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Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

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where a – T = 0.3262.<br />

Sharpe (1990) noted that for most practical, existent HAWTs, the value <strong>of</strong> a – rarely<br />

exceeds 0.6.<br />

Estimating the power output<br />

Preliminary estimates <strong>of</strong> rotor diameter can easily be made using simple actuator<br />

disc theory. A number <strong>of</strong> factors need to be taken into account, i.e. the wind regime in<br />

which the turbine is to operate <strong>and</strong> the tip–speed ratio. Various losses must be allowed<br />

for, the main ones being the mechanical transmission including gearbox losses <strong>and</strong> the<br />

electrical generation losses. From the actuator disc theory the turbine aerodynamic<br />

power output is<br />

P= A C c<br />

1 r<br />

2 2 p x1<br />

3<br />

Under theoretical ideal conditions the maximum value <strong>of</strong> Cp = 0.593. According to<br />

Eggleston <strong>and</strong> Stoddard (1987), rotor Cp values as high as 0.45 have been reported.<br />

Such high, real values <strong>of</strong> Cp relate to very precise, smooth aer<strong>of</strong>oil blades <strong>and</strong> tip–speed<br />

ratios above 10. For most machines <strong>of</strong> good design a value <strong>of</strong> Cp from 0.3 to 0.35 would<br />

be possible. With a drive train efficiency, hd <strong>and</strong> an electrical generation efficiency, hg<br />

the output electrical power would be<br />

P = A C c<br />

1 r h h<br />

el 2 2 p g d x1<br />

3<br />

Example10.4. Determine the size <strong>of</strong> rotor required to generate 20kW <strong>of</strong> electrical<br />

power in a steady wind <strong>of</strong> 7.5m/s. It can be assumed that the air density, r = 1.2kg/m 3 ,<br />

Cp = 0.35, hg = 0.75 <strong>and</strong> hd = 0.85.<br />

Solution. From the above expression the disc area is<br />

A = 2 P ( rC h h c )= 2 ¥ 20 ¥ 10 1. 2 ¥ 0. 35 ¥ 0. 75 ¥ 0. 85 ¥ 7. 5<br />

3 3 3<br />

2 el p g d x1<br />

= 354. 1 m2 Hence, the diameter is 21.2m.<br />

Power output range<br />

The kinetic power available in the wind is<br />

1 P0 A cx<br />

3<br />

= r<br />

2 2 1<br />

( )<br />

Wind Turbines 337<br />

(10.10b)<br />

where A2 is the disc area <strong>and</strong> cx1 is the velocity upstream <strong>of</strong> the disc. The ideal power<br />

generated by the turbine can therefore be expected to vary as the cube <strong>of</strong> the wind<br />

speed. Figure 10.9 shows the idealised power curve for a wind turbine, where the above<br />

cubic “law” applies between the so-called cut-in wind speed <strong>and</strong> the rated wind speed<br />

at which the maximum power is first reached. The cut-in speed is the lowest wind speed<br />

at which net (or positive) power is produced by the turbine. The rated wind speed generally<br />

corresponds to the point at which the efficiency <strong>of</strong> energy conversion is close to<br />

its maximum.<br />

At wind speeds greater than the rated value, for most wind turbines, the power output<br />

is maintained constant by aerodynamic controls (discussed under “Control Methods”).

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