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Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

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Example 10.2. Determine the radii <strong>of</strong> the unmixed slipstream at the disc (R2) <strong>and</strong><br />

far downstream <strong>of</strong> the disc (R3) compared with the radius far upstream (R1).<br />

Solution. Continuity requires that<br />

pRc 1 x pRcx pRcx<br />

R R cx cx a R R a<br />

R R cx cx a R R a<br />

R R a a<br />

2<br />

1 2 2<br />

2 3 2<br />

= = 3<br />

( 2<br />

2<br />

1)<br />

= 1 2 = 1 ( 1- ) 2 1<br />

.<br />

= 1 ( 1-<br />

)<br />

( 3<br />

2<br />

1)<br />

= 1 3 = 1 ( 1-2 ) 3 1 = 1 ( 1-2 )<br />

(<br />

0.5<br />

)= ( 1- ) ( 1-2 )<br />

3 2<br />

Choosing a value <strong>of</strong> a – = 1 – 3, corresponding to the maximum power condition, the radius<br />

ratios are R2/R1 = 1.225, R3/R1 = 1.732 <strong>and</strong> R3/R2 = 1.414.<br />

Example 10.3. Using the above expressions for an actuator disc, determine the<br />

power output <strong>of</strong> a HAWT <strong>of</strong> 30m tip diameter in a steady wind blowing at<br />

(i) 7.5m/s,<br />

(ii) 10m/s.<br />

Assume that the air density is 1.2kg/m 3 <strong>and</strong> that a – = 1 – 3 .<br />

Solution. Using eqn. (10.10) <strong>and</strong> substituting a – = 1 – 3 , r = 1.2kg/m 2 <strong>and</strong> A 2 =p15 2 ,<br />

then<br />

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

3<br />

r<br />

= 251. 3c<br />

2 x1<br />

2 = ¥ 1. 2 ¥ p15<br />

¥ 1-<br />

3<br />

3<br />

x1<br />

P 1<br />

[ ]<br />

( )<br />

(i) With cx1 = 7.5m/s, P = 106kW.<br />

(ii) With cx1 = 10m/s, P = 251.3kW.<br />

2<br />

2 1<br />

3<br />

2<br />

c<br />

3<br />

x1<br />

These two examples give some indication <strong>of</strong> the power available in the wind.<br />

P 2+<br />

P 2–<br />

05<br />

05 .<br />

Wind Turbines 335<br />

FIG. 10.7. Schematic <strong>of</strong> the pressure variation before <strong>and</strong> after the plane <strong>of</strong> the<br />

actuator disc.

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