Near-tip correction functions for the actuator line method to improve the predicted lift and drag distributions
DOI10.1017/JFM.2024.461MaRDI QIDQ6585140
Grégoire S. Winckelmans, Guy Dumas, Thierry Villeneuve, Francois Trigaux
Publication date: 9 August 2024
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
SIMPLE algorithmReynolds-averaged Navier-Stokes simulationrectangular wingvortex lattice methodhorizontal axis wind turbinelifting line methodtapered wing
Incompressible viscous fluids (76D99) Finite volume methods applied to problems in fluid mechanics (76M12) General aerodynamics and subsonic flows (76G25) Vortex methods applied to problems in fluid mechanics (76M23)
Cites Work
- Low-speed aerodynamics.
- Investigation of eddy-viscosity models modified using discrete filters: A simplified “regularized variational multiscale model” and an “enhanced field model”
- A survey of modelling methods for high-fidelity wind farm simulations using large eddy simulation
- Filtered lifting line theory and application to the actuator line model
- Actuator curve embedding – an advanced actuator line model
- Non-iterative vortex-based smearing correction for the actuator line method
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