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

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<strong>The</strong> locus <strong>of</strong> points equidistant from the main surfaces <strong>of</strong> the<br />

shell is called the middle surface. <strong>The</strong> gecmetric shapes <strong>of</strong> a shell<br />

are completely determined by the shape <strong>of</strong> the middle surface <strong>and</strong> the<br />

law <strong>of</strong> variation for the shell thickness. As a rule, this thickness<br />

is constant.<br />

<strong>The</strong> most widely used are shells <strong>of</strong> revolution, i.e., shells<br />

which have a middle surface formed by the rotation <strong>of</strong> any plane<br />

curve around an axis lying in the plane <strong>of</strong> this curve <strong>and</strong> called<br />

the generatrix.<br />

If the middle surface is a plane, the shell is called a plate.<br />

<strong>The</strong> curve formed on the surface <strong>of</strong> the shell by the intersection<br />

<strong>of</strong> it by the plane passing through the axis is called the meridian.<br />

Obviously the meridians agree with the generatrices <strong>of</strong> the shell.<br />

<strong>The</strong> meridian's radius <strong>of</strong> curvature at any point is called the first<br />

principal radius <strong>of</strong> curvature R1 <strong>of</strong> the surface at a given point;<br />

the radius <strong>of</strong> curvature <strong>of</strong> the curve obtained from the intersection<br />

<strong>of</strong> the surface by a plane perpendicular to the meridian is called<br />

.the second principal radiusjR <strong>of</strong> the 4urface at a given point.<br />

Sometimes the word "principal" is omitted.<br />

<strong>The</strong> radii R1 <strong>and</strong> R2 are variable quantities characterizing th,•<br />

geometry <strong>of</strong> a shell <strong>of</strong> rotation. Completely geometric forms <strong>of</strong><br />

a shell <strong>of</strong> revolution are characterized by these two radii <strong>and</strong> the<br />

angle 0, formed by the normal to the middle surface <strong>and</strong> the axis<br />

<strong>of</strong> symmetry. Figure 2.20 presents these parameters for various<br />

types <strong>of</strong> single-layer shells.<br />

In engines, in addition to simple single-layer shelis, complex<br />

two- <strong>and</strong> multilayer shells are used, which have, as a rule, the<br />

shape <strong>of</strong> a body <strong>of</strong> revolution. Between the walls <strong>of</strong> the shells<br />

flows liquid or gas, frequently used for cooling the walls. Various<br />

types <strong>of</strong> complex multilayer shells are shown in Fig. 2.21.<br />

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