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

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SI<br />

Now we seek the pressure <strong>of</strong> the gases which cause this radial.<br />

strain. For this we find from formula (2.41) e = AR/R = 0.25/92 =<br />

= .72"103. Next we find e <strong>and</strong> 0:<br />

=• •-<br />

-a' t' = 2,72.1-- _10,4- 10-3 =--7,68-10-';<br />

t; •. -WaT" = 2,72.10-3-- l~610-3 = ,610-3.<br />

According to the known values <strong>of</strong> relative strains el <strong>and</strong> 0"<br />

from the graph a = f(C) presented in Fig. 2.37, we find the value<br />

<strong>of</strong> the stresses<br />

a' = -21.4"107 N/m 2 <strong>and</strong> a" = 9.4"10 7 N/m 2 .<br />

As mentioned above, we assume that with negative values <strong>of</strong><br />

9 the diagram a = f(e) has the same form as at positive values,<br />

only the sign <strong>of</strong> a changes.<br />

At low values <strong>of</strong> e the stress cs can be directly calculated<br />

from'formula a0 = EE9, where the Young's modulus for each temper.ture<br />

is taken from the graph presented in Fig. 2.38.<br />

In our case, E' = 1.6"1011 N/m 2 ; E" = 2'1011 N/m 2 .<br />

N<br />

1,8 .(2)~ Cm a.<br />

0,8xn9_ nb<br />

_<br />

,0 1....go t0<br />

Fig. 2.38. Variation in the Young's modulus <strong>of</strong> various materials.<br />

KEY: (1) N/m 2 ; (2) Steel.<br />

149

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