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

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* "1<br />

Fig. 2.25. A: cylindrical<br />

single-layer shell.<br />

' -X (b)<br />

(a)<br />

P<br />

A<br />

Thus, the peripheral stress a in the walls <strong>of</strong> a cylindrical<br />

she:ll is twice as great as ithe axial stress a Also important is<br />

the fact that this peripheral stress is almost equal to the equivalent<br />

stress which determines the strength <strong>and</strong> the supporting capacity <strong>of</strong><br />

the shell. Actu~lly, equivalent stress<br />

*<br />

since =k : 0.507.<br />

I<br />

<strong>The</strong> forniula (2.33) is widely used in rough calculations <strong>of</strong> more<br />

pomplex design.<br />

I<br />

I<br />

<strong>The</strong> safety coefficient <strong>of</strong> the shell is<br />

found by the usual method:<br />

SI 2<br />

I<br />

i(2.35)<br />

depending upon the purpose <strong>of</strong> the element n = 1.2-1.5.<br />

End plate <strong>of</strong> a cylindrical shell<br />

II<br />

Frequently single4-layer cylindrical shells have a closed shape.<br />

One <strong>of</strong> the possible forms <strong>of</strong> the end part is a sphere with a radius<br />

equal to the radius <strong>of</strong> the cylinder, i.e., r = R (Fig. 2.26).<br />

* II<br />

1311<br />

! ~ -~

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