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Vortex Shedding Lock-In due to Pitching Oscillation of a Wind Turbine Blade Section at High Angles of Attack

The unsteady flow around a pitching two-dimensional airfoil section (NREL S809) has been simulated using unsteady RANS with the transition SST turbulence model. This geometry is chosen to represent a wind turbine blade in a standstill configuration. The Reynolds number is Re=106 based on a chord len...

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Bibliografiset tiedot
Päätekijät: Craig Meskell, Alberto Pellegrino
Aineistotyyppi: Artigo
Kieli:Inglês
Julkaistu: Wiley 2019-01-01
Sarja:International Journal of Aerospace Engineering
Linkit:http://dx.doi.org/10.1155/2019/6919505
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