2011
DOI: 10.1063/1.3637914
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3D CFD Modeling and Simulation of NREL Phase VI Rotor

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Cited by 3 publications
(3 citation statements)
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“…The deviation at 9c downstream slightly increases at the AOA of 22°( Figure 16F). This is associated with the stall state of the blade section and the corresponding reduced accuracy of the CFD for high AOAs (Mahu et al, 2011). However, the VG parametric model is used to predict the aerodynamic characteristics of the blade in a non-stall state, and the accuracy loss of the model when the blade is in stall is acceptable.…”
Section: Boundary Layer Velocity Profilementioning
confidence: 99%
“…The deviation at 9c downstream slightly increases at the AOA of 22°( Figure 16F). This is associated with the stall state of the blade section and the corresponding reduced accuracy of the CFD for high AOAs (Mahu et al, 2011). However, the VG parametric model is used to predict the aerodynamic characteristics of the blade in a non-stall state, and the accuracy loss of the model when the blade is in stall is acceptable.…”
Section: Boundary Layer Velocity Profilementioning
confidence: 99%
“…A sliding interface is used in this paper and generally applied in literature, to address the effect of the full rotating wind turbine. The extensive measurements were studied by different computational researchers using a variety of computational methods and grid topologies [7,[13][14][15][16]. In recent years, many efforts have been directed towards raising the fidelity of numerical modeling in predicting the complex flow behavior around wind turbines.…”
Section: Introductionmentioning
confidence: 99%
“…3D CFD simulations of different wind turbines, e.g. conducted by Laursen et al [3] or Mahu et al [4], yield a fairly well suited performance prediction. However, they showed that using transition turbulence models seem to result in an overprediction of integral values like the generated torque at the hub.…”
Section: Introductionmentioning
confidence: 99%