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48 Numerical Computations of <strong>Wind</strong> Turbine Wakes 261<br />

Frame 001 ⏐ 27 Jan 2005 ⏐ volume solution<br />

Fig. 48.2. x = 0-plane, pressure distribution; y = 0-plane, streamwise velocity; iso<br />

surface, constant vorticity with a surface of a contour pressure distribution<br />

block side. The total number of node points are then: 5.5×10 5 , 1.3×10 6 , 2.6×<br />

10 6 , and 4.4 × 10 6 .<br />

The sensitivity of the Gaussian smearing and the Reynolds number has<br />

also been studied.<br />

An evaluation method to extract values of the circulation from the wake<br />

flow field is developed. When the circulation is evaluated in the wake, an<br />

integration is performed around a loop, enclosing the vortex. Each vortex is<br />

evaluated in terms of its circulation in a plane perpendicular to the turbine<br />

disc. The vortex created at the tip, or at least close to the tip, is evaluated<br />

every 30 ◦ behind the blade. The root vortex is evaluated in the same manner<br />

but since the vortices tend to be smeared out further downstream, because of<br />

diffusion, it is more difficult to evaluate the circulation further downstream in<br />

this case. The circulation is integrated at a specific value of the vorticity.<br />

The sensitivity of the circulation with respect to the grid resolution has<br />

been evaluated. The evaluation was performed with three different grid sizes,<br />

64, 80, and 96 node points at each side of the blocks. The solution converges<br />

with greater grid size.<br />

Some wiggles appear at some distance downstream and can probably be<br />

explained by a too few number of grid points when the circulation is integrated<br />

and because of increasing smearing of the cores further downstream. When<br />

using a finer grid, the vortices become more concentrated and the integration<br />

can be performed further downstream without large fluctuations in the result.

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