Aaircraft strut consists of two cylindrical portions ab and bc and is restrained at both ends. portion ab is made of 7075-t6 aluminum (eal = 10.4 msi, αal = 13.1 x 10-6 /°f) and portion bc is made of 6al-4v titanium (eti = 16.5 msi, αti= 5.3 x 10-6 /°f). if the strut is initially unstressed but is then subjected to a temperature rise of 70°f, determine the normal stresses induced in portions ab and bc by the temperature rise.
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Aaircraft strut consists of two cylindrical portions ab and bc and is restrained at both ends. porti...
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