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

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<strong>Stress</strong>es in a circular diret.ion or<br />

05; (ro) = E u3 +<br />

-80. 10. 3.5.10-6.1411,5 + 12,) = 4,b2 daN/mm 2 ;<br />

2,(rj)= 1,77 6aIl.m.0.; c•(r)=--3,44 daN/mm 2<br />

Fi; .ire 5. ?i shows the tends <strong>and</strong> stresses <strong>of</strong> an anode.<br />

Integral method <strong>of</strong> solving the equation<br />

<strong>of</strong> a conical shell<br />

As 13 apparent from the example <strong>of</strong> shell analysis, the asymptotic<br />

method is rather cumbersome. In many cases, calculations should be<br />

r-erformed according to the integral method.<br />

Let us examine a case when the anode parameters h,<br />

constant <strong>and</strong> the only variable is At.<br />

E, D are<br />

<strong>The</strong> initial equation will have the form<br />

(r' )"--r WO + DrtgOe =Dtg" ( 5 .54)<br />

<strong>The</strong> procedure for solving the problem remains the same. We shall<br />

seek a general solution to equation (5.54) as the sum <strong>of</strong> its<br />

particular solution <strong>and</strong> a general solution without the right side:<br />

Wp = W0 + Wr.<br />

Let us find the particular solution. We assume that the temperature<br />

& 2<br />

gradient is given by formula At = B 0 + Blr + B 2 r<br />

We also assume wr = A 0 + Air + A 2 r 2 + A 3 r 3 . Let us substitute<br />

this expression into (5.54), equate the terms with identical<br />

functions relative to r, <strong>and</strong> obtain the values for AO; A 1 ; A 2 ; A 3<br />

<strong>and</strong>, consequently, w :<br />

572<br />

mmm _ m ~ lm m •.<br />

ip • • _ • : -- :. . ,e .- m

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