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Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

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330 <strong>Fluid</strong> <strong>Mechanics</strong>, <strong>Thermodynamics</strong> <strong>of</strong> <strong>Turbomachinery</strong><br />

electricity produced from wind energy are set to continue. They estimate that 22,000MW<br />

<strong>of</strong> wind energy capacity, in the form <strong>of</strong> 40,000 wind turbines, will be installed in the next<br />

ten years. However, in the trade journal Wind Power Monthly (March 2004), around<br />

8200MW <strong>of</strong> new wind power capacity was installed in 2003, 21% more than the previous<br />

year. This was enough to maintain the annual growth rate at almost the same level<br />

<strong>of</strong> over 26%. The European growth rate in 2003 was similar to the global figure <strong>of</strong> around<br />

24% while in the USA (up to the end <strong>of</strong> 2003) a surge <strong>of</strong> economic activity pushed<br />

its growth rate up to 35%. In the 1990s the cost <strong>of</strong> manufacturing wind turbines declined<br />

by 20% for each doubling <strong>of</strong> the number <strong>of</strong> wind turbines manufactured. Currently,<br />

the production <strong>of</strong> large-scale, grid-connected wind turbines doubles about every three<br />

years. A general survey <strong>of</strong> the economics <strong>of</strong> wind turbines <strong>and</strong> the forecasting <strong>of</strong><br />

cost reduction <strong>of</strong> electricity production is given by Ackermann <strong>and</strong> Söder (2002).<br />

Outline <strong>of</strong> the theory<br />

In the following pages the aerodynamic theory <strong>of</strong> the HAWT is gradually developed,<br />

starting with the simple one-dimensional momentum analysis <strong>of</strong> the actuator disc <strong>and</strong><br />

followed by the more detailed analysis <strong>of</strong> the blade element theory. The flow state just<br />

upstream <strong>of</strong> the rotor plane forms the so-called inflow condition for the rotor blades<br />

<strong>and</strong> from which the aerodynamic forces acting on the blades can be determined. The<br />

well-known blade element momentum (BEM) method is outlined <strong>and</strong> used extensively.<br />

A number <strong>of</strong> worked examples are included at each stage <strong>of</strong> development to illustrate<br />

the application <strong>of</strong> the theory. Detailed calculations using the BEM method were made<br />

to show the influence <strong>of</strong> various factors such as the tip–speed ratio <strong>and</strong> blade number<br />

on performance. Further development <strong>of</strong> the theory includes the application <strong>of</strong> Pr<strong>and</strong>tl’s<br />

tip loss correction factor that corrects for a finite number <strong>of</strong> blades. Glauert’s optimisation<br />

analysis is developed <strong>and</strong> used to determine the ideal blade shape for a given lift<br />

coefficient <strong>and</strong> to show how optimum rotor power coefficient is influenced by the choice<br />

<strong>of</strong> tip–speed ratio.<br />

Actuator disc approach<br />

Introduction<br />

The concept <strong>of</strong> the actuator disc was used in Chapter 6 as a method <strong>of</strong> determining<br />

the three-dimensional flows in compressor <strong>and</strong> turbine blade rows. Betz (1926) in his<br />

seminal work on the flow through windmill blades used a much simpler version <strong>of</strong> the<br />

actuator disc. As a start to underst<strong>and</strong>ing the power production process <strong>of</strong> the turbine<br />

consider the flow model shown in Figure 10.5 where the rotor <strong>of</strong> the HAWT is replaced<br />

by an actuator disc. It is necessary to make a number <strong>of</strong> simplifying assumptions concerning<br />

the flow but, fortunately, the analysis yields useful approximate results.<br />

Theory <strong>of</strong> the actuator disc<br />

The assumptions made are as follows:<br />

(i) steady uniform flow upstream <strong>of</strong> the disc;<br />

(ii) uniform <strong>and</strong> steady velocity at the disc;

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