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Mechanics of Fluids

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658 Fluid machines<br />

0.85. Show that the power specific speed is 1.21 d/D rad,<br />

where d represents the jet diameter and D the wheel diameter.<br />

For the nozzle Cv = 0.97.<br />

13.5 The following data refer to a Pelton wheel. Maximum overall<br />

efficiency 79%, occurring at a speed ratio <strong>of</strong> 0.46; Cv<br />

for nozzle = 0.97; jet turned through 165 ◦ . Assuming that<br />

the optimum speed ratio differs from 0.5 solely as a result <strong>of</strong><br />

losses to windage and bearing friction which are proportional<br />

to the square <strong>of</strong> the rotational speed, obtain a formula for the<br />

optimum speed ratio and hence estimate the ratio <strong>of</strong> the relative<br />

velocity at outlet from the buckets to the relative velocity<br />

at inlet.<br />

13.6 In a vertical-shaft inward-flow reaction turbine the sum <strong>of</strong><br />

the pressure and kinetic heads at entrance to the spiral casing<br />

is 120 m and the vertical distance between this section<br />

and the tail-race level is 3 m. The peripheral velocity <strong>of</strong><br />

the runner at entry is 30 m · s −1 , the radial velocity <strong>of</strong> the<br />

water is constant at 9 m · s −1 and discharge from the runner<br />

is without whirl. The estimated hydraulic losses are:<br />

(1) between turbine entrance and exit from the guide vanes,<br />

4.8 m (2) in the runner, 8.8 m, (3) in the draft tube, 790 mm,<br />

(4) kinetic head rejected to the tail race, 460 mm. Calculate<br />

the guide vane angle and the runner blade angle at<br />

inlet and the pressure heads at entry to and exit from the<br />

runner.<br />

13.7 An inward-flow reaction turbine has an inlet guide vane angle<br />

<strong>of</strong> 30 ◦ and the inlet edges <strong>of</strong> the runner blades are at 120 ◦ to<br />

the direction <strong>of</strong> whirl. The breadth <strong>of</strong> the runner at inlet is<br />

a quarter <strong>of</strong> the diameter at inlet and there is no velocity <strong>of</strong><br />

whirl at outlet. The overall head is 15 m and the rotational<br />

speed 104.7 rad · s −1 (16.67 rev/s). The hydraulic and overall<br />

efficiencies may be assumed to be 88% and 85% respectively.<br />

Calculate the runner diameter at inlet and the power<br />

developed. (The thickness <strong>of</strong> the blades may be neglected.)<br />

13.8 A vertical-shaft Francis turbine, with an overall efficiency <strong>of</strong><br />

90%, runs at 44.86 rad · s −1 (7.14 rev/s) with a water discharge<br />

<strong>of</strong> 15.5 m 3 · s −1 . The velocity at the inlet <strong>of</strong> the spiral<br />

casing is 8.5 m · s −1 and the pressure head at this point is<br />

240 m, the centre-line <strong>of</strong> the casing inlet being 3 m above the<br />

tail-water level. The diameter <strong>of</strong> the runner at inlet is 2.23 m<br />

and the width at inlet is 300 mm. The hydraulic efficiency is<br />

93%. Determine (a) the output power, (b) the power specific<br />

speed, (c) the guide vane angle, (d) the runner blade angle<br />

at inlet, (e) the percentage <strong>of</strong> the net head which is kinetic at<br />

entry to the runner. Assume that there is no whirl at outlet<br />

from the runner and neglect the thickness <strong>of</strong> the blades.<br />

13.9 The runner <strong>of</strong> a vertical-shaft Francis turbine is 450 mm diameter<br />

and 50 mm wide at inlet and 300 mm diameter and

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