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Artigo de periodico
Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil (2023)
Parra, Hector G.; Cerón Muñoz, Hernán Darío ; Gomez, William; Gaona, Elvis E.
Source: Energies. Unidade: EESC
Subjects: TURBINAS, VIBRAÇÕES DE AERONAVES, TÚNEIS DE VENTO, ENGENHARIA AERONÁUTICA
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ABNT
PARRA, Hector G. et al. Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil. Energies, v. 16, n. 12, p. 1-22, 2023Tradução . . Disponível em: https://doi.org/10.3390/en16124538. Acesso em: 27 abr. 2024.
APA
Parra, H. G., Cerón Muñoz, H. D., Gomez, W., & Gaona, E. E. (2023). Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil. Energies, 16( 12), 1-22. doi:10.3390/en16124538
NLM
Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil [Internet]. Energies. 2023 ; 16( 12): 1-22.[citado 2024 abr. 27 ] Available from: https://doi.org/10.3390/en16124538
Vancouver
Parra HG, Cerón Muñoz HD, Gomez W, Gaona EE. Experimental analysis of bio-inspired vortex generators on a blade with S822 airfoil [Internet]. Energies. 2023 ; 16( 12): 1-22.[citado 2024 abr. 27 ] Available from: https://doi.org/10.3390/en16124538
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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ABNT
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: 27 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. 27 ] 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. 27 ] Available from: https://doi.org/10.1007/s00707-022-03457-3
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: 27 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. 27 ] 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. 27 ] Available from: http://dx.doi.org/10.1007/s00707-023-03736-7
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: 27 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. 27 ] 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. 27 ] Available from: https://doi.org/10.1016/j.compstruct.2021.115128
Trabalho de evento-anais periodico
Effects of negative capacitance circuits on the vibration attenuation performance of a nonlinear piezoelectric metamaterial (2022)
Mosquera Sánchez, Jaime Alberto; Ootani, Nicholas K; De Marqui Júnior, Carlos
Source: Proceedings of SPIE. Conference titles: Active and Passive Smart Structures and Integrated Systems. Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, PIEZOELETRICIDADE, ENGENHARIA AERONÁUTICA
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ABNT
MOSQUERA SÁNCHEZ, Jaime Alberto e OOTANI, Nicholas K e DE MARQUI JÚNIOR, Carlos. Effects of negative capacitance circuits on the vibration attenuation performance of a nonlinear piezoelectric metamaterial. Proceedings of SPIE. Bellingham: SPIE. Disponível em: https://doi.org/10.1117/12.2612553. Acesso em: 27 abr. 2024. , 2022
APA
Mosquera Sánchez, J. A., Ootani, N. K., & De Marqui Júnior, C. (2022). Effects of negative capacitance circuits on the vibration attenuation performance of a nonlinear piezoelectric metamaterial. Proceedings of SPIE. Bellingham: SPIE. doi:10.1117/12.2612553
NLM
Mosquera Sánchez JA, Ootani NK, De Marqui Júnior C. Effects of negative capacitance circuits on the vibration attenuation performance of a nonlinear piezoelectric metamaterial [Internet]. Proceedings of SPIE. 2022 ; 12043 1-12.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1117/12.2612553
Vancouver
Mosquera Sánchez JA, Ootani NK, De Marqui Júnior C. Effects of negative capacitance circuits on the vibration attenuation performance of a nonlinear piezoelectric metamaterial [Internet]. Proceedings of SPIE. 2022 ; 12043 1-12.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1117/12.2612553
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: 27 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. 27 ] 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. 27 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2022.103656
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
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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: 27 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. 27 ] 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. 27 ] Available from: https://doi.org/10.1016/j.tws.2020.107379
Artigo de periodico
Nonlinear energy sink to enhance the landing gear shimmy performance (2021)
Sanches, Leonardo ; Guimarães, Thiago A. M; Marques, Flavio Donizeti
Source: Acta Mechanica. Unidade: EESC
Subjects: ATERRISSAGEM, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA
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ABNT
SANCHES, Leonardo e GUIMARÃES, Thiago A. M e MARQUES, Flavio Donizeti. Nonlinear energy sink to enhance the landing gear shimmy performance. Acta Mechanica, v. 232, p. 2605-2622, 2021Tradução . . Disponível em: https://doi.org/10.1007/s00707-021-02985-8. Acesso em: 27 abr. 2024.
APA
Sanches, L., Guimarães, T. A. M., & Marques, F. D. (2021). Nonlinear energy sink to enhance the landing gear shimmy performance. Acta Mechanica, 232, 2605-2622. doi:10.1007/s00707-021-02985-8
NLM
Sanches L, Guimarães TAM, Marques FD. Nonlinear energy sink to enhance the landing gear shimmy performance [Internet]. Acta Mechanica. 2021 ; 232 2605-2622.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1007/s00707-021-02985-8
Vancouver
Sanches L, Guimarães TAM, Marques FD. Nonlinear energy sink to enhance the landing gear shimmy performance [Internet]. Acta Mechanica. 2021 ; 232 2605-2622.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1007/s00707-021-02985-8
Artigo de periodico
Effect of parametric uncertainties on vibration mitigation with periodically distributed and interconnected piezoelectric patches (2020)
Trindade, Marcelo Areias; Lossouarn, Boris; Deü, Jean-François
Source: Journal of Intelligent Material Systems and Structures. Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, PIEZOELETRICIDADE, ENGENHARIA AERONÁUTICA
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ABNT
TRINDADE, Marcelo Areias e LOSSOUARN, Boris e DEÜ, Jean-François. Effect of parametric uncertainties on vibration mitigation with periodically distributed and interconnected piezoelectric patches. Journal of Intelligent Material Systems and Structures, p. 1-15, 2020Tradução . . Disponível em: https://doi.org/10.1177/1045389X20942847. Acesso em: 27 abr. 2024.
APA
Trindade, M. A., Lossouarn, B., & Deü, J. -F. (2020). Effect of parametric uncertainties on vibration mitigation with periodically distributed and interconnected piezoelectric patches. Journal of Intelligent Material Systems and Structures, 1-15. doi:10.1177/1045389X20942847
NLM
Trindade MA, Lossouarn B, Deü J-F. Effect of parametric uncertainties on vibration mitigation with periodically distributed and interconnected piezoelectric patches [Internet]. Journal of Intelligent Material Systems and Structures. 2020 ; 1-15.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1177/1045389X20942847
Vancouver
Trindade MA, Lossouarn B, Deü J-F. Effect of parametric uncertainties on vibration mitigation with periodically distributed and interconnected piezoelectric patches [Internet]. Journal of Intelligent Material Systems and Structures. 2020 ; 1-15.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1177/1045389X20942847
Artigo de periodico
On the modeling of nonlinear supersonic flutter of multibay composite panels (2020)
Guimarães, Thiago A. M.; Marques, Flavio Donizeti ; Ferreira, Antonio J. M
Source: Composite Structures. Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, MATERIAIS COMPÓSITOS, PAINÉIS, ESTRUTURAS
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ABNT
GUIMARÃES, Thiago A. M. e MARQUES, Flavio Donizeti e FERREIRA, Antonio J. M. On the modeling of nonlinear supersonic flutter of multibay composite panels. Composite Structures, v. 232, n. Ja 2020, p. 1-6, 2020Tradução . . Disponível em: https://doi.org/10.1016/j.compstruct.2019.111522. Acesso em: 27 abr. 2024.
APA
Guimarães, T. A. M., Marques, F. D., & Ferreira, A. J. M. (2020). On the modeling of nonlinear supersonic flutter of multibay composite panels. Composite Structures, 232( Ja 2020), 1-6. doi:10.1016/j.compstruct.2019.111522
NLM
Guimarães TAM, Marques FD, Ferreira AJM. On the modeling of nonlinear supersonic flutter of multibay composite panels [Internet]. Composite Structures. 2020 ; 232( Ja 2020): 1-6.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1016/j.compstruct.2019.111522
Vancouver
Guimarães TAM, Marques FD, Ferreira AJM. On the modeling of nonlinear supersonic flutter of multibay composite panels [Internet]. Composite Structures. 2020 ; 232( Ja 2020): 1-6.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1016/j.compstruct.2019.111522
Dissertação (Mestrado)
Effects of piezoelectric based nonlinear energy sink on the aeroelastic behavior of a typical section (2020)
Otsubo, Gabriela Mayumi de Freitas; Marqui Junior, Carlos de (Orientador)
Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, AEROELASTICIDADE DE AERONAVES, PIEZOELETRICIDADE
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ABNT
OTSUBO, Gabriela Mayumi de Freitas. Effects of piezoelectric based nonlinear energy sink on the aeroelastic behavior of a typical section. 2020. Dissertação (Mestrado) – Universidade de São Paulo, São Carlos, 2020. Disponível em: https://www.teses.usp.br/teses/disponiveis/18/18161/tde-14092020-115737/. Acesso em: 27 abr. 2024.
APA
Otsubo, G. M. de F. (2020). Effects of piezoelectric based nonlinear energy sink on the aeroelastic behavior of a typical section (Dissertação (Mestrado). Universidade de São Paulo, São Carlos. Recuperado de https://www.teses.usp.br/teses/disponiveis/18/18161/tde-14092020-115737/
NLM
Otsubo GM de F. Effects of piezoelectric based nonlinear energy sink on the aeroelastic behavior of a typical section [Internet]. 2020 ;[citado 2024 abr. 27 ] Available from: https://www.teses.usp.br/teses/disponiveis/18/18161/tde-14092020-115737/
Vancouver
Otsubo GM de F. Effects of piezoelectric based nonlinear energy sink on the aeroelastic behavior of a typical section [Internet]. 2020 ;[citado 2024 abr. 27 ] Available from: https://www.teses.usp.br/teses/disponiveis/18/18161/tde-14092020-115737/
Artigo de periodico
Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers (2020)
Beli, Danilo; Ruzzene, Massimo; De Marqui Júnior, Carlos
Source: Physical Review Applied. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, PIEZOELETRICIDADE, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
BELI, Danilo e RUZZENE, Massimo e DE MARQUI JÚNIOR, Carlos. Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers. Physical Review Applied, v. 14, p. 1-14, 2020Tradução . . Disponível em: https://doi.org/10.1103/PhysRevApplied.14.034032. Acesso em: 27 abr. 2024.
APA
Beli, D., Ruzzene, M., & De Marqui Júnior, C. (2020). Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers. Physical Review Applied, 14, 1-14. doi:10.1103/PhysRevApplied.14.034032
NLM
Beli D, Ruzzene M, De Marqui Júnior C. Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers [Internet]. Physical Review Applied. 2020 ; 14 1-14.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1103/PhysRevApplied.14.034032
Vancouver
Beli D, Ruzzene M, De Marqui Júnior C. Bridging-coupling phenomenon in linear elastic metamaterials by exploiting locally resonant metachain isomers [Internet]. Physical Review Applied. 2020 ; 14 1-14.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1103/PhysRevApplied.14.034032
Tese (Doutorado)
Design and experimental verification of a smart piezoelectric pitch link for vibration attenuation (2019)
Clementino, Marcel Araujo; De Marqui Junior, Carlos (Orientador); Niztsche, Fred (coorient)
Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, PIEZOELETRICIDADE, HELICÓPTEROS
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ABNT
CLEMENTINO, Marcel Araujo. Design and experimental verification of a smart piezoelectric pitch link for vibration attenuation. 2019. Tese (Doutorado) – Universidade de São Paulo, São Carlos, 2019. . Acesso em: 27 abr. 2024.
APA
Clementino, M. A. (2019). Design and experimental verification of a smart piezoelectric pitch link for vibration attenuation (Tese (Doutorado). Universidade de São Paulo, São Carlos.
NLM
Clementino MA. Design and experimental verification of a smart piezoelectric pitch link for vibration attenuation. 2019 ;[citado 2024 abr. 27 ]
Vancouver
Clementino MA. Design and experimental verification of a smart piezoelectric pitch link for vibration attenuation. 2019 ;[citado 2024 abr. 27 ]
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
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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: 27 abr. 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 abr. 27 ] 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 abr. 27 ] Available from: https://doi.org/10.2514/6.2020-0941
Tese (Doutorado)
Elastic and aeroelastic behavior of electromechanical coupled structures in cases of energy harvesting and structural control considering piezoelectric nonlinearities. (2019)
Dias, José Augusto de Carvalho; De Marqui Júnior, Carlos (Orientador)
Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, AEROELASTICIDADE DE AERONAVES
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ABNT
DIAS, José Augusto de Carvalho. Elastic and aeroelastic behavior of electromechanical coupled structures in cases of energy harvesting and structural control considering piezoelectric nonlinearities. 2019. Tese (Doutorado) – Universidade de São Paulo, São Carlos, 2019. Disponível em: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-21102019-093851/. Acesso em: 27 abr. 2024.
APA
Dias, J. A. de C. (2019). Elastic and aeroelastic behavior of electromechanical coupled structures in cases of energy harvesting and structural control considering piezoelectric nonlinearities. (Tese (Doutorado). Universidade de São Paulo, São Carlos. Recuperado de http://www.teses.usp.br/teses/disponiveis/18/18148/tde-21102019-093851/
NLM
Dias JA de C. Elastic and aeroelastic behavior of electromechanical coupled structures in cases of energy harvesting and structural control considering piezoelectric nonlinearities. [Internet]. 2019 ;[citado 2024 abr. 27 ] Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-21102019-093851/
Vancouver
Dias JA de C. Elastic and aeroelastic behavior of electromechanical coupled structures in cases of energy harvesting and structural control considering piezoelectric nonlinearities. [Internet]. 2019 ;[citado 2024 abr. 27 ] Available from: http://www.teses.usp.br/teses/disponiveis/18/18148/tde-21102019-093851/
Trabalho de evento
Active control of band gaps on a smart phononic beam (2019)
Dourado, Massao Kodama; Gonçalves, Paulo José Paupitz; De Marqui Júnior, Carlos ; Beli, Danilo
Conference titles: ABCM International Congress of Mechanical Engineering - COBEM. Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA
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ABNT
DOURADO, Massao Kodama et al. Active control of band gaps on a smart phononic beam. 2019, Anais.. Rio de Janeiro, RJ: ABCM, 2019. Disponível em: https://repositorio.usp.br/directbitstream/65c1d900-ef07-4607-ac17-bd9f440aa9a3/trabalho%2001%20-%20ACTIVE%20CONTROL%20OF%20BAND%20GAPS%20ON%20A%20SMART%20BEAM%20%28cobem%202019%29_removed.pdf. Acesso em: 27 abr. 2024.
APA
Dourado, M. K., Gonçalves, P. J. P., De Marqui Júnior, C., & Beli, D. (2019). Active control of band gaps on a smart phononic beam. In . Rio de Janeiro, RJ: ABCM. Recuperado de https://repositorio.usp.br/directbitstream/65c1d900-ef07-4607-ac17-bd9f440aa9a3/trabalho%2001%20-%20ACTIVE%20CONTROL%20OF%20BAND%20GAPS%20ON%20A%20SMART%20BEAM%20%28cobem%202019%29_removed.pdf
NLM
Dourado MK, Gonçalves PJP, De Marqui Júnior C, Beli D. Active control of band gaps on a smart phononic beam [Internet]. 2019 ;[citado 2024 abr. 27 ] Available from: https://repositorio.usp.br/directbitstream/65c1d900-ef07-4607-ac17-bd9f440aa9a3/trabalho%2001%20-%20ACTIVE%20CONTROL%20OF%20BAND%20GAPS%20ON%20A%20SMART%20BEAM%20%28cobem%202019%29_removed.pdf
Vancouver
Dourado MK, Gonçalves PJP, De Marqui Júnior C, Beli D. Active control of band gaps on a smart phononic beam [Internet]. 2019 ;[citado 2024 abr. 27 ] Available from: https://repositorio.usp.br/directbitstream/65c1d900-ef07-4607-ac17-bd9f440aa9a3/trabalho%2001%20-%20ACTIVE%20CONTROL%20OF%20BAND%20GAPS%20ON%20A%20SMART%20BEAM%20%28cobem%202019%29_removed.pdf
Artigo de periodico
Dynamic assessment of nonlinear typical section aeroviscoelastic systems using fractional derivative-based viscoelastic model (2018)
Sales, Thiago P.; Marques, Flavio Donizeti ; Pereira, Daniel A.; Rade, Domingos Alves
Source: Journal of Sound and Vibration. Unidade: EESC
Subjects: VIBRAÇÕES DE AERONAVES, AERODINÂMICA DE AERONAVES, VISCOELASTICIDADE DAS ESTRUTURAS, 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. Dynamic assessment of nonlinear typical section aeroviscoelastic systems using fractional derivative-based viscoelastic model. Journal of Sound and Vibration, v. 423, p. 230-245, 2018Tradução . . Disponível em: https://doi.org/10.1016/j.jsv.2018.02.008. Acesso em: 27 abr. 2024.
APA
Sales, T. P., Marques, F. D., Pereira, D. A., & Rade, D. A. (2018). Dynamic assessment of nonlinear typical section aeroviscoelastic systems using fractional derivative-based viscoelastic model. Journal of Sound and Vibration, 423, 230-245. doi:10.1016/j.jsv.2018.02.008
NLM
Sales TP, Marques FD, Pereira DA, Rade DA. Dynamic assessment of nonlinear typical section aeroviscoelastic systems using fractional derivative-based viscoelastic model [Internet]. Journal of Sound and Vibration. 2018 ; 423 230-245.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1016/j.jsv.2018.02.008
Vancouver
Sales TP, Marques FD, Pereira DA, Rade DA. Dynamic assessment of nonlinear typical section aeroviscoelastic systems using fractional derivative-based viscoelastic model [Internet]. Journal of Sound and Vibration. 2018 ; 423 230-245.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1016/j.jsv.2018.02.008
Artigo de periodico
Structural health monitoring for impact damaged composite: a new methodology based on a combination of techniques (2018)
Medeiros, Ricardo de; Vandepitte, Dirk; Tita, Volnei
Source: Structural Health Monitoring. Unidade: EESC
Subjects: MATERIAIS COMPÓSITOS DE FIBRAS, INTEGRIDADE ESTRUTURAL, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
MEDEIROS, Ricardo de e VANDEPITTE, Dirk e TITA, Volnei. Structural health monitoring for impact damaged composite: a new methodology based on a combination of techniques. Structural Health Monitoring, v. 17, n. Ja 2018, p. 185-200, 2018Tradução . . Disponível em: https://doi.org/10.1177/1475921716688442. Acesso em: 27 abr. 2024.
APA
Medeiros, R. de, Vandepitte, D., & Tita, V. (2018). Structural health monitoring for impact damaged composite: a new methodology based on a combination of techniques. Structural Health Monitoring, 17( Ja 2018), 185-200. doi:10.1177/1475921716688442
NLM
Medeiros R de, Vandepitte D, Tita V. Structural health monitoring for impact damaged composite: a new methodology based on a combination of techniques [Internet]. Structural Health Monitoring. 2018 ; 17( Ja 2018): 185-200.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1177/1475921716688442
Vancouver
Medeiros R de, Vandepitte D, Tita V. Structural health monitoring for impact damaged composite: a new methodology based on a combination of techniques [Internet]. Structural Health Monitoring. 2018 ; 17( Ja 2018): 185-200.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1177/1475921716688442
Artigo de periodico
Experimental study on the aeroelastic behavior of a typical airfoil section with superelastic shape memory alloy springs (2018)
Sousa, Vagner Candido de; De Marqui Júnior, Carlos
Source: Journal of Intelligent Material Systems and Structures. Unidade: EESC
Subjects: AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA AERONÁUTICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
SOUSA, Vagner Candido de e DE MARQUI JÚNIOR, Carlos. Experimental study on the aeroelastic behavior of a typical airfoil section with superelastic shape memory alloy springs. Journal of Intelligent Material Systems and Structures, v. 29, n. 4, p. 623-635, 2018Tradução . . Disponível em: https://doi.org/10.1177/1045389X17721024. Acesso em: 27 abr. 2024.
APA
Sousa, V. C. de, & De Marqui Júnior, C. (2018). Experimental study on the aeroelastic behavior of a typical airfoil section with superelastic shape memory alloy springs. Journal of Intelligent Material Systems and Structures, 29( 4), 623-635. doi:10.1177/1045389X17721024
NLM
Sousa VC de, De Marqui Júnior C. Experimental study on the aeroelastic behavior of a typical airfoil section with superelastic shape memory alloy springs [Internet]. Journal of Intelligent Material Systems and Structures. 2018 ; 29( 4): 623-635.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1177/1045389X17721024
Vancouver
Sousa VC de, De Marqui Júnior C. Experimental study on the aeroelastic behavior of a typical airfoil section with superelastic shape memory alloy springs [Internet]. Journal of Intelligent Material Systems and Structures. 2018 ; 29( 4): 623-635.[citado 2024 abr. 27 ] Available from: https://doi.org/10.1177/1045389X17721024
Trabalho de evento
Efeito de absorvedores peizoelétricos de vibração não-lineares sobre o comportamento aeroelástico de uma seção típica (2018)
Otsubo, Gabriela Mayumi de Freitas; De Marqui Júnior, Carlos
Source: Anais. Conference titles: Simpósio do Programa de Pós-Graduação em Engenharia Mecânica - SIPGEM. Unidade: EESC
Subjects: PIEZOELETRICIDADE, AEROELASTICIDADE DE AERONAVES, VIBRAÇÕES DE AERONAVES, ENGENHARIA MECÂNICA
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
ABNT
OTSUBO, Gabriela Mayumi de Freitas e DE MARQUI JÚNIOR, Carlos. Efeito de absorvedores peizoelétricos de vibração não-lineares sobre o comportamento aeroelástico de uma seção típica. 2018, Anais.. São Carlos, SP: EESC-USP, 2018. Disponível em: http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1359/820. Acesso em: 27 abr. 2024.
APA
Otsubo, G. M. de F., & De Marqui Júnior, C. (2018). Efeito de absorvedores peizoelétricos de vibração não-lineares sobre o comportamento aeroelástico de uma seção típica. In Anais. São Carlos, SP: EESC-USP. Recuperado de http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1359/820
NLM
Otsubo GM de F, De Marqui Júnior C. Efeito de absorvedores peizoelétricos de vibração não-lineares sobre o comportamento aeroelástico de uma seção típica [Internet]. Anais. 2018 ;[citado 2024 abr. 27 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1359/820
Vancouver
Otsubo GM de F, De Marqui Júnior C. Efeito de absorvedores peizoelétricos de vibração não-lineares sobre o comportamento aeroelástico de uma seção típica [Internet]. Anais. 2018 ;[citado 2024 abr. 27 ] Available from: http://soac.eesc.usp.br/index.php/SiPGEM/iiisipgem/paper/view/1359/820

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