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Artigo de periodico
A review on bistable composite laminates for aerospace applications (2024)
Lemos, Diego Magela; Marques, Flavio Donizeti ; Ferreira, Antonio Joaquim Mendes
Source: Composite Structures. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS, LAMINADOS, ENGENHARIA MECÂNICA
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ABNT
LEMOS, Diego Magela e MARQUES, Flavio Donizeti e FERREIRA, Antonio Joaquim Mendes. A review on bistable composite laminates for aerospace applications. Composite Structures, v. 329, p. 1-21, 2024Tradução . . Disponível em: http://dx.doi.org/10.1016/j.compstruct.2023.117756. Acesso em: 19 abr. 2024.
APA
Lemos, D. M., Marques, F. D., & Ferreira, A. J. M. (2024). A review on bistable composite laminates for aerospace applications. Composite Structures, 329, 1-21. doi:10.1016/j.compstruct.2023.117756
NLM
Lemos DM, Marques FD, Ferreira AJM. A review on bistable composite laminates for aerospace applications [Internet]. Composite Structures. 2024 ; 329 1-21.[citado 2024 abr. 19 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117756
Vancouver
Lemos DM, Marques FD, Ferreira AJM. A review on bistable composite laminates for aerospace applications [Internet]. Composite Structures. 2024 ; 329 1-21.[citado 2024 abr. 19 ] Available from: http://dx.doi.org/10.1016/j.compstruct.2023.117756
Artigo de periodico
Real-time optimization of wing drag and lift performance using a movable leading edge (2024)
Camacho, Emanuel A. R.; Silva, Maíra Martins da ; Silva, Andre Resende Rodrigues; Marques, Flavio Donizeti
Source: Physics of Fluids. Unidade: EESC
Subjects: TEMPO-REAL, AERONAVES, ASAS DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
CAMACHO, Emanuel A. R. et al. Real-time optimization of wing drag and lift performance using a movable leading edge. Physics of Fluids, v. 36, n. 1, p. 1-11, 2024Tradução . . Disponível em: https://dx.doi.org/10.1063/5.0185716. Acesso em: 19 abr. 2024.
APA
Camacho, E. A. R., Silva, M. M. da, Silva, A. R. R., & Marques, F. D. (2024). Real-time optimization of wing drag and lift performance using a movable leading edge. Physics of Fluids, 36( 1), 1-11. doi:10.1063/5.0185716
NLM
Camacho EAR, Silva MM da, Silva ARR, Marques FD. Real-time optimization of wing drag and lift performance using a movable leading edge [Internet]. Physics of Fluids. 2024 ; 36( 1): 1-11.[citado 2024 abr. 19 ] Available from: https://dx.doi.org/10.1063/5.0185716
Vancouver
Camacho EAR, Silva MM da, Silva ARR, Marques FD. Real-time optimization of wing drag and lift performance using a movable leading edge [Internet]. Physics of Fluids. 2024 ; 36( 1): 1-11.[citado 2024 abr. 19 ] Available from: https://dx.doi.org/10.1063/5.0185716
Trabalho de evento-resumo
Influência de parâmetros geométricos em um sistema biestável (2023)
Correa, Renan Franco; Marques, Flavio Donizeti
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Assunto: ENGENHARIA MECÂNICA
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CORREA, Renan Franco e MARQUES, Flavio Donizeti. Influência de parâmetros geométricos em um sistema biestável. 2023, Anais.. São Carlos, SP: EESC-USP, 2023. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3758/2674. Acesso em: 19 abr. 2024.
APA
Correa, R. F., & Marques, F. D. (2023). Influência de parâmetros geométricos em um sistema biestável. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3758/2674
NLM
Correa RF, Marques FD. Influência de parâmetros geométricos em um sistema biestável [Internet]. Anais. 2023 ;[citado 2024 abr. 19 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3758/2674
Vancouver
Correa RF, Marques FD. Influência de parâmetros geométricos em um sistema biestável [Internet]. Anais. 2023 ;[citado 2024 abr. 19 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/viisipgem/paper/view/3758/2674
Artigo de periodico
Centimeter‑scale wind turbines design and analysis (2023)
Suzuki, Pedro Kaneto; Marques, Flavio Donizeti ; Pereira, Daniel A.
Source: Meccanica: An International Journal of Theoretical and Applied Mmechanics. Unidade: EESC
Subjects: ENERGIA EÓLICA, GERAÇÃO DE ENERGIA ELÉTRICA, ENGENHARIA MECÂNICA
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SUZUKI, Pedro Kaneto e MARQUES, Flavio Donizeti e PEREIRA, Daniel A. Centimeter‑scale wind turbines design and analysis. Meccanica: An International Journal of Theoretical and Applied Mmechanics, p. 1-15, 2023Tradução . . Disponível em: https://doi.org/10.1007/s11012-023-01652-7. Acesso em: 19 abr. 2024.
APA
Suzuki, P. K., Marques, F. D., & Pereira, D. A. (2023). Centimeter‑scale wind turbines design and analysis. Meccanica: An International Journal of Theoretical and Applied Mmechanics, 1-15. doi:10.1007/s11012-023-01652-7
NLM
Suzuki PK, Marques FD, Pereira DA. Centimeter‑scale wind turbines design and analysis [Internet]. Meccanica: An International Journal of Theoretical and Applied Mmechanics. 2023 ; 1-15.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1007/s11012-023-01652-7
Vancouver
Suzuki PK, Marques FD, Pereira DA. Centimeter‑scale wind turbines design and analysis [Internet]. Meccanica: An International Journal of Theoretical and Applied Mmechanics. 2023 ; 1-15.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1007/s11012-023-01652-7
Artigo de periodico
Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method (2023)
Camacho, Emanuel A. R; Marques, Flavio Donizeti ; Silva, Andre R. R
Source: Engineering Proceedings. Unidade: EESC
Subjects: AEROFÓLIOS, PROPULSÃO DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
CAMACHO, Emanuel A. R e MARQUES, Flavio Donizeti e SILVA, Andre R. R. Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method. Engineering Proceedings, v. 56, n. 1, p. 1-8, 2023Tradução . . Disponível em: https://dx.doi.org/10.3390/ASEC2023-15886. Acesso em: 19 abr. 2024.
APA
Camacho, E. A. R., Marques, F. D., & Silva, A. R. R. (2023). Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method. Engineering Proceedings, 56( 1), 1-8. doi:10.3390/ASEC2023-15886
NLM
Camacho EAR, Marques FD, Silva ARR. Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method [Internet]. Engineering Proceedings. 2023 ; 56( 1): 1-8.[citado 2024 abr. 19 ] Available from: https://dx.doi.org/10.3390/ASEC2023-15886
Vancouver
Camacho EAR, Marques FD, Silva ARR. Predicting the NACA0012-IK30 airfoil propulsive capabilities with a panel method [Internet]. Engineering Proceedings. 2023 ; 56( 1): 1-8.[citado 2024 abr. 19 ] Available from: https://dx.doi.org/10.3390/ASEC2023-15886
Artigo de periodico
Fast flapping aerodynamics prediction using a recurrent neural network (2023)
Pereira, João A. F.; Camacho, Emanuel A. R.; Marques, Flavio Donizeti ; Silva, Andre R. R
Source: Engineering Proceedings. Unidade: EESC
Subjects: PETRÓLEO, GASES, APRENDIZADO COMPUTACIONAL, AERODINÂMICA, REDES NEURAIS, ENGENHARIA MECÂNICA
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ABNT
PEREIRA, João A. F. et al. Fast flapping aerodynamics prediction using a recurrent neural network. Engineering Proceedings, v. 56, n. 1, p. 1-7, 2023Tradução . . Disponível em: https://dx.doi.org/10.3390/ASEC2023-16272. Acesso em: 19 abr. 2024.
APA
Pereira, J. A. F., Camacho, E. A. R., Marques, F. D., & Silva, A. R. R. (2023). Fast flapping aerodynamics prediction using a recurrent neural network. Engineering Proceedings, 56( 1), 1-7. doi:10.3390/ASEC2023-16272
NLM
Pereira JAF, Camacho EAR, Marques FD, Silva ARR. Fast flapping aerodynamics prediction using a recurrent neural network [Internet]. Engineering Proceedings. 2023 ; 56( 1): 1-7.[citado 2024 abr. 19 ] Available from: https://dx.doi.org/10.3390/ASEC2023-16272
Vancouver
Pereira JAF, Camacho EAR, Marques FD, Silva ARR. Fast flapping aerodynamics prediction using a recurrent neural network [Internet]. Engineering Proceedings. 2023 ; 56( 1): 1-7.[citado 2024 abr. 19 ] Available from: https://dx.doi.org/10.3390/ASEC2023-16272
Artigo de periodico
Dynamic characterization of an aeroelastic typical section under nonlinear energy sink passive control by using multiple scales and harmonic balance methods (2023)
Silva, Jose Augusto Ignácio da; Sanches, Leonardo; Marques, Flavio Donizeti
Source: Acta Mechanica. Unidade: EESC
Subjects: ENGENHARIA MECÂNICA, SISTEMAS DINÂMICOS, DISSIPADORES DE ENERGIA, AERONAVES, VIBRAÇÕES DE AERONAVES
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SILVA, Jose Augusto Ignácio da e SANCHES, Leonardo e MARQUES, Flavio Donizeti. Dynamic characterization of an aeroelastic typical section under nonlinear energy sink passive control by using multiple scales and harmonic balance methods. Acta Mechanica, p. 1-28, 2023Tradução . . Disponível em: https://doi.org/10.1007/s00707-022-03457-3. Acesso em: 19 abr. 2024.
APA
Silva, J. A. I. da, Sanches, L., & Marques, F. D. (2023). Dynamic characterization of an aeroelastic typical section under nonlinear energy sink passive control by using multiple scales and harmonic balance methods. Acta Mechanica, 1-28. doi:10.1007/s00707-022-03457-3
NLM
Silva JAI da, Sanches L, Marques FD. Dynamic characterization of an aeroelastic typical section under nonlinear energy sink passive control by using multiple scales and harmonic balance methods [Internet]. Acta Mechanica. 2023 ; 1-28.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1007/s00707-022-03457-3
Vancouver
Silva JAI da, Sanches L, Marques FD. Dynamic characterization of an aeroelastic typical section under nonlinear energy sink passive control by using multiple scales and harmonic balance methods [Internet]. Acta Mechanica. 2023 ; 1-28.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1007/s00707-022-03457-3
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: 19 abr. 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 abr. 19 ] 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 abr. 19 ] Available from: https://doi.org/10.3390/aerospace10070615
Artigo de periodico
An enhanced electromagnetic-based nonlinear energy sink for hybrid passive control and energy harvesting from resonant vibrations (2023)
Silva, Jose Augusto Ignácio da; Sanches, Leonardo; Michon, Guilhem; Marques, Flavio Donizeti
Source: Acta Mechanica. Unidade: EESC
Subjects: ENERGIA, DISSIPADORES DE ENERGIA, SISTEMAS DINÂMICOS, VIBRAÇÕES, ENGENHARIA MECÂNICA, SISTEMAS DINÂMICOS, DISSIPADORES DE ENERGIA, AERONAVES, VIBRAÇÕES DE AERONAVES
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ABNT
SILVA, Jose Augusto Ignácio da et al. An enhanced electromagnetic-based nonlinear energy sink for hybrid passive control and energy harvesting from resonant vibrations. Acta Mechanica, p. 1-22, 2023Tradução . . Disponível em: http://dx.doi.org/10.1007/s00707-023-03736-7. Acesso em: 19 abr. 2024.
APA
Silva, J. A. I. da, Sanches, L., Michon, G., & Marques, F. D. (2023). An enhanced electromagnetic-based nonlinear energy sink for hybrid passive control and energy harvesting from resonant vibrations. Acta Mechanica, 1-22. doi:10.1007/s00707-023-03736-7
NLM
Silva JAI da, Sanches L, Michon G, Marques FD. An enhanced electromagnetic-based nonlinear energy sink for hybrid passive control and energy harvesting from resonant vibrations [Internet]. Acta Mechanica. 2023 ; 1-22.[citado 2024 abr. 19 ] Available from: http://dx.doi.org/10.1007/s00707-023-03736-7
Vancouver
Silva JAI da, Sanches L, Michon G, Marques FD. An enhanced electromagnetic-based nonlinear energy sink for hybrid passive control and energy harvesting from resonant vibrations [Internet]. Acta Mechanica. 2023 ; 1-22.[citado 2024 abr. 19 ] Available from: http://dx.doi.org/10.1007/s00707-023-03736-7
Artigo de periodico
Energy harvesting from a rotational nonlinear energy sink in vortex-induced vibrations (2022)
Araujo, Gabriel P.; Silva, Jose Augusto Ignácio da; Marques, Flavio Donizeti
Source: Journal of Fluids and Structures. Unidade: EESC
Subjects: VÓRTICES DOS FLUÍDOS, VIBRAÇÕES, ENERGIA, ENGENHARIA MECÂNICA
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ABNT
ARAUJO, Gabriel P. e SILVA, Jose Augusto Ignácio da e MARQUES, Flavio Donizeti. Energy harvesting from a rotational nonlinear energy sink in vortex-induced vibrations. Journal of Fluids and Structures, v. 113, p. 1-18, 2022Tradução . . Disponível em: https://doi.org/10.1016/j.jfluidstructs.2022.103656. Acesso em: 19 abr. 2024.
APA
Araujo, G. P., Silva, J. A. I. da, & Marques, F. D. (2022). Energy harvesting from a rotational nonlinear energy sink in vortex-induced vibrations. Journal of Fluids and Structures, 113, 1-18. doi:10.1016/j.jfluidstructs.2022.103656
NLM
Araujo GP, Silva JAI da, Marques FD. Energy harvesting from a rotational nonlinear energy sink in vortex-induced vibrations [Internet]. Journal of Fluids and Structures. 2022 ; 113 1-18.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2022.103656
Vancouver
Araujo GP, Silva JAI da, Marques FD. Energy harvesting from a rotational nonlinear energy sink in vortex-induced vibrations [Internet]. Journal of Fluids and Structures. 2022 ; 113 1-18.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2022.103656
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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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: 19 abr. 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 abr. 19 ] 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 abr. 19 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
Artigo de periodico
Geometrically nonlinear study of functionally graded saturated porous plates based on refined shear deformation plate theory and biot's theory (2022)
Kumar, H. S. Naveen; Kattimani, Subhaschandra; Marques, Flavio Donizeti ; Thoi, T. Nguyen; Shariati, Mehdi
Source: International Journal of Structural Stability and Dynamics. Unidade: EESC
Subjects: CISALHAMENTO, PLACAS, ANÁLISE NÃO LINEAR DE ESTRUTURAS, ENGENHARIA MECÂNICA
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ABNT
KUMAR, H. S. Naveen et al. Geometrically nonlinear study of functionally graded saturated porous plates based on refined shear deformation plate theory and biot's theory. International Journal of Structural Stability and Dynamics, p. 1-28, 2022Tradução . . Disponível em: https://doi.org/10.1142/S021945542350013X. Acesso em: 19 abr. 2024.
APA
Kumar, H. S. N., Kattimani, S., Marques, F. D., Thoi, T. N., & Shariati, M. (2022). Geometrically nonlinear study of functionally graded saturated porous plates based on refined shear deformation plate theory and biot's theory. International Journal of Structural Stability and Dynamics, 1-28. doi:10.1142/S021945542350013X
NLM
Kumar HSN, Kattimani S, Marques FD, Thoi TN, Shariati M. Geometrically nonlinear study of functionally graded saturated porous plates based on refined shear deformation plate theory and biot's theory [Internet]. International Journal of Structural Stability and Dynamics. 2022 ; 1-28.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1142/S021945542350013X
Vancouver
Kumar HSN, Kattimani S, Marques FD, Thoi TN, Shariati M. Geometrically nonlinear study of functionally graded saturated porous plates based on refined shear deformation plate theory and biot's theory [Internet]. International Journal of Structural Stability and Dynamics. 2022 ; 1-28.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1142/S021945542350013X
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: 19 abr. 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 abr. 19 ] 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 abr. 19 ] Available from: https://doi.org/10.1016/j.ijnonlinmec.2022.104100
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: 19 abr. 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 abr. 19 ] 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 abr. 19 ] Available from: https://doi.org/10.1177/10775463221089732
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: 19 abr. 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 abr. 19 ] 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 abr. 19 ] Available from: https://doi.org/10.1115/1.4050792
Artigo de periodico
Improvements on the Beddoes–Leishman dynamic stall model for low speed applications (2021)
Santos, Luiz Guilherme Pancini dos; Marques, Flavio Donizeti
Source: Journal of Fluids and Structures. Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, VÓRTICES DOS FLUÍDOS, ENERGIA, ENGENHARIA MECÂNICA
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ABNT
SANTOS, Luiz Guilherme Pancini dos e MARQUES, Flavio Donizeti. Improvements on the Beddoes–Leishman dynamic stall model for low speed applications. Journal of Fluids and Structures, v. 106, p. 1-29, 2021Tradução . . Disponível em: https://doi.org/10.1016/j.jfluidstructs.2022.103656. Acesso em: 19 abr. 2024.
APA
Santos, L. G. P. dos, & Marques, F. D. (2021). Improvements on the Beddoes–Leishman dynamic stall model for low speed applications. Journal of Fluids and Structures, 106, 1-29. doi:10.1016/j.jfluidstructs.2022.103656
NLM
Santos LGP dos, Marques FD. Improvements on the Beddoes–Leishman dynamic stall model for low speed applications [Internet]. Journal of Fluids and Structures. 2021 ; 106 1-29.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2022.103656
Vancouver
Santos LGP dos, Marques FD. Improvements on the Beddoes–Leishman dynamic stall model for low speed applications [Internet]. Journal of Fluids and Structures. 2021 ; 106 1-29.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2022.103656
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: 19 abr. 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 abr. 19 ] 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 abr. 19 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/vsipgem/paper/view/3163/2280
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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 19 abr. 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 abr. 19 ] 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 abr. 19 ] Available from: https://doi.org/10.1177/10775463211000161
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: 19 abr. 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 abr. 19 ] 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 abr. 19 ] Available from: https://doi.org/10.1016/j.tws.2020.107379
Artigo de periodico
Experimental analysis of passive bio-inspired covert feathers for stall and post-stall performance enhancement (2021)
Diaz Izquierdo, David Orlando; Marques, Flavio Donizeti
Source: Meccanica: An International Journal of Theoretical and Applied Mmechanics. Unidade: EESC
Subjects: AERODINÂMICA DE AERONAVES, TÚNEIS DE VENTO, AERONAVES NÃO TRIPULADAS, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
DIAZ IZQUIERDO, David Orlando e MARQUES, Flavio Donizeti. Experimental analysis of passive bio-inspired covert feathers for stall and post-stall performance enhancement. Meccanica: An International Journal of Theoretical and Applied Mmechanics, p. 1-19, 2021Tradução . . Disponível em: https://doi.org/10.1007/s11012-021-01409-0. Acesso em: 19 abr. 2024.
APA
Diaz Izquierdo, D. O., & Marques, F. D. (2021). Experimental analysis of passive bio-inspired covert feathers for stall and post-stall performance enhancement. Meccanica: An International Journal of Theoretical and Applied Mmechanics, 1-19. doi:10.1007/s11012-021-01409-0
NLM
Diaz Izquierdo DO, Marques FD. Experimental analysis of passive bio-inspired covert feathers for stall and post-stall performance enhancement [Internet]. Meccanica: An International Journal of Theoretical and Applied Mmechanics. 2021 ; 1-19.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1007/s11012-021-01409-0
Vancouver
Diaz Izquierdo DO, Marques FD. Experimental analysis of passive bio-inspired covert feathers for stall and post-stall performance enhancement [Internet]. Meccanica: An International Journal of Theoretical and Applied Mmechanics. 2021 ; 1-19.[citado 2024 abr. 19 ] Available from: https://doi.org/10.1007/s11012-021-01409-0

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