Do not round intermediate answers. Give your final answer(s) to three decimal places. Check your units. The aluminum shell is fully bonded to the brass core and the assembly is unstressed at a temperature of 25°C. Considering on axial deformations, determine the stress in the aluminum when the temperature reaches 170°C. 40 mm, 55 mm Brass core E = 105 GPa a = 20.9 × 10-6/°C Aluminum shell E = 70 GPa α= 23.6 × 10-6°C σ (AI) = MPa Check Answer for this Problem Close
Do not round intermediate answers. Give your final answer(s) to three decimal places. Check your units. The aluminum shell is fully bonded to the brass core and the assembly is unstressed at a temperature of 25°C. Considering on axial deformations, determine the stress in the aluminum when the temperature reaches 170°C. 40 mm, 55 mm Brass core E = 105 GPa a = 20.9 × 10-6/°C Aluminum shell E = 70 GPa α= 23.6 × 10-6°C σ (AI) = MPa Check Answer for this Problem Close
Materials Science And Engineering Properties
1st Edition
ISBN:9781111988609
Author:Charles Gilmore
Publisher:Charles Gilmore
Chapter6: Introduction To Mechanical Properties
Section: Chapter Questions
Problem 6.2P
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