Lift prediction including stall, using vortex lattice method with Kirchhoff-Based correction (2018)
- Authors:
- USP affiliated authors: MARQUES, FLAVIO DONIZETI - EESC ; SANTOS, CARLOS RENAN DOS - EESC
- Unidade: EESC
- DOI: 10.2514/1.C034451
- Subjects: DINÂMICA DE VOO; AERODINÂMICA DE AERONAVES; ENGENHARIA MECÂNICA
- Agências de fomento:
- Language: Inglês
- Imprenta:
- Publisher place: Reston, VA
- Date published: 2018
- Source:
- Título: Journal of Aircraft
- ISSN: 1533-3868
- Volume/Número/Paginação/Ano: v. 55, n. 2, p. 887-891, Mar./Apr. 2018
- Este periódico é de assinatura
- Este artigo NÃO é de acesso aberto
- Cor do Acesso Aberto: closed
-
ABNT
SANTOS, Carlos Renan dos e MARQUES, Flavio Donizeti. Lift prediction including stall, using vortex lattice method with Kirchhoff-Based correction. Journal of Aircraft, v. 55, n. 2, p. 887-891, 2018Tradução . . Disponível em: https://doi.org/10.2514/1.C034451. Acesso em: 10 jan. 2026. -
APA
Santos, C. R. dos, & Marques, F. D. (2018). Lift prediction including stall, using vortex lattice method with Kirchhoff-Based correction. Journal of Aircraft, 55( 2), 887-891. doi:10.2514/1.C034451 -
NLM
Santos CR dos, Marques FD. Lift prediction including stall, using vortex lattice method with Kirchhoff-Based correction [Internet]. Journal of Aircraft. 2018 ; 55( 2): 887-891.[citado 2026 jan. 10 ] Available from: https://doi.org/10.2514/1.C034451 -
Vancouver
Santos CR dos, Marques FD. Lift prediction including stall, using vortex lattice method with Kirchhoff-Based correction [Internet]. Journal of Aircraft. 2018 ; 55( 2): 887-891.[citado 2026 jan. 10 ] Available from: https://doi.org/10.2514/1.C034451 - Stall-induced oscillations of typical aeroelastic sections in low airspeeds
- 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
- Strucutral nonlinearitties effect on aeroelastic bifurcation phenomena in airfoils
- Energy harvesting from stall-induced oscillations of pitching airfoils at high-subsonic regime
- On limit cycle oscillations of typical aeroelastic section with different preset angles of incidence at low airspeeds
- The effects of structural and aerodynamic nonlinearities on the energy harvesting from airfoil stall-induced oscillations
- Onera-type corrections into the unsteady vortex lattice method for dynamic stall representation
- Finite wing effects on the energy harvesting from stall-induced oscillations
- Metamodel-based optimization of an energy harvester from stall-induced pitching oscillations of airfoils
Informações sobre o DOI: 10.2514/1.C034451 (Fonte: oaDOI API)
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