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

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Example 5.1.<br />

Find the stress <strong>and</strong> the coefficient <strong>of</strong> safety<br />

for a cylindrical anode whose dimensions are shown in Fig. 5.22<br />

if the following is given: material is Khl8N9T steel; E = 1.45.10'<br />

daN/mm2; a = (21.2-22.2)10-6 I/C. <strong>The</strong> left end <strong>of</strong> the anode is<br />

rigidly attached.<br />

is<br />

distributed linearly.<br />

<strong>The</strong> temperature along the length <strong>of</strong> the anode<br />

1. Law <strong>of</strong> temperature variation along the anode is<br />

At = B0 + B 1 X.<br />

From the condition when x = 0 At = 430'C; when x = 1 At = 58000<br />

we obtain B 0 = 430; B 1 = 4.3.<br />

2. Let us evaluate the length <strong>of</strong> a shell:<br />

.• - 3 1 rh= 3 J 50.0,-5=1 .1..t,<br />

i.e., the shell is long; Z = 35.<br />

3. We find the reaction Q <strong>and</strong> MO. If the shell did not have<br />

an attachment, its deformation would be equal to the deformation<br />

<strong>of</strong> a free shell, i.e., 6 = rcAt; at the attachment point<br />

6= raAt 0 = 50'21.2*10- 6 "130 = 0.455 mm.<br />

Since the shell is<br />

attached, we deform its end by quantity<br />

60= -0.455 <strong>and</strong> find what force QO <strong>and</strong> moment M 0 should be applied<br />

for this. We solve the system <strong>of</strong> equations (5.19) with boundary<br />

conditions:<br />

! ~~~x = O; zt, (o) =- , '(o) =<br />

V (0) (3Mo +QJ) =- to, W'(o)=---L (31MIO 4-Qo)=O<br />

w -2.sD<br />

2:"-OD<br />

hence<br />

Qo<br />

M 0 • 2,.N = 2.0.9-:572.••N6,3.0,455 = 10,02 daN mm/nmm;<br />

-'1-31)-,, -=- 1.0, 2573.166,3-0.455 =.-5, 14 daN/inn.<br />

539

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