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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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 10 ago. 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 ago. 10 ] 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 ago. 10 ] 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
A citação é gerada automaticamente e pode não estar totalmente de acordo com as normas
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: 10 ago. 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 ago. 10 ] 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 ago. 10 ] Available from: http://dx.doi.org/10.1007/s00707-023-03736-7
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: 10 ago. 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 ago. 10 ] 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 ago. 10 ] Available from: https://doi.org/10.1016/j.ast.2019.04.031

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