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In the figure, determine the normal stress and change in length of the aluminum rod if the temperature was raised by 126°C. The 0.5-mm gap exists at 25°C. 0.56 mm 366 mm 255 mm Aluminum A = 2TTT mm² E = 75 GPa x = 23 x 10*/°C B Stainless Steel A = 8QQ mm² E = 190 GPa α = 17.3 × 10%/°C

In the figure, determine the normal stress and change in length of the aluminum rod if the temperature was raised by 126°C. The 0.5-mm gap exists at 25°C. 0.56 mm 366 mm 255 mm Aluminum A = 2TTT mm² E = 75 GPa x = 23 x 10*/°C B Stainless Steel A = 8QQ mm² E = 190 GPa α = 17.3 × 10%/°C

Structural Analysis
Structural Analysis
6th Edition
ISBN:9781337630931
Author:KASSIMALI, Aslam.
Publisher:KASSIMALI, Aslam.
Chapter2: Loads On Structures
Section: Chapter Questions
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In the figure, determine the normal stress and change in length of the aluminum rod if the temperature was raised by 126°C. The 0.5-mm gap exists at 25°C. 0.56 mm 366 mm 255 mm Aluminum A = 2TTT mm² E = 75 GPa x = 23 x 10*/°C B Stainless Steel A = 8QQ mm² E = 190 GPa α = 17.3 x 10/°℃
Transcribed Image Text:In the figure, determine the normal stress and change in length of the aluminum rod if the temperature was raised by 126°C. The 0.5-mm gap exists at 25°C. 0.56 mm 366 mm 255 mm Aluminum A = 2TTT mm² E = 75 GPa x = 23 x 10*/°C B Stainless Steel A = 8QQ mm² E = 190 GPa α = 17.3 x 10/°℃
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