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15<br />

Simulation of Turbulence, Gusts and Wakes<br />

for Load Calculations<br />

Jakob Mann<br />

15.1 Introduction<br />

In order to simulate dynamic loads on a wind turbine rotor it is necessary to<br />

simulate the turbulent inflow to the rotor realistically. In this paper we review<br />

various methods to do so. In many situations, for example for strong winds<br />

over flat terrain, turbulence may be considered for practical load calculation<br />

purposes not far from being Gaussian. In this situation it is enough to know the<br />

second-order statistics, e.g. spectra and cross-spectra, to be able to simulate.<br />

The second-order statistics are either obtained from empirical one-dimensional<br />

spectra and coherences as in the Sandia method, or from a semi-empirical<br />

three-dimensional spectral tensor as in the Mann model [4,5]. These methods,<br />

which both appear in the third edition of the IEC standard 61400-1, will be<br />

compared.<br />

The assumptions of the models; stationarity, homogeneity, and gaussianity,<br />

can all be questioned, especially when the terrain is not simple or when<br />

turbines appear in wind farms. Here a variety of methods are possible and we<br />

will present a few practical examples of these. Particular emphasis will be put<br />

on “constrained Gaussian simulation” where extreme gusts can be embedded<br />

in a turbulent field. This method can also be used simulate entire fields based<br />

on measurements in a few points. Practical simulations of wake turbulence<br />

based on meandering will also be presented together with preliminary remote<br />

sensing measurements [2].<br />

15.2 Simulation over Flat Terrain<br />

The basis of most practical models to simulate the inflow turbulence for aeroelastic<br />

codes, such as HAWC and FLEX, is the second order statistics. It<br />

is true that real turbulence can not be gaussian. This can, for example, be<br />

seen from the famous relation � δv�(r) 3� = − 4<br />

5εr [3], which states that the<br />

mean of the cube of difference in the velocity component along the separation

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