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ME211_Sol12 - 1-102 The smooth rigid-body cav ity is 1Ied...

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,5r ii:5 9o i-&-) c3 r —c COO 7 Si 7i’€ ro.ds of ite cc 4 g Jf 0 , )af 40 2 -. 3 - P(e”e Pricpt ( 1e,: 7Le 1oTdaas 01 L ot 112ad S )erJetiL 4 6, qlA/ 6 J, sfec’e. f. SQ - 7.I t t34 9 Thiee Mohr Csc4j Pio t iLe n’sLl(tf QLT 4 eI *Lo’e, - (cc’ psi’ / 1o(c Mcii. Letir c-&tss: fLo uie /t,1obr c’ic&s T;45 ((‘a) 2- 2- 1 -102. The smooth rigid-body cavity is 1Ied with liquid 061-T6 aluminum. When cooled it is 0012 in. from the top of the cavity. If the top of the cavity is not covered and the temperature is increased by 200° F, determine the strain components e,, e,, and e in the aluminum. Hint: Use Eqs. 15-32 with an additional strain term of aT (Eq.10-4). iite rjt: MoLr C,’fC(’t 74K 4’4 tL. y_i &te c i&ui fict. l iZ’ 4 ø. w ILe - ao( 9’s 4f 9. qç. q&. q s1ruci of cr
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cs 2 -qc f 4 (s(ç) 2(o(ro o. c iy 0. Ci J I = (8t ((0 ) .. 24 0 4 ç -‘ - dtny Ef s. tiJ ii yWd 1 . ftg Crd€ k/ 7 ’j fCo ), = -13 o(’) ( =-i75 ((06) e L ‘i” C- - 6) j(o ) 2.u((0 7?e oro 64 -/ po A d C are A (i. -27c) ao 4 ) c 2S0, o) (06) Tt..€ raas g (Jü-v #.ic’ ) - P1aie fiya TLe cv of ptr J t) Ci ey,erfs’8.
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