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

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External loads during blade vibration are, the forces <strong>of</strong> inertia.<br />

<strong>The</strong> linear load from the force <strong>of</strong> iflertia is<br />

expressed by. equality<br />

f0¢2 (a)<br />

or,<br />

q = --QFtj,<br />

(a')<br />

where opF is2 the linear mass <strong>of</strong> the blade (the mass <strong>of</strong> a unit<br />

length <strong>of</strong> a blade);<br />

ýp, is- the; dens!ity, <strong>of</strong> the b2!ade;,materia-1l-;<br />

F is- the area .<strong>of</strong> the current blade cross section;<br />

= n(z, t) is the bending func~tion (the equation <strong>of</strong> an elastic<br />

line) o2 the blade.<br />

<strong>The</strong> externf.l force <strong>of</strong> inertia is<br />

ba~anced by- the internal<br />

elastic forces.<br />

As we know,<br />

the bending moment during bending <strong>of</strong> a beam is<br />

l-f<br />

A ,dz2 (b)<br />

or<br />

•"M, "E IEV (b",<br />

w.'ere E is the elasticity modulus <strong>of</strong> the first kind;<br />

I is the moment <strong>of</strong> inertia <strong>of</strong> the cross sectional area <strong>of</strong><br />

a blade relative to the ý ax1s.;<br />

1 nr is the second derivative with respect to z <strong>of</strong> the function<br />

<strong>of</strong> deflection.<br />

•:61

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