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Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

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C t<br />

(a)<br />

C P<br />

(b)<br />

2.5<br />

2.0<br />

1.5<br />

1.0<br />

0.5<br />

0<br />

20<br />

15<br />

10<br />

5<br />

0<br />

0<br />

0<br />

Axial-flow Turbines: Two-dimensional Theory 135<br />

g<br />

0°<br />

4°<br />

6°<br />

8°<br />

10°<br />

12°<br />

0.5<br />

g<br />

0°<br />

4°<br />

6°<br />

8°<br />

10°<br />

12°<br />

0.5<br />

FIG 4.30. Turbine characteristics under steady flow conditions: (a) Torque coefficient;<br />

(b) Input power coefficient. (From Kim et al. 2002, with permission <strong>of</strong> Elsevier).<br />

shown in Figure 4.31, the mean efficiency <strong>of</strong> the cycle can be computed. Figure 4.32<br />

shows the mean efficiency as a function <strong>of</strong> the flow coefficient f for a range <strong>of</strong> g values<br />

with c xi = 0.6cxo.<br />

Compared to the basic Wells turbine (with g =0deg), the optimum result for g =10<br />

deg shows an improved mean efficiency <strong>and</strong> an optimum flow coefficient <strong>of</strong> about 0.4.<br />

It is apparent that further field testing would be needed to prove the concept.<br />

f<br />

f<br />

1.0<br />

1.0<br />

1.5<br />

1.5

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