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Aerodynamic calculation of loads and dynamic behavior of wind ...

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it is obvious that the power output <strong>of</strong> a <strong>wind</strong> turbine is a function <strong>of</strong> the power<br />

coefficient, the air density, the rotor area <strong>and</strong> the <strong>wind</strong> velocity. The power<br />

coefficient varies with the tip speed ratio (see Chapter 3) <strong>and</strong> describes the fraction <strong>of</strong><br />

the power in the <strong>wind</strong> that may be converted into mechanical work. Although several<br />

attempts have been made in order to increase its value, a maximum limit <strong>of</strong> 0.593<br />

cannot be exceeded, as will be proven later on. As for the air density, its variations<br />

are essentially negligible. Thus, major changes in the power output can only be<br />

achieved by two means: either by increasing the swept area <strong>of</strong> the rotor, or by<br />

locating the <strong>wind</strong> turbines on sites with higher <strong>wind</strong> speeds. More specifically, a<br />

doubling <strong>of</strong> the rotor diameter leads to a four-time increase in power output. The<br />

influence <strong>of</strong> the <strong>wind</strong> speed is, <strong>of</strong> course, more pronounced with a doubling <strong>of</strong> <strong>wind</strong><br />

speed leading to an eight-fold increase in power. This fact has led to today’s<br />

enormous rotor diameters <strong>of</strong> 60m <strong>and</strong> tower heights <strong>of</strong> more than 100m, in order to<br />

take advantage <strong>of</strong> the increase <strong>of</strong> <strong>wind</strong> speed with height (see Chapter 2). Both these<br />

characteristics <strong>of</strong> modern <strong>wind</strong> turbines, despite the remarkable addition to the<br />

efficiency, encumber the tower with all the greater <strong>wind</strong> <strong>loads</strong>. The blades, the tower<br />

<strong>and</strong> finally the foundation <strong>of</strong> a <strong>wind</strong> turbine are exposed to even more significant<br />

forces <strong>and</strong> moments as the <strong>wind</strong> speed <strong>and</strong> rotor diameters increase. Furthermore,<br />

these <strong>loads</strong> are <strong>of</strong> a <strong>dynamic</strong> nature, that is, they vary with time <strong>and</strong> spatial distance,<br />

an aspect that renders their <strong>calculation</strong> a rather complex procedure. This complexity<br />

is based on two different factors: Firstly, the <strong>wind</strong> variations are impossible to predict<br />

<strong>and</strong> calculate using any kind <strong>of</strong> deterministic methods. The mean <strong>wind</strong> speed is<br />

subject to changes from one point to another, let alone the <strong>wind</strong> turbulence, which is<br />

a continuously varying parameter, which can only be approached by means <strong>of</strong><br />

stochastic analysis. Secondly, the aero<strong>dynamic</strong> characteristics <strong>of</strong> the rotor follow their<br />

own, rather complicated physical laws. The less the simplistic assumptions made<br />

regarding these rules, the more one has to indulge into the subject in order to reach an<br />

adequate knowledge level.<br />

1.2 Thesis’s objective<br />

The aim <strong>of</strong> this thesis is to <strong>of</strong>fer a concise description <strong>of</strong> the phenomenon <strong>of</strong><br />

airflow passing through the rotor <strong>of</strong> a modern horizontal-axis <strong>wind</strong> turbine, as well as<br />

an algorithm with the utilization <strong>of</strong> which the dimensioning <strong>of</strong> the tower can be<br />

achieved. In chapters 2, 3 the above-mentioned complex concepts are analyzed with<br />

the simpler language possible. Additionally, chapter 2 describes the way a stochastic<br />

<strong>wind</strong> field can be digitally simulated, while chapter 3 provides the means by which<br />

the aero<strong>dynamic</strong> theory <strong>of</strong> the rotating rotor exposed to airflow can be<br />

computationally approached. In chapter 4 the reader shall find some information<br />

regarding the algorithm produced in this thesis, in the MATLAB environment, for<br />

both the simulation <strong>of</strong> the <strong>wind</strong> velocity field <strong>and</strong> the <strong>calculation</strong> <strong>of</strong> the <strong>loads</strong> exerted<br />

on the rotor <strong>and</strong>, consequently on the top <strong>of</strong> the tower. In the 5 th chapter <strong>of</strong> this thesis<br />

the results <strong>of</strong> the program’s execution are demonstrated. These results are obtained<br />

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