An axial force of 100 kN is applied to the assembly shown by means of rigid end plates. Determine (a) the normal stress in the aluminum shell, (b) the corresponding deformation of the assembly.
An axial force of 100 kN is applied to the assembly shown by means of rigid end plates. Determine (a) the normal stress in the aluminum shell, (b) the corresponding deformation of the assembly.
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Question
An axial force of 100 kN is applied to the assembly shown by means of rigid end plates. Determine (a)
the normal stress in the aluminum shell, (b) the corresponding deformation of the assembly.
![25 mm
Brass core
E = 105 GPa
300 mm
- Aluminium shell
E = 70 GPa
60 mm](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F97f57a47-3cf4-4499-a616-4ee0bd2006f7%2F39150800-f9e7-4900-8238-4ac8365ebbc5%2Fnpu5ddg_processed.png&w=3840&q=75)
Transcribed Image Text:25 mm
Brass core
E = 105 GPa
300 mm
- Aluminium shell
E = 70 GPa
60 mm
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