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

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i.e.,<br />

the plate bends along a spherical surface whose curvature<br />

is defined by the quantity 1/rx = r = 1/r. <strong>The</strong> stress<br />

ax cay =a= 6f/h 2<br />

4Z<br />

- A tc<br />

b ~tb *At x ~ 3 8 a<br />

) (a)<br />

Fig. 4.17.<br />

Determining the temperature gradient.<br />

Let us examine the deformation-<strong>of</strong> a plate during thermal loading.<br />

If<br />

we read the temperature from the middle surface <strong>of</strong> the plate,<br />

assuming that on one side it is heated <strong>and</strong> on the other cooled,<br />

it is natural to concluae that the thermal deformations <strong>of</strong> expansion<br />

<strong>and</strong> contraction will be proportional to the distance from the middle<br />

surface.<br />

Consequently, we arrive at the same deformation law as in<br />

the pure bend <strong>of</strong> a plate by bending moments.<br />

If heat is supplied to <strong>and</strong> drawn from-a plate which is uniformly<br />

heated to temper, .ure to, as was shown in Fig. 4.17a, it can be<br />

established that in<br />

the steady thermal mode the temperature variation<br />

along the thickness will be linerr, while the temperature <strong>of</strong> the<br />

plate's neutral surface will remain constant, i.e.,<br />

be equal to<br />

Such a temperature variation in<br />

a section causes analogous<br />

thermal deformation. <strong>The</strong>se daformations in an unattached plate will<br />

be proportional to the distance from the middle surface; thus, the<br />

law <strong>of</strong> variation for thermal deformation is<br />

completely identical<br />

to the law-<strong>of</strong> deformation with a pure bend by bending moments.<br />

Figure 4.17a shows the temperatures <strong>of</strong> a plate element during such<br />

heating.<br />

458

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