2022
DOI: 10.1088/1742-6596/2265/3/032019
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Stall flutter instabilities on the IEA-15 reference wind turbine in idling conditions: code-to-code comparisons and physical analyses

Abstract: The present study investigates stall-induced vibrations on a IEA-15-RWT wind turbine blade. At standstill and under specific strong crosswind conditions, simulations using the codes OpenFAST and DeepLines WindTM exhibit large-amplitude vibrations. Results of both codes are first compared, showing an overall good agreement. Then, the influence of the wind misalignment angle is assessed as well as the choice of aerodynamic polar datasets. Vibrations are observed within two well-marked angular sectors, and the hi… Show more

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Cited by 3 publications
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“…Aerodynamic loads in such conditions (i.e., in deep stall) can be accurately estimated using engineering tools that rely on tabulated airfoil data (i.e., the so-called polars), only if a valid dynamic stall model is employed. Nevertheless, the uncertainty in the prediction of the aerodynamic loads in dynamic stall is a well-known fact within the wind energy sector [3][4][5] and it is the main cause of the consequent uncertainty in the prediction of the stall-induced edgewise vibrations. Different state-of-the-art dynamic stall models (e.g., Beddoes-Leishman [6] and ONERA [7]) can give significantly different load results in the onset of dynamic stall due to the quite different aerodynamic damping predicted by the stall models.…”
Section: Introductionmentioning
confidence: 99%
“…Aerodynamic loads in such conditions (i.e., in deep stall) can be accurately estimated using engineering tools that rely on tabulated airfoil data (i.e., the so-called polars), only if a valid dynamic stall model is employed. Nevertheless, the uncertainty in the prediction of the aerodynamic loads in dynamic stall is a well-known fact within the wind energy sector [3][4][5] and it is the main cause of the consequent uncertainty in the prediction of the stall-induced edgewise vibrations. Different state-of-the-art dynamic stall models (e.g., Beddoes-Leishman [6] and ONERA [7]) can give significantly different load results in the onset of dynamic stall due to the quite different aerodynamic damping predicted by the stall models.…”
Section: Introductionmentioning
confidence: 99%