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Design and Stress Analysis of Extraterrestrial ... - The Black Vault

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<strong>The</strong> angular velocity w A<strong>of</strong> natural vibrations,, with rotation<br />

taken intc account, is<br />

determi.ned from formula<br />

A<br />

w+Bw C<br />

2 (3.48)<br />

where w. is the angular velo,,viy <strong>of</strong> natural vibrations in a nonrotating<br />

blade;<br />

w is the angular velocity;<br />

B is the coefficient allowing for the effect <strong>of</strong> centrifugal<br />

forces on the natural frequency <strong>of</strong> a blade.<br />

Coefficient B depends on the geometric dimensions <strong>of</strong> the blade<br />

<strong>and</strong> can be determined from formula<br />

F(ro+ z) dz<br />

dz'•<br />

(3.4 9)<br />

where F is the current cross-sectional Area <strong>of</strong> the blade.<br />

Figure 3.28 shows the character <strong>of</strong> variation in w as a function<br />

<strong>of</strong> the angular velocIty <strong>of</strong> the rotor.<br />

<strong>The</strong> effect <strong>of</strong> blade heating on the frequency<br />

<strong>of</strong> its natural vibrations<br />

During turbine operation from the moment <strong>of</strong> starting up to the<br />

steady run the gas temperature <strong>and</strong> blade temperature vary.<br />

Due to the increase in blade temperature with a change in w<br />

the modulus <strong>of</strong> elasticity for the material is reduced, which leads<br />

to a reduction in the frequency <strong>of</strong> natural vibration, as shown in<br />

Fig. 3.28 (dashes).<br />

If the blade temperature for each mode is known then we can<br />

account for the effect <strong>of</strong> heating from formula<br />

282

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