On limit cycle oscillations of typical aeroelastic section with different preset angles of incidence at low airspeeds (2017)
- Authors:
- USP affiliated authors: MARQUES, FLAVIO DONIZETI - EESC ; SANTOS, CARLOS RENAN DOS - EESC
- Unidade: EESC
- DOI: 10.1016/j.jfluidstructs.2017.07.008
- Assunto: ENGENHARIA MECÂNICA
- Agências de fomento:
- Language: Inglês
- Imprenta:
- Publisher: Elsevier
- Publisher place: London, United Kingdom
- Date published: 2017
- Source:
- Título: Journal of Fluids and Structures
- ISSN: 0889-9746
- Volume/Número/Paginação/Ano: v. 74, p. 19-34, 2017
- Este periódico é de acesso aberto
- Este artigo NÃO é de acesso aberto
-
ABNT
SANTOS, Carlos Renan dos e PEREIRA, Daniel A. e MARQUES, Flavio Donizeti. On limit cycle oscillations of typical aeroelastic section with different preset angles of incidence at low airspeeds. Journal of Fluids and Structures, v. 74, p. 19-34, 2017Tradução . . Disponível em: https://doi.org/10.1016/j.jfluidstructs.2017.07.008. Acesso em: 26 fev. 2026. -
APA
Santos, C. R. dos, Pereira, D. A., & Marques, F. D. (2017). On limit cycle oscillations of typical aeroelastic section with different preset angles of incidence at low airspeeds. Journal of Fluids and Structures, 74, 19-34. doi:10.1016/j.jfluidstructs.2017.07.008 -
NLM
Santos CR dos, Pereira DA, Marques FD. On limit cycle oscillations of typical aeroelastic section with different preset angles of incidence at low airspeeds [Internet]. Journal of Fluids and Structures. 2017 ; 74 19-34.[citado 2026 fev. 26 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2017.07.008 -
Vancouver
Santos CR dos, Pereira DA, Marques FD. On limit cycle oscillations of typical aeroelastic section with different preset angles of incidence at low airspeeds [Internet]. Journal of Fluids and Structures. 2017 ; 74 19-34.[citado 2026 fev. 26 ] Available from: https://doi.org/10.1016/j.jfluidstructs.2017.07.008 - Stall-induced oscillations of typical aeroelastic sections in low airspeeds
- Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation
- Finite wing effects on the energy harvesting from stall-induced oscillations
- The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations
- Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils
- Lift prediction including stall, using vortex lattice method with Kirchhoff-Based correction
- Modeling and prediction of aerodynamic characteristics of free fall rotating wing based on experiments
- Structural nonlinearities influence on the energy harvesting from stall-induced oscillations
- Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime
- Optimization of energy harvesting from stall-induced oscillations using the multidimensional kriging metamodel
Informações sobre o DOI: 10.1016/j.jfluidstructs.2017.07.008 (Fonte: oaDOI API)
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