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

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

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Functions S, T, U <strong>and</strong> V during differentiation have the property<br />

<strong>of</strong> circular replacement, i.e.,<br />

S" ( a)=2U (a-); S"'(a7)== 'T (a-);<br />

T (aZ);<br />

T' (a)=aS (C);<br />

T" (a )=•-•V ( 7s); T" (a)= L (Z);<br />

U(c); U' ( a)=raT (jz);<br />

U" (a) =a-s (aii); U", (Ci,•) =a 3 " (a-);<br />

v (Q); V' (a.) =au ()<br />

V"/(a1).=u-T(a); V"(Z')=a3S(UZ). )<br />

(3.33)<br />

<strong>The</strong> use <strong>of</strong> these functions makes it possible to immediately<br />

obtain a solution to equation (3.28) which satisfies the boundary<br />

conditions. We have the following boundary conditions for our<br />

problem:<br />

1) " = 0; u(0) = 0 (deflection in-the seal is zero);<br />

2) z = 0; u'(0) = 0 (the angle <strong>of</strong> pitch <strong>of</strong> the section in the<br />

framing is equal to zero);<br />

3) • = 1; u"(M) = 0 (bending moment at the free blade tip is<br />

equal to zero);<br />

4) -z = 1; u"0(a) = 0 (shearing force at the free blade tip is<br />

equal to zero).<br />

If we use the first two boundary conditions, we obtain A = 0;<br />

B = 0. <strong>The</strong>n the solution to (3.31') will be<br />

u() =CU(,;):+Dv (a). (3.31")<br />

We shall use the third <strong>and</strong> fourth botu•dary condition.s (when = 1).<br />

From formulas (3.33) we obtain:<br />

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