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12.10 Chapter Summary and Study Guide 691<br />

Corrected mass flow rate, lb m /s<br />

50<br />

49<br />

48<br />

47<br />

46<br />

45<br />

44<br />

43<br />

42<br />

41<br />

Corrected mass flow rate, kg/s<br />

23.0<br />

22.5<br />

22.0<br />

21.5<br />

21.0<br />

20.5<br />

20.0<br />

19.5<br />

19.0<br />

18.5<br />

Corrected speed as percent<br />

of design speed<br />

40<br />

50<br />

60<br />

70<br />

80<br />

90<br />

100<br />

110<br />

40<br />

39<br />

18.0<br />

17.5<br />

1.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2.0 2.1 2.2 2.3<br />

Ratio of inlet–total to exit–total pressure<br />

F I G U R E 12.40<br />

Typical compressible flow turbine<br />

performance “map.” (Ref. 20)<br />

Turbine performance<br />

maps are<br />

used to display<br />

complex turbine<br />

characteristics.<br />

Because of the reduction of static pressure in the downstream direction, the gas expands, and<br />

the flow passage area must increase from the inlet to the outlet of this turbine. This is seen in Fig.<br />

12.39b.<br />

Performance data for compressible flow turbines are summarized with the help of parameters<br />

derived from dimensional analysis. Isentropic and polytropic efficiencies 1see Refs. 2, 3, and<br />

202 are commonly used as are inlet-to-outlet total pressure ratios 1p 01p 02 2, corrected rotor speed<br />

1see Eq. 12.552, and corrected mass flowrate 1see Eq. 12.542. In Fig. 12.40 is shown a compressible<br />

flow turbine performance “map.”<br />

12.10 Chapter Summary and Study Guide<br />

turbomachine<br />

axial-, mixed-, and<br />

radial-flow<br />

velocity triangle<br />

angular momentum<br />

shaft torque<br />

Euler turbomachine<br />

equation<br />

shaft power<br />

centrifugal pump<br />

pump performance<br />

curve<br />

overall efficiency<br />

system equation<br />

head rise<br />

coefficient<br />

power coefficient<br />

flow coefficient<br />

pump scaling laws<br />

specific speed<br />

impulse turbine<br />

reaction turbine<br />

Pelton wheel<br />

Various aspects of turbomachine flow are considered in this chapter. The connection between <strong>fluid</strong><br />

angular momentum change and shaft torque is key to understanding how turbo-pumps and turbines<br />

operate.<br />

The shaft torque associated with change in the axial component of angular momentum of a<br />

<strong>fluid</strong> as it flows through a pump or turbine is described in terms of the inlet and outlet velocity<br />

triangles diagrams. Such diagrams indicate the relationship among absolute, relative, and blade<br />

velocities.<br />

Performance characteristics for centrifugal pumps are discussed. Standard dimensionless<br />

pump parameters, similarity laws, and the concept of specific speed are presented for use in pump<br />

analysis. How to use pump performance curves and the system curve for proper pump selection<br />

is presented. A brief discussion of axial-flow and mixed-flow pumps is given.<br />

An analysis of impulse turbines is provided, with emphasis on the Pelton wheel turbine. For<br />

impulse turbines there is negligible pressure difference across the blade; the torque is a result of<br />

the change in direction of the <strong>fluid</strong> jet striking the blade. Radial-flow and axial-flow reaction turbines<br />

are also briefly discussed.<br />

The following checklist provides a study guide for this chapter. When your study of the entire<br />

chapter and end-of-chapter exercises has been completed you should be able to<br />

write out meanings of the terms listed here in the margin and understand each of the related<br />

concepts. These terms are particularly important and are set in italic, bold, and color type in<br />

the text.<br />

draw appropriate velocity triangles for flows entering and leaving given pump or turbine<br />

configurations.

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