2018
DOI: 10.1002/we.2225
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Vortex simulations of wind turbines operating in atmospheric conditions using a prescribed velocity‐vorticity boundary layer model

Abstract: A prescribed velocity-vorticity boundary layer model for the vorticity transport equation is proposed, which corrects the unphysical upward deflection of the wake seen in a simpler prescribed velocity shear approach. A Lagrangian implementation of the boundary layer model has been investigated using our in-house vortex solver MIRAS. The MIRAS code contains both an aerodynamic part and a structural-mechanical part taking into account aeroelastic phenomena. The solver is employed to simulate flows around wind tu… Show more

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Cited by 19 publications
(31 citation statements)
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“…The Navier-Stokes equations are solved using the SIMPLE algorithm (Patankar and Spalding, 1972), and the convective terms are discretized using a QUICK scheme (Leonard, 1979). The wind turbine rotors are represented by actuator discs (ADs) based on airfoil data as presented in Réthoré et al (2014). The RANS-AD model can only model stiff blades.…”
Section: Ellipsys3d Rans-admentioning
confidence: 99%
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“…The Navier-Stokes equations are solved using the SIMPLE algorithm (Patankar and Spalding, 1972), and the convective terms are discretized using a QUICK scheme (Leonard, 1979). The wind turbine rotors are represented by actuator discs (ADs) based on airfoil data as presented in Réthoré et al (2014). The RANS-AD model can only model stiff blades.…”
Section: Ellipsys3d Rans-admentioning
confidence: 99%
“…In order to do so, a simplification of the 4R-V29 wind turbine is used so that a fair comparison with a equivalent single-rotor wind turbine can be made. The simplified 4R-V29 wind turbine has a zero toe-out angle, and the force distributions are defined by prescribed normalized blade force distributions (calculated by Réthoré et al, 2014, employing a detached eddy simulation of the NREL-5MW rotor for a wind speed of 8 m s −1 ). The blade force distributions are scaled by the hub height velocity U H , R, C T , C P and the rotational speed (RPM) as discussed by van der Laan et al (2015).…”
Section: Wake Recovery Of the 4r-v29 Wind Turbinementioning
confidence: 99%
“…The in‐house vortex code MIRAS, 17‐19,26 that is, Method for Interactive Rotor Aerodynamic Simulations, has been used in the current work. MIRAS is a multi‐fidelity aerodynamic tool for wind turbine performance analyses.…”
Section: Methodsmentioning
confidence: 99%
“…The VIPM being the most physically correct approach, since it resolves the actual geometry of the blade and accounts for the viscous effects enclosed inside the boundary layer. Regarding the flow/wake models implemented in MIRAS, they range from the classic free‐wake using filaments, 17 the hybrid filament‐mesh 18 which keeps the filament structure of the wake, to the hybrid filament‐particle‐mesh 19 . The hybrid filament‐particle‐mesh being regarded as the highest order since it resolves the vorticity equation, which is obtained by taking the curl of the Navier‐Stokes equation, and describes the evolution of the vorticity of a fluid particle as it moves with the flow.…”
Section: Introductionmentioning
confidence: 99%
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