Design and tests of an experimental flutter mount system (2004)
- Authors:
- USP affiliated authors: BELO, EDUARDO MORGADO - EESC ; TSUNAKI, ROBERTO HIDEAKI - EESC ; MARQUES, FLAVIO DONIZETI - EESC
- Unidade: EESC
- Subjects: AERODINÂMICA; AEROELASTICIDADE DE AERONAVES
- Language: Inglês
- Imprenta:
- Publisher: SEM
- Publisher place: Bethel, CT
- Date published: 2004
- Source:
- Título: Proceedings
- Conference titles: International Modal Analysis Conference - IMAC : a conference and exposition on structural dynamics
-
ABNT
DE MARQUI JÚNIOR, Carlos et al. Design and tests of an experimental flutter mount system. 2004, Anais.. Bethel, CT: SEM, 2004. . Acesso em: 18 fev. 2026. -
APA
De Marqui Júnior, C., Belo, E. M., Tsunaki, R. H., Rebolho, D. C., & Marques, F. D. (2004). Design and tests of an experimental flutter mount system. In Proceedings. Bethel, CT: SEM. -
NLM
De Marqui Júnior C, Belo EM, Tsunaki RH, Rebolho DC, Marques FD. Design and tests of an experimental flutter mount system. Proceedings. 2004 ;[citado 2026 fev. 18 ] -
Vancouver
De Marqui Júnior C, Belo EM, Tsunaki RH, Rebolho DC, Marques FD. Design and tests of an experimental flutter mount system. Proceedings. 2004 ;[citado 2026 fev. 18 ] - Variação do número de saídas no processo de identificação em tempo real
- Design of an experimental flutter mount system
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- Aplication of feedforward and recurrent neural networks for flapping and torsion identification of a helicopter blade
- Aeroelastic functional approximation via an artificial neural network reduced-order model
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