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Handbook of Turbomachinery Second Edition Revised - Ventech!

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Figure 22 Typical precessional modes: generalized Laval–Jeffcott rotor. (a) First<br />

forward mode, (b) second forward mode.<br />

Disk Flexibility Effects<br />

Rotordynamics analyst should carefully evaluate whether disk flexibility<br />

may significantly influence the lateral dynamics <strong>of</strong> a rotating assembly. A<br />

flexible disk or bladed disk assembly is usually cyclosymmetric. These<br />

flexible disks have a large number <strong>of</strong> natural frequencies consisting <strong>of</strong><br />

‘‘umbrella-type’’ modes that have only circular nodal lines, and ‘‘diametraltype’’<br />

modes where diametral and circular nodal lines may exist. Examples<br />

<strong>of</strong> these types <strong>of</strong> modes are illustrated in Fig. 24.<br />

The umbrella-type modes are coupled only with the axial motion <strong>of</strong><br />

the rotating assembly. Since axial motion is usually <strong>of</strong> minor importance for<br />

rotordynamics systems, these modes are generally not <strong>of</strong> concern. All <strong>of</strong> the<br />

remaining modes, those with diametral nodal lines, are self-equilibrating<br />

with the exception <strong>of</strong> modes with a single nodal diameter such as illustrated<br />

in Fig. 24(b). The term ‘‘self-equilibrating’’ implies that the summations <strong>of</strong><br />

Copyright © 2003 Marcel Dekker, Inc.

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