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Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

Fluid Mechanics and Thermodynamics of Turbomachinery, 5e

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154 <strong>Fluid</strong> <strong>Mechanics</strong>, <strong>Thermodynamics</strong> <strong>of</strong> <strong>Turbomachinery</strong><br />

FIG. 5.5. Simplified <strong>of</strong>f-design performance <strong>of</strong> a compressor stage (adapted from<br />

Horlock 1958).<br />

The values <strong>of</strong> yd <strong>and</strong> fd chosen for a particular stage design determines the value <strong>of</strong> t.<br />

Thus t is fixed without regard to the degree <strong>of</strong> reaction <strong>and</strong>, therefore, the variation <strong>of</strong><br />

stage loading at <strong>of</strong>f-design conditions is not dependent on the choice <strong>of</strong> design reaction.<br />

However, from eqn. (5.13) it is apparent that, except for the case <strong>of</strong> 50% reaction<br />

when a1 = b2, the reaction does change away from the design point. For design reactions<br />

exceeding 50% (b 2 > a1), the reaction decreases towards 50% as f decreases;<br />

conversely, for design reactions less than 50% the reaction approaches 50% with diminishing<br />

flow coefficient.<br />

If t is eliminated between eqns. (5.20a) <strong>and</strong> (5.20b) the following expression results,<br />

(5.21)<br />

This equation shows that, for a given design stage loading yd, the fractional change<br />

in stage loading corresponding to a fractional change in flow coefficient is always<br />

the same, independent <strong>of</strong> the stage reaction. In Figure 5.6 it is seen that heavily loaded<br />

stages (yd Æ 1) are the most flexible producing little variation <strong>of</strong> y with change <strong>of</strong><br />

f. Lightly loaded stages (yd Æ 0) produce large changes in y with changing f.<br />

Data from cascade tests show that yd is limited to the range 0.3 to 0.4 for the most efficient<br />

operation <strong>and</strong> so substantial variations <strong>of</strong> y can be expected away from the design<br />

point.<br />

In order to calculate the pressure rise at <strong>of</strong>f-design conditions the variation <strong>of</strong> stage<br />

efficiency with flow coefficient is required. For an ideal stage (no losses) the pressure<br />

rise in incompressible flow is given by<br />

(5.22)

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