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U mean / U ref<br />

1<br />

0.9<br />

0.8<br />

0.7<br />

49 Modelling <strong>Wind</strong> Turbine Wakes with a Porosity Concept 267<br />

0.6<br />

X = 2D<br />

X = 4D<br />

X = 6D<br />

X = 9D<br />

X = 12D<br />

0.5<br />

−1.5 −1 −0.5 0 0.5<br />

X = 15D<br />

1 1.5<br />

r/D<br />

I u / I u0<br />

3<br />

2.5<br />

2<br />

1.5<br />

1<br />

−1.5 −1 −0.5 0 0.5 1 1.5<br />

Fig. 49.1. Streamwise velocity and turbulence intensity downstream of a porous<br />

disc<br />

Figure 49.1 presents results for a 100 mm-diameter disc made of mesh 6 at<br />

different downstream locations. The near-wake area, characterized by an annular<br />

shear layer and an annular turbulence intensity distribution, is well<br />

defined and ends up at x/D = 4, where the two shear layers start collapsing.<br />

The deduced axial flow induction factor is a =0.18. The far wake starts at<br />

x/D = 9, from where the mean velocity and turbulence intensity profiles are<br />

self-similar. At x/D = 9, the turbulence intensity is locally three times higher<br />

than the freestream turbulence intensity Iu0.<br />

Tests on the influence of the porosity level on the velocity and turbulence<br />

distributions show that one can totally control the velocity deficit, and so the<br />

shear-generated turbulence, using the appropriate mesh porosity level. Tests<br />

on the mesh cell size for a fixed porosity level (65%) illustrate that when the<br />

ratio between the mesh cell size and the disc diameter is smaller than 0.05,<br />

the velocity distribution is independent of the mesh. If this ratio is respected,<br />

it is also independent of the disc size.<br />

49.4 Results for Shear Freestream Conditions<br />

A wind farm was built with 9 square-arranged porous discs made of mesh<br />

6 mounted on masts (Fig. 49.2). The masts spacing is ∆x = ∆y = 3D.<br />

Figure 49.3 shows the mean velocity distributions 3D downstream of the first,<br />

the second and the third row of porous discs. The black circle shows the disc<br />

circumference. Classical features of the wind turbine wakes are found [4]. As<br />

expected, the velocity deficit is located lower than the disc centre, due to the<br />

ground effect. The velocity deficit increases between the first and the second<br />

row, but stays constant between the second and the third one, although the<br />

wake extend is still growing. Figure 49.4 shows the turbulence intensity distributions<br />

at the same locations. It is worth to notice that, after three rows,<br />

the turbulence intensity can locally reach 26%, due to the combination of the<br />

r/D

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