01.07.2014 Views

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

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

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

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

We<br />

determine<br />

1.29 1.29<br />

D' Eh3 1,45 104.0,53 166.3 daNmm.<br />

1i2(1- •,) 12(1_o,.2)<br />

L4. We find<br />

P -o j1Afcs Ix-- sin ýx) + Qo ros •xj + • lo +t•;<br />

" 2jP3D<br />

0ý=- , where wy=wp-raI.<br />

r<br />

Calculation is reduced in Table 5.2.<br />

coefficients:<br />

Let us determine the<br />

2PD = 2.0,2573.166,3 = 5,65 daN/mm2;<br />

fo -- 0,257.-10,02--- 2,58 daN/mm;<br />

E - 1,45.104 290 daN/mm 3 .<br />

r 50<br />

<strong>The</strong> bend determining the stress in a cylindrical shell is<br />

found in line 10.<br />

Actually,<br />

w p<br />

r.CAl; sincewP = u 0 + t <strong>and</strong> ? raMf, then Wy = WO.<br />

Figure 5.22 presents curves <strong>of</strong> w 0 , wy,<br />

bend w, as a result <strong>of</strong> its heating.<br />

6 <strong>and</strong> the total anode<br />

5. We find<br />

w" [- [}M (cos 3x + sin Ox) + Qo sin Sx];<br />

6Dw' •=h2I<br />

.' %(M) = Pox.<br />

540

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!