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

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x or r (distance al- g the generatrices <strong>of</strong> the shell from the<br />

summit <strong>of</strong> thE -one to the examined section).<br />

Figure 5.27 shows the positive internal loads applied to an<br />

element cut out <strong>of</strong> a conical shell. Let us find the membrane stresses<br />

a, <strong>and</strong> a <strong>and</strong> strains <strong>of</strong> the shell.<br />

If fae assume, for exariple, that the internal pressure on the<br />

shell is constant <strong>and</strong> acts on the entire internal surface <strong>of</strong> an<br />

uncut snell (Fig. 5.28), the axial force in an arbitrary section<br />

is determined by radius r:<br />

-N., = p;Tr2 sinl2 0, •.n .(5.38)<br />

where 0 is<br />

the angle cf the generatrix <strong>of</strong> the shell with the x-ax).:<br />

perimeter:<br />

Axial force N x causes normal stresses constant along the<br />

nrh sin 20<br />

where h is<br />

the thickness <strong>of</strong> the shell <strong>and</strong> generally variable.<br />

Particularly, when Nx is determined from formula (5.38),<br />

pr t •r-• tg 0."<br />

Let us find circular stresses a., We shall examine the eqLilibrium<br />

<strong>of</strong> the shell element (Fig. 5.29) separated into spherAcal co<br />

conical section.<br />

Projecting the external <strong>and</strong> internal forces onto t!e normal<br />

to the surface <strong>of</strong> the shell, we obtain plidpdr -OahdrdcI,<br />

557

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