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14-119. The smooth rigid-body cavity is filled with liquid 606L-T6 aluminum. When cooled it is 0.3 mm from the top of the cavity. If the top of the cavity is covered and the temperature is increased by 110°C, determine the stress components os, ay, and o, in the aluminum. Hint Use Eqs 14-32 with an additional strain term of aAT (Eq. 9-4). 100mim 150 mm

14-119. The smooth rigid-body cavity is filled with liquid 606L-T6 aluminum. When cooled it is 0.3 mm from the top of the cavity. If the top of the cavity is covered and the temperature is increased by 110°C, determine the stress components os, ay, and o, in the aluminum. Hint Use Eqs 14-32 with an additional strain term of aAT (Eq. 9-4). 100mim 150 mm

Structural Analysis
Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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14-119. The smooth rigid-body cavity is filled with liquid 606L-T6 aluminum. When cooled it is 0.3 mm from the top of the cavity. If the top of the cavity is covered and the temperature is increased by 110°C, determine the stress components os, ay, and o, in the aluminum. Hint Use Eqs 14-32 with an additional strain term of aAT (Eq. 9-4). 100mim 150 mm
Transcribed Image Text:14-119. The smooth rigid-body cavity is filled with liquid 606L-T6 aluminum. When cooled it is 0.3 mm from the top of the cavity. If the top of the cavity is covered and the temperature is increased by 110°C, determine the stress components os, ay, and o, in the aluminum. Hint Use Eqs 14-32 with an additional strain term of aAT (Eq. 9-4). 100mim 150 mm
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