In the figure shown below, determine: 1) The final temperature if the normal stress at aluminium is Oa = -90 MPa and the initial temperature 20°C. 2) The final length of the aluminium member. Aluminum A=1800mm? E=73GPA a=23.2x10-6/°C Bronze A=1500mm? E=105GPA a=21.6x10-6/°C Gap=0.5mm 0.35m 0.45m

In the figure shown below, determine: 1) The final temperature if the normal stress at aluminium is Oa = -90 MPa and the initial temperature 20°C. 2) The final length of the aluminium member. Aluminum A=1800mm? E=73GPA a=23.2x10-6/°C Bronze A=1500mm? E=105GPA a=21.6x10-6/°C Gap=0.5mm 0.35m 0.45m

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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