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Handbook of Turbomachinery Second Edition Revised - Ventech!

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where<br />

and<br />

y ¼ T 0 in<br />

TSTD<br />

d ¼ p0 in<br />

pSTD<br />

ð47Þ<br />

ð48Þ<br />

The standard conditions are usually taken to be 518.7 R and 14.7 psia.<br />

Corrected speed is defined as<br />

Ncorr ¼ N pffiffiffi ð49Þ<br />

y<br />

Equation (5) shows torque to be the product <strong>of</strong> flow rate and the change in<br />

tangential velocity across the rotor. Corrected flow is defined above;<br />

corrected velocities appear with y 1=2 in the denominator from the corrected<br />

shaft speed. Therefore, corrected torque is defined as<br />

Gcorr ¼ G<br />

d<br />

ð50Þ<br />

The form <strong>of</strong> the corrected power is determined from the product <strong>of</strong><br />

corrected torque and corrected speed:<br />

Pcorr ¼ P<br />

d ffiffi p ð51Þ<br />

y<br />

These corrected quantities are used to reduce turbine performance data to<br />

curves <strong>of</strong> constant-pressure ratio on two charts. Figure 11 presents typical<br />

turbine performance maps using the corrected quantities. Figure 11(a)<br />

presents corrected flow as afunction <strong>of</strong> corrected speed and pressure ratio,<br />

while Fig. 11(b) shows corrected torque versus corrected speed and pressure<br />

ratio. Characteristics typical <strong>of</strong> both radial-inflow and axial-flow turbines<br />

are presented in Fig. 11.<br />

AXIAL-FLOW TURBINE SIZING<br />

Axial-Flow Turbine Performance Prediction<br />

Prediction methods for axial-flow turbine performance methods can be<br />

roughly broken into two groups according to Sieverding [10]. The first<br />

group bases turbine stage performance on overall parameters such as work<br />

coefficient and flow coefficient. These are most <strong>of</strong>ten used in preliminary<br />

Copyright © 2003 Marcel Dekker, Inc.

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