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684 Chapter 12 ■ Turbomachines<br />

For geometrically similar turbines and for negligible Reynolds number and surface roughness difference<br />

effects, the relationships between the dimensionless parameters are given functionally by<br />

that shown in Eqs. 12.29, 12.30, and 12.31. That is,<br />

C H f 1 1C Q 2, C p f 2 1C Q 2, and h f 3 1C Q 2<br />

where the functions f 1 , f 2 , and f 3 are dependent on the type of turbine involved. Also, for turbines<br />

the efficiency, h, is related to the other coefficients according to h C pC H C Q .<br />

As indicated above, the design engineer has a variety of turbine types available for any given<br />

application. It is necessary to determine which type of turbine would best fit the job 1i.e., be most efficient2<br />

before detailed design work is attempted. As with pumps, the use of a specific speed parameter<br />

can help provide this information. For hydraulic turbines, the rotor diameter D is eliminated<br />

between the flow coefficient and the power coefficient to obtain the power specific speed, N¿ s , where<br />

N¿ s v2W# shaftr<br />

1gh a 2 5 4<br />

We use the more common, but not dimensionless, definition of specific speed<br />

Specific speed may<br />

be used to approximate<br />

what kind of<br />

turbine geometry<br />

(axial to radial)<br />

would operate most<br />

efficiently.<br />

N¿ sd v1rpm2 2W# shaft 1bhp2<br />

(12.53)<br />

3h a 1ft24 5 4<br />

That is, N¿ is calculated with angular velocity, in rpm; shaft power, W # sd v,<br />

shaft, in brake horsepower;<br />

and actual head available, h a , in feet. Optimum turbine efficiency 1for large turbines2 as a function<br />

of specific speed is indicated in Fig. 12.32. Also shown are representative rotor and casing cross<br />

sections. Note that impulse turbines are best at low specific speeds; that is, when operating with<br />

large heads and small flowrate. The other extreme is axial-flow turbines, which are the most efficient<br />

type if the head is low and if the flowrate is large. For intermediate values of specific speeds,<br />

radial- and mixed-flow turbines offer the best performance.<br />

The data shown in Fig. 12.32 are meant only to provide a guide for turbine-type selection.<br />

The actual turbine efficiency for a given turbine depends very strongly on the detailed design of<br />

the turbine. Considerable analysis, testing, and experience are needed to produce an efficient turbine.<br />

However, the data of Fig. 12.32 are representative. Much additional information can be found<br />

in the literature.<br />

Impulse turbines<br />

Reaction turbines<br />

Radial-flow Mixed-flow Axial-flow<br />

100<br />

90<br />

10 20 40 60 80 100<br />

N′<br />

sd<br />

Impulse<br />

Francis<br />

Kaplan<br />

η %<br />

80<br />

70<br />

N′<br />

sd<br />

and maximum efficiencies as a<br />

function of specific speed.<br />

F I G U R E 12.32<br />

10 20 40 60 80 100<br />

Typical turbine cross sections

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