2014
DOI: 10.1016/j.jfluidstructs.2014.06.029
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Aeroelastic analysis of wind turbines using a tightly coupled CFD–CSD method

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Cited by 46 publications
(25 citation statements)
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“…HMB3 solves the Navier-Stokes equations in integral form using the arbitrary Lagrangian-Eulerian formulation for time-dependent domains with moving boundaries (Dehaeze and Barakos 2012a, b;Carrión et al 2014a). The solver uses a cell-centred finite volume approach combined with an implicit dual-time method (Jameson 1991).…”
Section: Methodsmentioning
confidence: 99%
“…HMB3 solves the Navier-Stokes equations in integral form using the arbitrary Lagrangian-Eulerian formulation for time-dependent domains with moving boundaries (Dehaeze and Barakos 2012a, b;Carrión et al 2014a). The solver uses a cell-centred finite volume approach combined with an implicit dual-time method (Jameson 1991).…”
Section: Methodsmentioning
confidence: 99%
“…To validate the current result, the modal frequency of a 62.7 m long blade from [28] is plotted with it. The two blades have similar aerofoil distributions [15,28], with some differences such as pre-bended blade in [6] but pre-coned blade in [15] and a 1.2 m length difference. Assessing Figure 8 and the modal frequencies for each mode, the frequencies of the FE model and LMH64-5 blade are closer for the 1st, 2nd and 4th mode but a significant difference is seen in the third mode, i.e., the 2nd flapwise mode.…”
Section: Fe Modelmentioning
confidence: 99%
“…Wang et al [3] established an FSI model using CFD and FEA with one-way coupling interface between them. Carrión et al [4] applied a CFD-CSD method to perform aeroelastic analysis on NREL and MEXICO wind turbines where flapwise and edgewise instabilities were studied. Recently, Heinz et al [5] conducted a high-fedility study on the blade of the reference wind turbine DTU 10 MW to investigate the aeroelastic response in deep stall conditions using HAWC2CFD tool [6].…”
Section: Introductionmentioning
confidence: 99%