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

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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