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Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

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It is convenient to define an axial flow induction factor, a – (invariant with radius), for<br />

the actuator disc,<br />

Hence,<br />

The power coefficient<br />

(10.9)<br />

(10.10)<br />

For the unperturbed wind (i.e. velocity is c x1) with the same flow area as the disc (A2<br />

= pR 2 ), the kinetic power available in the wind is<br />

1 P c Ac Ac<br />

2<br />

1 3<br />

= ( r )= r .<br />

0<br />

2<br />

a = ( c -c<br />

) c<br />

P= 2a A c ( 1-a)<br />

3<br />

cx2 = cx1( 1-a)<br />

r<br />

A power coefficient Cp is defined as<br />

Cp = P P0= 4a( 1 -a)<br />

.<br />

(10.11)<br />

The maximum value <strong>of</strong> Cp is found by differentiating Cp with respect to a – , i.e. finally<br />

dCp da<br />

= 41 ( -a)<br />

( 1-3a)= 0<br />

which gives two roots, a – = 1/3 <strong>and</strong> 1.0. Using the first value, the maximum value <strong>of</strong><br />

the power coefficient is<br />

C pmax = 16 27 = 0. 593.<br />

(10.12)<br />

This value <strong>of</strong> Cp is <strong>of</strong>ten referred to as the Betz limit, referring to the maximum<br />

possible power coefficient <strong>of</strong> the turbine (with the prescribed flow conditions).<br />

A useful measure <strong>of</strong> wind turbine performance is the ratio <strong>of</strong> the power coefficient<br />

CP to the maximum power coefficient CPmax. This ratio, which may be called the relative<br />

maximum power coefficient, is<br />

z = 27 16C P.<br />

x12 x1 2 2 x1<br />

The axial force coefficient<br />

The axial force coefficient is defined as<br />

1 C X c A 2 r<br />

= ( )<br />

X 2 x1<br />

x1 x2 x1<br />

2 x1<br />

( ) ( )<br />

1<br />

= mc -ccA<br />

2<br />

2 ˙<br />

r<br />

x1 x2 2 x1<br />

x2 x1 x2 x1<br />

2<br />

= 4c<br />

( c -c<br />

) c<br />

= 4a( 1-a)<br />

(10.12a)<br />

(10.13)<br />

By differentiating this expression with respect to a – we can show that CX has a maximum<br />

value <strong>of</strong> unity at a – = 0.5. Figure 10.6 shows the variation <strong>of</strong> both Cp <strong>and</strong> C X as functions<br />

<strong>of</strong> the axial induction factor, a – .<br />

Example 10.1. Determine the static pressure changes that take place<br />

(i) across the actuator disc;<br />

(ii) up to the disc from far upstream;<br />

(iii) from the disc to far downstream.<br />

2<br />

2<br />

2<br />

2<br />

Wind Turbines 333

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