13.02.2013 Views

Mechanics of Fluids

Mechanics of Fluids

Mechanics of Fluids

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

622 Fluid machines<br />

Fig. 13.20<br />

Cavitation is a phenomenon by no means confined to turbines. Wherever<br />

it exists it is an additional factor to be considered if dynamic similarity is<br />

sought between one situation and another. Similarity <strong>of</strong> cavitation requires<br />

the cavitation number (p − pv)/ 1<br />

2ϱu2 (see Section 5.5.3) to be the same<br />

at corresponding points. Experiments suggest, however, that similarity <strong>of</strong><br />

cavitation is difficult to achieve.<br />

Example 13.2 A vertical-shaft Francis water turbine rotates at 6.25<br />

revolutions per second under a net head <strong>of</strong> 27.5 m. The runner has,<br />

at inlet, a diameter <strong>of</strong> 0.75 m, a flow area <strong>of</strong> 0.2 m 2 , and a blade<br />

angle <strong>of</strong> 75 ◦ . The guide-vane angle (at outlet) is 15 ◦ . At the entrance<br />

to the draft tube there is no whirl velocity and the absolute pressure is<br />

35 kPa. Atmospheric pressure is 101.3 kPa. To design the draft tube,<br />

the critical cavitation parameter σc, based on the minimum pressure in<br />

the draft tube, is related to the power specific speed �P <strong>of</strong> the machine<br />

by σc = 0.119(�P) 1.84 , where �P is in radians. Calculate the overall<br />

efficiency <strong>of</strong> the turbine assuming that the mechanical efficiency is 0.97<br />

and determine the limiting value for the height <strong>of</strong> the draft tube above<br />

the surface <strong>of</strong> the tail race.<br />

Solution<br />

u1 = wr = πND = π6.25 × 0.75 m · s −1 = 14.73 m · s −1<br />

v1 = u1 sin 105 ◦ / sin 60 ◦ = 16.42 m · s −1<br />

vr1 = v1 sin 15 ◦ = 4.25 m · s −1<br />

vw1 = v1 cos 15 ◦ = 15.87 m · s −1<br />

vw2 = 0

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!