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

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In order to find the relationship between the coefficient <strong>of</strong><br />

rigidity <strong>and</strong> unit load, let us examine a beam on two supports loaded<br />

by force P <strong>and</strong> moment M (Fig. 3.70) Under the effect <strong>of</strong> the force<br />

<strong>and</strong> the moment the beam at point 1 will be deflected by quantity y<br />

<strong>and</strong> turned by angle a-.<br />

If we use a "method <strong>of</strong> deformation," we can express the force<br />

<strong>and</strong> the moment in terms <strong>of</strong>, deformations:<br />

P=CIIY+C 1 2 a1; M=c 2 1Y1+C2 (3. 117)<br />

where cl, c 1 2 , c21' <strong>and</strong> c 22 are the i 1 tidity coefficients.<br />

Fig. 3.70. Determining the rela- I<br />

tionship between the coefficients<br />

<strong>of</strong> rigidity <strong>and</strong> unit load.<br />

From the system <strong>of</strong> equ.tions. (3.117) we find the value <strong>of</strong><br />

deflection y <strong>and</strong> the angle <strong>of</strong> turn a:<br />

P~ C12L<br />

Af = I= - P-- -- M<br />

I<br />

C21 C22I<br />

~1C<br />

C22 IC22<br />

C21 M 21 P+ C11 M<br />

JCH C12C1K2--C1 1C2-C2<br />

cnc --c• ( 3.118)<br />

On the other h<strong>and</strong>, if we use the "method <strong>of</strong> forces, we can<br />

express the deflection y <strong>and</strong> angle turn a in terms <strong>of</strong> force P <strong>and</strong><br />

moment M:<br />

f 363

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