2012
DOI: 10.1016/j.egypro.2012.06.122
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Wake Modeling with the Actuator Disc Concept

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Cited by 50 publications
(27 citation statements)
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“…The associated pressure drop ( ) ∆p is calculated from a semi-empirical relation between the thrust coefficient curve and the velocity at the disc. While these simulations provide a good estimate for the far wake velocity profiles, the flow behavior in front of the AD and in the near wake is not captured accurately [12]. The discrepancies between computed velocity profiles and real measurements may be attributed to the way the∆p is distributed over several cells.…”
Section: Introductionmentioning
confidence: 98%
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“…The associated pressure drop ( ) ∆p is calculated from a semi-empirical relation between the thrust coefficient curve and the velocity at the disc. While these simulations provide a good estimate for the far wake velocity profiles, the flow behavior in front of the AD and in the near wake is not captured accurately [12]. The discrepancies between computed velocity profiles and real measurements may be attributed to the way the∆p is distributed over several cells.…”
Section: Introductionmentioning
confidence: 98%
“…The influence of AD in the equations can be implemented as an additional body force acting against the flow. The most common approach reported in the literature is to create an interface where a momentum sink term is applied [12,13]. The associated pressure drop ( ) ∆p is calculated from a semi-empirical relation between the thrust coefficient curve and the velocity at the disc.…”
Section: Introductionmentioning
confidence: 99%
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“…The under-prediction of the far wake by ADM was observed also by other studies (Rados et al, 2012;Sanderse et al, 2011;Vafiadis et al, 2013;Crasto et al, 2012;Prospathopoulos et al, 2011). Especially for the downstream distance of five diameters, which is of high interest since it is commonly used by industry as a separation distance in wind farms, results show that there is a failure to capture accurately the velocity deficit with the standard actuator disk model for most turbulence models.…”
mentioning
confidence: 56%
“…Once the U ref is known, C T can be estimated through the thrust curve of the wind turbine generator considered as uniform 15 over the rotor area (Rados et al, 2012;Crasto et al, 2012;Mikkelsen, 2003). However, in operating conditions, the flow across the rotor is very complex with varying span-wise properties, due to the blade characteristics, rotational velocity, turbulence, finite number of blades and also other flow characteristics related to non-uniform inflow conditions, atmospheric boundary layer shear and so on.…”
Section: Wind Turbine Modellingmentioning
confidence: 99%