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48<br />

Numerical Computations of <strong>Wind</strong> Turbine<br />

Wakes<br />

Stefan Ivanell, Jens N. Sørensen and Dan Henningson<br />

48.1 Numerical Method<br />

Numerical simulations using CFD are performed for wind turbine applications.<br />

The aim of the project is to get a better understanding of wake behaviour<br />

that cannot be obtained by standard industrial design codes for wind<br />

power applications. Such codes are based on the Blade Element Momentum<br />

(BEM) technique, extended with a number of empirical corrections that are<br />

not entirely based on physical flow features. The importance of accurate design<br />

models also increases as the turbines become larger. Therefore, the research<br />

is today undergoing a shift toward more fundamental approaches, aiming at<br />

understanding basic aerodynamic mechanisms.<br />

Theoretically, the bound circulation on the blades is equal to the circulation<br />

behind the rotor, i.e. in the wake. For inviscid flows, the sum of the<br />

circulation of the tip and the root vortex should ideally be zero. However, this<br />

is not entirely correct for viscous flow. The tip and root vortex do, however,<br />

both for inviscid and viscous flows, have different sense of rotation, i.e. different<br />

signs of the circulation. A steep decline of circulation toward the tip will<br />

lead to a rapid concentration of the vortex at the tip (occurring a few chord<br />

lengths behind the tip). The sign of the circulation gradient along the blade<br />

will also determine the sense of rotation of the vortex behind the blade.<br />

The simulations are performed using the CFD program “EllipSys3D” developed<br />

at DTU (The Technical University of Denmark) and Risø. The socalled<br />

Actuator Line Method is used, where the blade is represented by a line<br />

instead of a large number of panels. The forces on that line are introduced<br />

by using tabulated aerodynamic coefficients. In this way, computer resources<br />

are used more efficiently since the number of node points locally around the<br />

blade is decreased, and they are instead concentrated in the wake behind the<br />

blades. The actuator line method was introduced by Sørensen and Shen [1]<br />

and later implemented into the EllipSys3D code by Mikkelsen [2]. EllipSys3D<br />

is a general purpose 3D solver developed by Sørensen [3] and Michelsen [4,5].

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