Find normal stresses in the steel core and aluminum shell


Compressive centric forces of 160 kN are applied at both ends of the assembly shown by means of rigid plates. Knowing that Es = 200 GPa and Ea = 70 GPa determine (a) the normal stresses in the steel core and the aluminum shell, (b) the deformation of the assembly Rs=25mm, Ra=62mm, L=250mm

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Mechanical Engineering: Find normal stresses in the steel core and aluminum shell
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