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Artigo de periodico
Passive flutter mitigation with rotary nonlinear energy sink (2024)
Araujo, Gabriel Placeres; Silva, Jose Augusto Ignácio da; Marques, Flavio Donizeti
Source: Nonlinear Dynamics. Unidade: EESC
Subjects: DISSIPADORES DE ENERGIA, AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
ARAUJO, Gabriel Placeres e SILVA, Jose Augusto Ignácio da e MARQUES, Flavio Donizeti. Passive flutter mitigation with rotary nonlinear energy sink. Nonlinear Dynamics, p. 1-19, 2024Tradução . . Disponível em: http://dx.doi.org/10.1007/s11071-024-09515-w. Acesso em: 18 nov. 2024.
APA
Araujo, G. P., Silva, J. A. I. da, & Marques, F. D. (2024). Passive flutter mitigation with rotary nonlinear energy sink. Nonlinear Dynamics, 1-19. doi:10.1007/s11071-024-09515-w
NLM
Araujo GP, Silva JAI da, Marques FD. Passive flutter mitigation with rotary nonlinear energy sink [Internet]. Nonlinear Dynamics. 2024 ; 1-19.[citado 2024 nov. 18 ] Available from: http://dx.doi.org/10.1007/s11071-024-09515-w
Vancouver
Araujo GP, Silva JAI da, Marques FD. Passive flutter mitigation with rotary nonlinear energy sink [Internet]. Nonlinear Dynamics. 2024 ; 1-19.[citado 2024 nov. 18 ] Available from: http://dx.doi.org/10.1007/s11071-024-09515-w
Artigo de periodico
Influence of a deflectable leading-edge on a flapping airfoil (2023)
Camacho, Emanuel A. R.; Marques, Flavio Donizeti ; Silva, Andre R. R.
Source: Aerospace. Unidade: EESC
Subjects: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, FLAPS, ENGENHARIA MECÂNICA
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ABNT
CAMACHO, Emanuel A. R. e MARQUES, Flavio Donizeti e SILVA, Andre R. R. Influence of a deflectable leading-edge on a flapping airfoil. Aerospace, v. 10, n. 7, p. 1-17, 2023Tradução . . Disponível em: https://doi.org/10.3390/aerospace10070615. Acesso em: 18 nov. 2024.
APA
Camacho, E. A. R., Marques, F. D., & Silva, A. R. R. (2023). Influence of a deflectable leading-edge on a flapping airfoil. Aerospace, 10( 7), 1-17. doi:10.3390/aerospace10070615
NLM
Camacho EAR, Marques FD, Silva ARR. Influence of a deflectable leading-edge on a flapping airfoil [Internet]. Aerospace. 2023 ; 10( 7): 1-17.[citado 2024 nov. 18 ] Available from: https://doi.org/10.3390/aerospace10070615
Vancouver
Camacho EAR, Marques FD, Silva ARR. Influence of a deflectable leading-edge on a flapping airfoil [Internet]. Aerospace. 2023 ; 10( 7): 1-17.[citado 2024 nov. 18 ] Available from: https://doi.org/10.3390/aerospace10070615
Artigo de periodico
Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels (2022)
Cabral, Myrella Vieira; Marques, Flavio Donizeti ; Ferreira, Antonio J. M
Source: Composite Structures. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, ENGENHARIA MECÂNICA
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ABNT
CABRAL, Myrella Vieira e MARQUES, Flavio Donizeti e FERREIRA, Antonio J. M. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels. Composite Structures, v. 286, p. 1-15, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2021.115128. Acesso em: 18 nov. 2024.
APA
Cabral, M. V., Marques, F. D., & Ferreira, A. J. M. (2022). Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels. Composite Structures, 286, 1-15. doi:10.1016/j.compstruct.2021.115128
NLM
Cabral MV, Marques FD, Ferreira AJM. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels [Internet]. Composite Structures. 2022 ; 286 1-15.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
Vancouver
Cabral MV, Marques FD, Ferreira AJM. Nonlinear supersonic post-flutter response of two-bay composite laminate curved panels [Internet]. Composite Structures. 2022 ; 286 1-15.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
Artigo de periodico
Aeroelastic analysis and nonlinear characterization of three-degree-of-freedom systems with discontinuous nonlinearities (2022)
Vasconcellos, Rui; Bouma, A.; Marques, Flavio Donizeti ; Abdelkefi, A; Hajj, Muhammad R
Source: International Journal of Non-Linear Mechanics. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
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ABNT
VASCONCELLOS, Rui et al. Aeroelastic analysis and nonlinear characterization of three-degree-of-freedom systems with discontinuous nonlinearities. International Journal of Non-Linear Mechanics, v. 145, p. 1-19, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.ijnonlinmec.2022.104100. Acesso em: 18 nov. 2024.
APA
Vasconcellos, R., Bouma, A., Marques, F. D., Abdelkefi, A., & Hajj, M. R. (2022). Aeroelastic analysis and nonlinear characterization of three-degree-of-freedom systems with discontinuous nonlinearities. International Journal of Non-Linear Mechanics, 145, 1-19. doi:10.1016/j.ijnonlinmec.2022.104100
NLM
Vasconcellos R, Bouma A, Marques FD, Abdelkefi A, Hajj MR. Aeroelastic analysis and nonlinear characterization of three-degree-of-freedom systems with discontinuous nonlinearities [Internet]. International Journal of Non-Linear Mechanics. 2022 ; 145 1-19.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2022.104100
Vancouver
Vasconcellos R, Bouma A, Marques FD, Abdelkefi A, Hajj MR. Aeroelastic analysis and nonlinear characterization of three-degree-of-freedom systems with discontinuous nonlinearities [Internet]. International Journal of Non-Linear Mechanics. 2022 ; 145 1-19.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2022.104100
Artigo de periodico
Influence of bistable plunge stiffness on nonlinear airfoil flutter (2021)
Correa, Renan F; Marques, Flavio Donizeti
Source: Journal of Computational and Nonlinear Dynamics. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
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ABNT
CORREA, Renan F e MARQUES, Flavio Donizeti. Influence of bistable plunge stiffness on nonlinear airfoil flutter. Journal of Computational and Nonlinear Dynamics, v. 16, p. 1-14, 2021Tradução . . Disponível em: https://doi.org/10.1115/1.4050792. Acesso em: 18 nov. 2024.
APA
Correa, R. F., & Marques, F. D. (2021). Influence of bistable plunge stiffness on nonlinear airfoil flutter. Journal of Computational and Nonlinear Dynamics, 16, 1-14. doi:10.1115/1.4050792
NLM
Correa RF, Marques FD. Influence of bistable plunge stiffness on nonlinear airfoil flutter [Internet]. Journal of Computational and Nonlinear Dynamics. 2021 ; 16 1-14.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1115/1.4050792
Vancouver
Correa RF, Marques FD. Influence of bistable plunge stiffness on nonlinear airfoil flutter [Internet]. Journal of Computational and Nonlinear Dynamics. 2021 ; 16 1-14.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1115/1.4050792
Trabalho de evento
Dynamic behavior of stall fluttering airfoils (2021)
Santos, Luiz Guilherme Pancini dos; Marques, Flavio Donizeti
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: AEROFÓLIOS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SANTOS, Luiz Guilherme Pancini dos e MARQUES, Flavio Donizeti. Dynamic behavior of stall fluttering airfoils. 2021, Anais.. São Carlos, SP: EESC-USP, 2021. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/vsipgem/paper/view/3163/2280. Acesso em: 18 nov. 2024.
APA
Santos, L. G. P. dos, & Marques, F. D. (2021). Dynamic behavior of stall fluttering airfoils. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/vsipgem/paper/view/3163/2280
NLM
Santos LGP dos, Marques FD. Dynamic behavior of stall fluttering airfoils [Internet]. Anais. 2021 ;[citado 2024 nov. 18 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/vsipgem/paper/view/3163/2280
Vancouver
Santos LGP dos, Marques FD. Dynamic behavior of stall fluttering airfoils [Internet]. Anais. 2021 ;[citado 2024 nov. 18 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/vsipgem/paper/view/3163/2280
Artigo de periodico
The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays (2021)
Cabral, Myrella V.; Marques, Flavio Donizeti ; Ferreira, António J. M.
Source: Thin-Walled Structures. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, MÉTODO DOS ELEMENTOS FINITOS, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
CABRAL, Myrella V. e MARQUES, Flavio Donizeti e FERREIRA, António J. M. The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays. Thin-Walled Structures, v. 161, p. 1-12, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.tws.2020.107379. Acesso em: 18 nov. 2024.
APA
Cabral, M. V., Marques, F. D., & Ferreira, A. J. M. (2021). The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays. Thin-Walled Structures, 161, 1-12. doi:10.1016/j.tws.2020.107379
NLM
Cabral MV, Marques FD, Ferreira AJM. The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays [Internet]. Thin-Walled Structures. 2021 ; 161 1-12.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.tws.2020.107379
Vancouver
Cabral MV, Marques FD, Ferreira AJM. The effect of curvature in nonlinear supersonic flutter of panels with adjacent bays [Internet]. Thin-Walled Structures. 2021 ; 161 1-12.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.tws.2020.107379
Artigo de periodico
Characterization of typical aeroelastic sections under combined structural concentrated nonlinearities (2021)
Silva, Jose Augusto Ignácio da; Marques, Flavio Donizeti
Source: Journal of Vibration and Control. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, ENGENHARIA MECÂNICA
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ABNT
SILVA, Jose Augusto Ignácio da e MARQUES, Flavio Donizeti. Characterization of typical aeroelastic sections under combined structural concentrated nonlinearities. Journal of Vibration and Control, p. 1-15, 2021Tradução . . Disponível em: https://doi.org/10.1177/10775463211000161. Acesso em: 18 nov. 2024.
APA
Silva, J. A. I. da, & Marques, F. D. (2021). Characterization of typical aeroelastic sections under combined structural concentrated nonlinearities. Journal of Vibration and Control, 1-15. doi:10.1177/10775463211000161
NLM
Silva JAI da, Marques FD. Characterization of typical aeroelastic sections under combined structural concentrated nonlinearities [Internet]. Journal of Vibration and Control. 2021 ; 1-15.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1177/10775463211000161
Vancouver
Silva JAI da, Marques FD. Characterization of typical aeroelastic sections under combined structural concentrated nonlinearities [Internet]. Journal of Vibration and Control. 2021 ; 1-15.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1177/10775463211000161
Trabalho de evento-resumo
Controle passivo de vibrações aeroelásticas empregando nonlinear energy sinks (2021)
Ribeiro, Adolfo Esteves; Marques, Flavio Donizeti
Source: Livro de Resumos Expandidos. Conference titles: Simpósio Internacional de Iniciação Científica e Tecnológica da Universidade de São Paulo - SIICUSP. Unidade: EESC
Subjects: VIBRAÇÕES, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
RIBEIRO, Adolfo Esteves e MARQUES, Flavio Donizeti. Controle passivo de vibrações aeroelásticas empregando nonlinear energy sinks. 2021, Anais.. São Carlos, SP: EESC/USP, 2021. Disponível em: http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3262/2068. Acesso em: 18 nov. 2024.
APA
Ribeiro, A. E., & Marques, F. D. (2021). Controle passivo de vibrações aeroelásticas empregando nonlinear energy sinks. In Livro de Resumos Expandidos. São Carlos, SP: EESC/USP. Recuperado de http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3262/2068
NLM
Ribeiro AE, Marques FD. Controle passivo de vibrações aeroelásticas empregando nonlinear energy sinks [Internet]. Livro de Resumos Expandidos. 2021 ;[citado 2024 nov. 18 ] Available from: http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3262/2068
Vancouver
Ribeiro AE, Marques FD. Controle passivo de vibrações aeroelásticas empregando nonlinear energy sinks [Internet]. Livro de Resumos Expandidos. 2021 ;[citado 2024 nov. 18 ] Available from: http://soac.eesc.usp.br/index.php/siicusp/29siicusp/paper/viewFile/3262/2068
Artigo de periodico
Nonlinear aeroelastic analysis of airfoil section under stall flutter oscillations and gust loads (2021)
Santos, Luiz Guilherme Pancini dos; Marques, Flavio Donizeti
Source: Journal of Fluids and Structures. Unidade: EESC
Subjects: TURBULÊNCIA ATMOSFÉRICA, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
SANTOS, Luiz Guilherme Pancini dos e MARQUES, Flavio Donizeti. Nonlinear aeroelastic analysis of airfoil section under stall flutter oscillations and gust loads. Journal of Fluids and Structures, v. 102, p. 1-20, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.jfluidstructs.2021.103250. Acesso em: 18 nov. 2024.
APA
Santos, L. G. P. dos, & Marques, F. D. (2021). Nonlinear aeroelastic analysis of airfoil section under stall flutter oscillations and gust loads. Journal of Fluids and Structures, 102, 1-20. doi:10.1016/j.jfluidstructs.2021.103250
NLM
Santos LGP dos, Marques FD. Nonlinear aeroelastic analysis of airfoil section under stall flutter oscillations and gust loads [Internet]. Journal of Fluids and Structures. 2021 ; 102 1-20.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2021.103250
Vancouver
Santos LGP dos, Marques FD. Nonlinear aeroelastic analysis of airfoil section under stall flutter oscillations and gust loads [Internet]. Journal of Fluids and Structures. 2021 ; 102 1-20.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2021.103250
Artigo de periodico
Nonlinear supersonic post-flutter motion of panels with adjacent bays and thermal effects (2020)
Guimarães, Thiago A. M; Sanches, Leonardo; Marques, Flavio Donizeti
Source: International Journal of Non-Linear Mechanics. Unidade: EESC
Subjects: ESTRUTURA DE AERONAVES, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
GUIMARÃES, Thiago A. M e SANCHES, Leonardo e MARQUES, Flavio Donizeti. Nonlinear supersonic post-flutter motion of panels with adjacent bays and thermal effects. International Journal of Non-Linear Mechanics, v. 125, p. 1-13, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.ijnonlinmec.2020.103545. Acesso em: 18 nov. 2024.
APA
Guimarães, T. A. M., Sanches, L., & Marques, F. D. (2020). Nonlinear supersonic post-flutter motion of panels with adjacent bays and thermal effects. International Journal of Non-Linear Mechanics, 125, 1-13. doi:10.1016/j.ijnonlinmec.2020.103545
NLM
Guimarães TAM, Sanches L, Marques FD. Nonlinear supersonic post-flutter motion of panels with adjacent bays and thermal effects [Internet]. International Journal of Non-Linear Mechanics. 2020 ; 125 1-13.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2020.103545
Vancouver
Guimarães TAM, Sanches L, Marques FD. Nonlinear supersonic post-flutter motion of panels with adjacent bays and thermal effects [Internet]. International Journal of Non-Linear Mechanics. 2020 ; 125 1-13.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2020.103545
Trabalho de evento
Review paper on composite panel flutter (2019)
Najafi, Maliheh; Marques, Flavio Donizeti
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, MATERIAIS COMPÓSITOS, ENGENHARIA MECÂNICA
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ABNT
NAJAFI, Maliheh e MARQUES, Flavio Donizeti. Review paper on composite panel flutter. 2019, Anais.. São Carlos, SP: EESC-USP, 2019. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1826/1030. Acesso em: 18 nov. 2024.
APA
Najafi, M., & Marques, F. D. (2019). Review paper on composite panel flutter. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1826/1030
NLM
Najafi M, Marques FD. Review paper on composite panel flutter [Internet]. Anais. 2019 ;[citado 2024 nov. 18 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1826/1030
Vancouver
Najafi M, Marques FD. Review paper on composite panel flutter [Internet]. Anais. 2019 ;[citado 2024 nov. 18 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/ivsipgem/paper/view/1826/1030
Trabalho de evento
Nonlinear dynamics of fluttering multibay panels in supersonic regime (2019)
Marques, Flavio Donizeti ; Ferreira, A. J. M.
Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: EESC
Subjects: PAINÉIS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MARQUES, Flavio Donizeti e FERREIRA, A. J. M. Nonlinear dynamics of fluttering multibay panels in supersonic regime. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2019-1867. Acesso em: 18 nov. 2024.
APA
Marques, F. D., & Ferreira, A. J. M. (2019). Nonlinear dynamics of fluttering multibay panels in supersonic regime. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2019-1867
NLM
Marques FD, Ferreira AJM. Nonlinear dynamics of fluttering multibay panels in supersonic regime [Internet]. Proceedings. 2019 ;[citado 2024 nov. 18 ] Available from: https://doi.org/10.2514/6.2019-1867
Vancouver
Marques FD, Ferreira AJM. Nonlinear dynamics of fluttering multibay panels in supersonic regime [Internet]. Proceedings. 2019 ;[citado 2024 nov. 18 ] Available from: https://doi.org/10.2514/6.2019-1867
Artigo de periodico
Multi-variable Volterra kernels identification using time-delay neural networks: application to unsteady aerodynamic loading (2019)
Paula, Natália Cristina Gomes de; Marques, Flavio Donizeti
Source: Nonlinear Dynamics. Unidade: EESC
Subjects: REDES NEURAIS, AERODINÂMICA DE AERONAVES, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PAULA, Natália Cristina Gomes de e MARQUES, Flavio Donizeti. Multi-variable Volterra kernels identification using time-delay neural networks: application to unsteady aerodynamic loading. Nonlinear Dynamics, v. 97, p. 767-780, 2019Tradução . . Disponível em: https://doi.org/10.1007/s11071-019-05011-8. Acesso em: 18 nov. 2024.
APA
Paula, N. C. G. de, & Marques, F. D. (2019). Multi-variable Volterra kernels identification using time-delay neural networks: application to unsteady aerodynamic loading. Nonlinear Dynamics, 97, 767-780. doi:10.1007/s11071-019-05011-8
NLM
Paula NCG de, Marques FD. Multi-variable Volterra kernels identification using time-delay neural networks: application to unsteady aerodynamic loading [Internet]. Nonlinear Dynamics. 2019 ; 97 767-780.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1007/s11071-019-05011-8
Vancouver
Paula NCG de, Marques FD. Multi-variable Volterra kernels identification using time-delay neural networks: application to unsteady aerodynamic loading [Internet]. Nonlinear Dynamics. 2019 ; 97 767-780.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1007/s11071-019-05011-8
Artigo de periodico
The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations (2019)
Santos, Carlos Renan dos ; Marques, Flavio Donizeti ; Hajj, Muhammad R
Source: Journal of Vibration and Control. Unidade: EESC
Subjects: ENERGIA ELÉTRICA, AEROELASTICIDADE DE AERONAVES, AEROFÓLIOS, PIEZOELETRICIDADE, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti e HAJJ, Muhammad R. The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations. Journal of Vibration and Control, v. 25, n. 14, p. 1991-2007, 2019Tradução . . Disponível em: https://doi.org/10.1177/1077546319844383. Acesso em: 18 nov. 2024.
APA
Santos, C. R. dos, Marques, F. D., & Hajj, M. R. (2019). The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations. Journal of Vibration and Control, 25( 14), 1991-2007. doi:10.1177/1077546319844383
NLM
Santos CR dos, Marques FD, Hajj MR. The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations [Internet]. Journal of Vibration and Control. 2019 ; 25( 14): 1991-2007.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1177/1077546319844383
Vancouver
Santos CR dos, Marques FD, Hajj MR. The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations [Internet]. Journal of Vibration and Control. 2019 ; 25( 14): 1991-2007.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1177/1077546319844383
Trabalho de evento
Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers (2019)
Guimarães, Thiago A. M.; Rade, Domingos A.; Cesnik, Carlos E. S.; Marques, Flavio Donizeti
Source: Proceedings. Conference titles: AIAA Scitech Forum. Unidade: EESC
Subjects: ENGENHARIA MECÂNICA, VIBRAÇÕES DE AERONAVES, AEROELASTICIDADE DE AERONAVES, PAINÉIS
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
GUIMARÃES, Thiago A. M. et al. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers. 2019, Anais.. Reston, VA, USA: AIAA, 2019. Disponível em: https://doi.org/10.2514/6.2020-0941. Acesso em: 18 nov. 2024.
APA
Guimarães, T. A. M., Rade, D. A., Cesnik, C. E. S., & Marques, F. D. (2019). Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers. In Proceedings. Reston, VA, USA: AIAA. doi:10.2514/6.2020-0941
NLM
Guimarães TAM, Rade DA, Cesnik CES, Marques FD. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers [Internet]. Proceedings. 2019 ;[citado 2024 nov. 18 ] Available from: https://doi.org/10.2514/6.2020-0941
Vancouver
Guimarães TAM, Rade DA, Cesnik CES, Marques FD. Nonlinear multibay panel flutter evaluation of composite laminates with curvilinear fibers [Internet]. Proceedings. 2019 ;[citado 2024 nov. 18 ] Available from: https://doi.org/10.2514/6.2020-0941
Artigo de periodico
Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs (2019)
Sanches, Leonardo ; Guimarães, Thiago A. M; Marques, Flavio Donizeti
Source: Aerospace Science and Technology. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SANCHES, Leonardo e GUIMARÃES, Thiago A. M e MARQUES, Flavio Donizeti. Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs. Aerospace Science and Technology, v. 90, p. 157-168, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.ast.2019.04.031. Acesso em: 18 nov. 2024.
APA
Sanches, L., Guimarães, T. A. M., & Marques, F. D. (2019). Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs. Aerospace Science and Technology, 90, 157-168. doi:10.1016/j.ast.2019.04.031
NLM
Sanches L, Guimarães TAM, Marques FD. Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs [Internet]. Aerospace Science and Technology. 2019 ; 90 157-168.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.ast.2019.04.031
Vancouver
Sanches L, Guimarães TAM, Marques FD. Aeroelastic tailoring of nonlinear typical section using the method of multiple scales to predict post-flutter stable LCOs [Internet]. Aerospace Science and Technology. 2019 ; 90 157-168.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.ast.2019.04.031
Artigo de periodico
Modeling and dynamic characterization of nonlinear non-smooth aeroviscoelastic systems (2019)
Sales, Thiago P; Pereira, Daniel A.; Marques, Flavio Donizeti ; Rade, Domingos Alves
Source: Mechanical Systems and Signal Processing. Unidade: EESC
Subjects: ALGORITMOS, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SALES, Thiago P et al. Modeling and dynamic characterization of nonlinear non-smooth aeroviscoelastic systems. Mechanical Systems and Signal Processing, v. 116, p. 900-915, 2019Tradução . . Disponível em: https://doi.org/10.1016/j.ymssp.2018.07.003. Acesso em: 18 nov. 2024.
APA
Sales, T. P., Pereira, D. A., Marques, F. D., & Rade, D. A. (2019). Modeling and dynamic characterization of nonlinear non-smooth aeroviscoelastic systems. Mechanical Systems and Signal Processing, 116, 900-915. doi:10.1016/j.ymssp.2018.07.003
NLM
Sales TP, Pereira DA, Marques FD, Rade DA. Modeling and dynamic characterization of nonlinear non-smooth aeroviscoelastic systems [Internet]. Mechanical Systems and Signal Processing. 2019 ; 116 900-915.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.ymssp.2018.07.003
Vancouver
Sales TP, Pereira DA, Marques FD, Rade DA. Modeling and dynamic characterization of nonlinear non-smooth aeroviscoelastic systems [Internet]. Mechanical Systems and Signal Processing. 2019 ; 116 900-915.[citado 2024 nov. 18 ] Available from: https://doi.org/10.1016/j.ymssp.2018.07.003
Trabalho de evento
Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation (2019)
Santos, Carlos Renan dos; Marques, Flavio Donizeti ; Taha, H. E.
Source: Proceedings. Conference titles: International Forum on Aeroelasticity and Structural Dynamics - IFASD. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, TRELIÇAS, ASAS DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti e TAHA, H. E. Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation. 2019, Anais.. Savannah, Georgia, USA: IFASD, 2019. Disponível em: https://repositorio.usp.br/directbitstream/4b87ed66-354d-4ea3-9407-b13430122efb/IFASD-2019-039.pdf. Acesso em: 18 nov. 2024.
APA
Santos, C. R. dos, Marques, F. D., & Taha, H. E. (2019). Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation. In Proceedings. Savannah, Georgia, USA: IFASD. Recuperado de https://repositorio.usp.br/directbitstream/4b87ed66-354d-4ea3-9407-b13430122efb/IFASD-2019-039.pdf
NLM
Santos CR dos, Marques FD, Taha HE. Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation [Internet]. Proceedings. 2019 ;[citado 2024 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/4b87ed66-354d-4ea3-9407-b13430122efb/IFASD-2019-039.pdf
Vancouver
Santos CR dos, Marques FD, Taha HE. Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation [Internet]. Proceedings. 2019 ;[citado 2024 nov. 18 ] Available from: https://repositorio.usp.br/directbitstream/4b87ed66-354d-4ea3-9407-b13430122efb/IFASD-2019-039.pdf
Artigo de periodico
Volterra kernels assessment via time-delay neural networks for nonlinear unsteady aerodynamic loading identification (2019)
Paula, Natália Cristina Gomes de; Marques, Flavio Donizeti ; Silva, Walter A.
Source: AIAA Journal. Unidade: EESC
Subjects: MÉTODO DOS ELEMENTOS FINITOS, POLÍMEROS (MATERIAIS), MATERIAIS COMPÓSITOS DE FIBRAS, FLAMBAGEM, CULTURA ORGANIZACIONAL, ADMINISTRAÇÃO ESTRATÉGICA, SETOR PÚBLICO, ADMINISTRAÇÃO DA EDUCAÇÃO, REVISÃO SISTEMÁTICA, AERODINÂMICA DE AERONAVES, SISTEMAS NÃO LINEARES, AEROELASTICIDADE DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
PAULA, Natália Cristina Gomes de e MARQUES, Flavio Donizeti e SILVA, Walter A. Volterra kernels assessment via time-delay neural networks for nonlinear unsteady aerodynamic loading identification. AIAA Journal, v. 57, n. 4, p. 1725-1735, 2019Tradução . . Disponível em: https://doi.org/10.2514/1.J057229. Acesso em: 18 nov. 2024.
APA
Paula, N. C. G. de, Marques, F. D., & Silva, W. A. (2019). Volterra kernels assessment via time-delay neural networks for nonlinear unsteady aerodynamic loading identification. AIAA Journal, 57( 4), 1725-1735. doi:10.2514/1.J057229
NLM
Paula NCG de, Marques FD, Silva WA. Volterra kernels assessment via time-delay neural networks for nonlinear unsteady aerodynamic loading identification [Internet]. AIAA Journal. 2019 ; 57( 4): 1725-1735.[citado 2024 nov. 18 ] Available from: https://doi.org/10.2514/1.J057229
Vancouver
Paula NCG de, Marques FD, Silva WA. Volterra kernels assessment via time-delay neural networks for nonlinear unsteady aerodynamic loading identification [Internet]. AIAA Journal. 2019 ; 57( 4): 1725-1735.[citado 2024 nov. 18 ] Available from: https://doi.org/10.2514/1.J057229

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