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Handbook of Turbomachinery Second Edition Revised - Ventech!

Handbook of Turbomachinery Second Edition Revised - Ventech!

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Figure 49 Modal diameters <strong>of</strong> a low-pressure turbine disk.<br />

blading modifications and have been used to assess the potential payback<br />

for such changes. In a number <strong>of</strong> cases, the need to replace worn or eroded<br />

airfoils and the nature <strong>of</strong> the replacement have been established by the use<br />

<strong>of</strong> three-dimensional CFD studies.<br />

Prior to the early 1990s, flow analysis was performed primarily with<br />

axisymmetric flow field computer programs (one-dimensional and later twodimensional<br />

models). However, in the final stages <strong>of</strong> the LP turbine, the flow<br />

undergoes a phase change because <strong>of</strong> steam expansion and is significantly<br />

three-dimensional (Fig.51). Furthermore, this nonequilibrium phasechange<br />

produces vapor subcooling (supersaturation), which can locally alter the<br />

velocity triangles in the critical area near the leading edges <strong>of</strong> fixed as well as<br />

rotating blades.<br />

Copyright © 2003 Marcel Dekker, Inc.

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