e MEDEIROS, Marcello Augusto Faraco de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3386. Acesso em: 03 nov. 2024.
APA
Mathias, M. S., & Medeiros, M. A. F. de. (2018). The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3386
NLM
Mathias MS, Medeiros MAF de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity [Internet]. Proceedings. 2018 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2018-3386
Vancouver
Mathias MS, Medeiros MAF de. The influence of the boundary layer thickness on the stability of the Rossiter modes of a compressible rectangular cavity [Internet]. Proceedings. 2018 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2018-3386
Trabalho de evento
Study on a camber adaptive winglet (2018)
Eguea, João Paulo; Catalano, Fernando Martini ; Abdalla, Alvaro Martins ; Santana, Leandro de; Venner, Cornelis H.
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidades: EEL, EESC
Subjects: ESTRUTURA DE AERONAVES, VOO (ENGENHARIA AERONÁUTICA), ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
EGUEA, João Paulo et al. Study on a camber adaptive winglet. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3960. Acesso em: 03 nov. 2024.
APA
Eguea, J. P., Catalano, F. M., Abdalla, A. M., Santana, L. de, & Venner, C. H. (2018). Study on a camber adaptive winglet. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3960
NLM
Eguea JP, Catalano FM, Abdalla AM, Santana L de, Venner CH. Study on a camber adaptive winglet [Internet]. Proceedings. 2018 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2018-3960
Vancouver
Eguea JP, Catalano FM, Abdalla AM, Santana L de, Venner CH. Study on a camber adaptive winglet [Internet]. Proceedings. 2018 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2018-3960
Trabalho de evento
Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC (2018)
Serrano Rico, Juan Carlos; Amaral, Filipe Ramos do; Bresci, Christian Salaro; Beraldo, Matheus Maia; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC
Subjects: TÚNEIS DE VENTO, AEROACÚSTICA, ENGENHARIA AERONÁUTICA
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ABNT
SERRANO RICO, Juan Carlos et al. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC. 2018, Anais.. Reston, VA, USA: AIAA, 2018. Disponível em: https://doi.org/10.2514/6.2018-3960. Acesso em: 03 nov. 2024.
APA
Serrano Rico, J. C., Amaral, F. R. do, Bresci, C. S., Beraldo, M. M., & Medeiros, M. A. F. de. (2018). Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2018-3960
NLM
Serrano Rico JC, Amaral FR do, Bresci CS, Beraldo MM, Medeiros MAF de. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC [Internet]. Proceedings. 2018 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2018-3960
Vancouver
Serrano Rico JC, Amaral FR do, Bresci CS, Beraldo MM, Medeiros MAF de. Low acoustic noise and turbulence (LANT) wind-tunnel at USP-EESC [Internet]. Proceedings. 2018 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2018-3960
Trabalho de evento
An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack (2015)
Zakaria, Mohamed Y.; Pereira, Daniel Almeida; Ragab, Saad; Hajj, Muhammad R; Marques, Flavio Donizeti
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
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ABNT
ZAKARIA, Mohamed Y. et al. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack. 2015, Anais.. Reston, VA, USA: AIAA, 2015. Disponível em: https://doi.org/10.2514/6.2015-3166. Acesso em: 03 nov. 2024.
APA
Zakaria, M. Y., Pereira, D. A., Ragab, S., Hajj, M. R., & Marques, F. D. (2015). An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2015-3166
NLM
Zakaria MY, Pereira DA, Ragab S, Hajj MR, Marques FD. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack [Internet]. Proceedings. 2015 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2015-3166
Vancouver
Zakaria MY, Pereira DA, Ragab S, Hajj MR, Marques FD. An experimental study of added mass on a plunging airfoil oscillating with high frequencies at high angles of attack [Internet]. Proceedings. 2015 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2015-3166
Trabalho de evento
Methods for preliminary airfoil optimization (2009)
Entz, Ricardo Maiko Uehoka; Correa, Luiz Guilherme Noujain; Oliveira, Rafael Fernandes de; Catalano, Fernando Martini ; Medeiros, Marcello Augusto Faraco de
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, AEROFÓLIOS, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
ENTZ, Ricardo Maiko Uehoka et al. Methods for preliminary airfoil optimization. 2009, Anais.. Reston, VA, USA: AIAA, 2009. . Acesso em: 03 nov. 2024.
APA
Entz, R. M. U., Correa, L. G. N., Oliveira, R. F. de, Catalano, F. M., & Medeiros, M. A. F. de. (2009). Methods for preliminary airfoil optimization. In Proceedings. Reston, VA, USA: AIAA.
NLM
Entz RMU, Correa LGN, Oliveira RF de, Catalano FM, Medeiros MAF de. Methods for preliminary airfoil optimization. Proceedings. 2009 ;[citado 2024 nov. 03 ]
Vancouver
Entz RMU, Correa LGN, Oliveira RF de, Catalano FM, Medeiros MAF de. Methods for preliminary airfoil optimization. Proceedings. 2009 ;[citado 2024 nov. 03 ]
Trabalho de evento
Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow (2008)
Camilo, Elizangela; Marques, Flavio Donizeti
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CAMILO, Elizangela e MARQUES, Flavio Donizeti. Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow. 2008, Anais.. Reston, VA, USA: AIAA, 2008. Disponível em: https://doi.org/10.2514/6.2008-6236. Acesso em: 03 nov. 2024.
APA
Camilo, E., & Marques, F. D. (2008). Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2008-6236
NLM
Camilo E, Marques FD. Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow [Internet]. Proceedings. 2008 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2008-6236
Vancouver
Camilo E, Marques FD. Hopf bifurcation analysis of typical sections with structural nonlinearities in transonic flow [Internet]. Proceedings. 2008 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2008-6236
Trabalho de evento
Non-conventional control approach for intelligent structures (2001)
Marques, Flavio Donizeti ; Nagamine, Renato Kazuki
Source: Proceedings. Conference titles: AAIA Applied Aerodynamics Conference. Unidade: EESC
Subjects: ESTRUTURA DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, Flavio Donizeti e NAGAMINE, Renato Kazuki. Non-conventional control approach for intelligent structures. 2001, Anais.. Reston, VA, USA: AIAA, 2001. Disponível em: https://doi.org/10.2514/6.2001-1683. Acesso em: 03 nov. 2024.
APA
Marques, F. D., & Nagamine, R. K. (2001). Non-conventional control approach for intelligent structures. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2001-1683
NLM
Marques FD, Nagamine RK. Non-conventional control approach for intelligent structures [Internet]. Proceedings. 2001 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2001-1683
Vancouver
Marques FD, Nagamine RK. Non-conventional control approach for intelligent structures [Internet]. Proceedings. 2001 ;[citado 2024 nov. 03 ] Available from: https://doi.org/10.2514/6.2001-1683

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