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Handbook of Turbomachinery Second Edition Revised - Ventech!

Handbook of Turbomachinery Second Edition Revised - Ventech!

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include not only the pressure change across the turbomachine blading <strong>of</strong><br />

interest but also the pressure losses due to flow-path ducting from the inlet<br />

pressure measurement plane to the stage <strong>of</strong> interest and from the blading<br />

exit plane to the discharge measurement station.<br />

A careful accounting <strong>of</strong> both stage pressure ratio characteristics and<br />

flow-path total pressure losses must be made. Often flow-path duct losses<br />

are ‘‘doubled-dipped’’ because the analyst fails to recognize that flow-path<br />

duct losses are included in the stage performance map because <strong>of</strong> the way<br />

the test rig was instrumented. Likewise, losses may be missed should the<br />

analyst not include duct losses that were thought to be included, but were<br />

not, in the stage performance map pressure characteristics.<br />

Radial immersion rakes, similar to the rake configuration seen in Fig.<br />

5, are used to measure turbomachine stage inlet and exit pressures. Total<br />

pressures are measured with impact or kiel sensors mounted on rakes that<br />

are immersed into the flow path. The individual impact sensor tube axes<br />

should be aligned parallel to the incoming flow direction. A choice must be<br />

made by the engineer to select the number <strong>of</strong> rakes such that the flow field is<br />

adequately defined but the flow path is not blocked nor significantly altered<br />

by the installed rakes.<br />

A generally accepted practice is to install inlet rakes at least a duct<br />

diameter upstream <strong>of</strong> the test stage. This separation distance minimizes flow<br />

and mechanical interactions due to the rake’s wake on the test blading, while<br />

Figure 5 Radial immersion rake.<br />

Copyright © 2003 Marcel Dekker, Inc.

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